E N G L I S H   T O   D U T C H   T R A N S L A T I N G  
  Peter de Jong
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  AERMACCHI – Italy
The Macchi aircraft factory in Varese was renamed Aermacchi in 1962. The company is now part of the Finmeccanic holding, grouped together with Alenia.
MB.326
FIRST FLIGHT 1957
One of the classic jet trainers for basic flying training conceived in the 1950s and 1960s, the MB.326 also appeared in single-seat form as a light attack aircraft, the MB.326K. The MB.326 was built not only in Italy,
but also in Australia, in Brazil (as the Embraer AT-26 Xavante) and in South Africa (as the Atlas Impala).
 
MB.326G
length 10.64 m (34 ft 11 in)
span 10.85 m (35 ft 7 in)
engine 1 × Rolls-Royce Viper, 1547 kg (3410 lb) thrust
max take-off weight 5217 kg (11,500 lb)
max speed 867 km/h (539 mph)
capacity 2 persons
MB.339
FIRST FLIGHT 1976
The MB.326's successor features a redesigned nose section, improving the instructor pilot's vision over his pupil's head. The MB.339 is used for both basic and advanced flying training in the Italian Air Force; with its straight wing and old Viper engine, however, it does not belong in the same class as the Alpha Jet or BAE Hawk.
 
MB.339A
length 10.97 m (36 ft 0 in)
span 10.85 m ( 35 ft 7 in)
engine 1 × Rolls-Royce Viper, 1814 kg (4000 lb) thrust
max take-off weight 5897 kg (13,000 lb)
max speed 898 km/h (558 mph)
capacity 2 persons
  AERO – Czech Republic
Aero Vodochody, based at Vodochody airfield, near Prague, dates back to 1919.
 
Ae 45
FIRST FLIGHT 1947
The rounded nose of this classic four to five-seat travel aircraft may have been inspired by the German Siebel Si 204, which was produced at Aero during World War II. Despite the limited need for such aircraft in the Eastern Bloc, some 800 Ae 45's were built in several variants, including the Ae 145, and used as far afield as China.

 

 
Ae 45S
length 7.54 m (24 ft 9 in)
span 12.60 m (46 ft 7 in)
engine 2 × Walter Minor, 2 × 105 hp
max take-off weight 1510 kg (3322 lb)
max speed 270 km/h (168 mph)
capacity 4-5 persons
 
L-29 Delfin
FIRST FLIGHT 1959
The winner of a 1961 competition, the Delfin (Dolphin) was selected as standard basic flying trainer for all the Warsaw Pact countries, except Poland, which wished
to proceed with the indigenous PZL TS-11 Iskra. Out of a total of 3500, the Soviet Union took delivery of over 2000 Delfins. The type was succeeded by the L-39 Albatros.
 
 
L-29
length 10.81 m (35 ft 6 in)
span 10.29 m (33 ft 9 in)
engine 1 × Motorlet M701, 890 kg (1960 lb) thrust
max take-off weight 3540 kg (7800 lb)
max speed 655 km/h (407 mph)
capacity 2 persons
 
L-39 / L-59 Albatros
FIRST FLIGHT 1968
The first jet trainer to be powered by a turbofan engine, the L-39 is comparatively economical to operate. About 3000 L-39s were built, many going to the Soviet Union. Currently in production is the L-59 Super Albatros, which features an uprated engine and a modernized cockpit. Although many older L-39s remain military use, some 300 have been sold to wealthy private pilots in the USA.
 
 
L-39C
length 12.13 m (39 ft 10 in)
span 9.46 m (31 ft 0 in)
engine 1 × Ivchenko AI-25, 1720 kg (3792 lb) thrust
max take-off weight 4700 kg (10 362 lb)
max speed 750 km/h (466 mph)
capacity 2 persons
 
L-159
FIRST FLIGHT 1997
In 1993 Aero flew the L-139 trainer, a modernized L-39 with a US TFE731 engine. It did not reach production, but led to the development of the L-159A single-seat light combat aircraft, powered by the TFE731-derived F124. The rear seat was simply replaced by a fuel tank.
The Czech Republic bought 72 L-159As, but most are
in storage; a few were converted to two-seat trainers.
 
 
L-159A
length 12.72 m (41 ft 8 in)
span 9.54 m (31 ft 3 in)
engine 1 × Honeywell F124, 2849 kg (6280 lb) thrust
max take-off weight 8000 kg (17 637 lb)
max speed 935 km/h (544 mph)
capacity 1 person
 
  AGUSTA – Italy
Giovanni Agusta flew his first aircraft in 1907, and started his own company at Cascina Costa, near Milan-Malpensa. After World War II it produced motorcycles before starting to build Bell helicopters under licence. Its own helicopter designs were unsuccesful until the appearance
of the A109. Agusta merged with Westland to form Agusta Westland.
 
A109
FIRST FLIGHT 1971
Originally named Hirundo (Swallow), the A109 is a fast and succesful helicopter for business, ambulance and military purpooses. Several versions have been built, including the current production A109E, named Power, which has Arrius or PW206 engines. In China, Changhe
Aircraft Industries produces the aircraft as the CA109.

 

 
A109A Mk.II
fuselage length 10.73 m
  (35 ft 2 in)
rotor diam 11.32 m (37 ft 2 in)
engine 2 × Allison 250, 2 x 420 hp
max take-off weight 2600 kg (5730 lb)
max speed 311 km/h (193 mph)
capacity 8 persons
 
  AGUSTA WESTLAND – Italy / United Kingdom
Partners in the AW101 project, Agusta and Westland were merged in 2000 by their parent companies, Finmeccanica and GKN. Finmeccanica is now the sole owner.
 
AW101 / Merlin
FIRST FLIGHT 1987
Previously designated EH101, and named Merlin by the British military, the AW101, powered by three RTM322 or T700 engines, is a large helicopter for naval use as well as military and passenger transport. A Canadian search and rescue variant is designated CH-149 Cormorant. A US version, the Lockheed VH-71 Kestrel VIP helicopter for presidential use was cancelled in 2009 because of the excessive cost of over 6 billion dollars for 23 aircraft.

 

 
Merlin HC.3
fuselage length 19.53 m
  (64 ft 1 in)
rotor diam 18.59 m (61 ft 0 in)
engine 3 × Rolls-Royce / Turboméca RTM322, 3 x 2312 hp
max take-off weight 15 600 kg (34 392 lb)
max cruising speed 278 km/h (173 mph)
capacity 30 passengers
 
AW139
FIRST FLIGHT 2001
Initially designated AB.139, the AW139 was developed by Agusta and Bell, but the American company withdrew from the project. Engines are either PT6 or CT7 turbines. Assembly takes place in Italy and in Agusta Westland's US plant in Philadelphia. An enlarged AW149 is under development, primarily as a military transport helicopter.

 

 
AW139
fuselage length 13.52 m
  (44 ft 4 in)
rotor diam 13.80 m (45 ft 3 in)
engine 2 × Pratt & Whitney Canada PT6, 2 x 1530 hp
max take-off weight 6400 kg (14 110 lb)
max speed 310 km/h (193 mph)
capacity 15 passengers
 
  AIRBUS – France / Germany / Spain
Airliners developed by national European manufacturers were often commercially unsuccesful, and in the early 1970s the French, German, British and Spanish industries joined forces in the Airbus consortium. Airbus is now a subsidiary of EADS, British partner BAE having withdrawn. Airbus has assembly lines in Toulouse, Hamburg and Seville. Wings are still made in Filton, UK.
 
A300
FIRST FLIGHT 1972
The first Airbus product was the A300 medium-range large airliner. 561 were built, with the A300B2, A300B4 and A300-600 as the main versions, the latter having the redesigned tail section and two-man cockpit of the A310. Its wide fuselage makes the A300 an attractive freighter, and many airframes have been built of rebuilt as such.
 
 
A300-600
length 54.08 m (177 ft 5 in)
span 44.84 m (147 ft 1 in)
engine 2 × General Electric CF6, 2 × 25 400 kg (56 000 lb) thrust
max take-off weight 165 000 kg (363 760 lb)
max cruising speed 890 km/h (553 mph)
capacity 267-344 passengers
 
A310
FIRST FLIGHT 1982
Originally designated A300B10, the A310 is a shortened A300 featuring a new, smaller wing, a redesigned tail section and a two-man cockpit. Like its larger brother it is powered by either GE CF6 or P&W JT9 turbofans. 255 examples were built, including longer-range A310-300s. The A310 MRTT military tanker/transport conversion, ordered by the German and Canadian air forces, is fitted with two hose-type aerial refuelling units on its wingtips.
 
 
A310-300
length 46.66 m (153 ft 1 in)
span 43.90 m (144 ft 0 in)
engine 2 × General Electric CF6, 2 × 22 680 kg (50 000 lb) thrust
max take-off weight 150 000 kg (330 688 lb)
max cruising speed 890 km/h (553 mph)
capacity 218-280 passengers
 
  ALENIA – Italy
Alenia has its origins in the aircraft factory of the Fiat company. Now part of the Finmeccanica group, Alenia is involved in various international projects including AMX, ATR and Eurofighter.
 
G-222 / C-27J Spartan
FIRST FLIGHT 1970
At first envisaged with a battery of vertical take-off liftjets by Fiat designer Gabrielli, the G.222 was ultimately built as a conventional military transport aircraft, powered by two T64 or Tyne turboprop engines only. A little over 100 G.222s were built, including a few for the US Air Force under the C-27A Spartan designation. The C-27J is a modernized version which entered production in 2000.
 
 
C-27J
length 22.70 m (74 ft 6 in)
span 28.70 m (94 ft 2 in)
engine 2 × Rols-Royce AE2100, 2 x 4640 hp
max take-off weight 30 500 kg (67 241lb)
max speed 602 km/h (374 mph)
capacity 60 passengers
 
  ANTONOV – Ukraine
Born in Moscow, Oleg Antonov (1906-1984) designed gliders and Yakovlev light aircraft before starting his own design bureau, which moved to Kiev in Ukraine in 1952. Antonov has produced a remarkabe series of transport aircraft from small to very large. It is now looking for markets for its newest aircraft, the An-70 mililtary transport and the An-140 and An-148 regional airliners.
 
An-2
FIRST FLIGHT 1947
A slow biplane was an excellent solution when Antonov was asked to develop an agricultural aircraft to spray the Soviet Union's vast collective farms. Able to carry twelve people as well as pesticides, the An-2 Colt became a 'Siberian school bus', and the standard light transport aircraft, civil and military, for the communist world. Over 18 000 An-2s were built, including 13 000 by PZL-Mielec in Poland, and hundreds more in China, known as Y-5s.
 
 
An-2P
length 12.40 m (40 ft 8 in)
span 18.18 m (59 ft 8 in)
engine 1 × Shvetsov ASh-621, 1000 hp
max take-off weight 5500 kg (12 125 lb)
max speed 258 km/h (160 mph)
capacity 12-14 passengers
 
An-10 Ukraina
FIRST FLIGHT 1957
Derived from the An-8, a freighter powered by two turbo- prop engines, the An-10 was a four-engined airliner, comparable to the Il-18 but able to use more primitive airports. Capacity varied from 84 seats, with a children's playground in the rear, in the original model to up to 115 in the stretched An-10A. Just over 100 examples were built. They were withdrawn from airline service in 1973, fatigue cracks having been discovered following a crash.
 
 
An-10A
length 34.00 m (111 ft 7 in)
span 38.00 m (124 ft 8 in)
engine 4 × Ivchenko AI-20, 4 x 4000 hp
max take-off weight 55 100 kg (121 473 lb)
max cruising speed 680 km/h (423 mph)
capacity 100-110 passengers
 
  BELL – United States
In 1935, Larry Bell left Consolidated Aircraft to form his own company in Buffalo, New York. Bell produced a number of unconventional fighters and experimental aircraft, including the X-1, but found its real domain as a helicopter manufacturer, producing the iconic helicopter types of both the Korean War and the Vietnam War. The company is now headquartered in Fort Worth, Texas.
 
P-63 Kingcobra
FIRST FLIGHT 1942
Like its predecessor, the P-39 Airacobra, the P-63 had its engine mounted behind the cockpit, a long propeller shaft leaving the nose free for armament, including a
37-mm cannon firing through the hub. The P-63 was not used in combat by US forces during World War II. The Soviet Union received most of the 3000 P-63s produced, and used them as attack aircraft on the Eastern Front.

 

 
P-63A
length 9.96 m (32 ft 8 in)
span 11.68 m (38 ft 4 in)
engine 1 × Allison V-1710, 1325 hp
max take-off weight 4763 kg (10 500 lb)
max speed 660 km/h (410 mph)
capacity 1 person
 
47 / H-13 Sioux
FIRST FLIGHT 1945
Designed mostly by Arthur Young, the Bell 47 was the first helicopter type in the world to gain civil certification. Designated OH-13, it was employed by the US Army for scouting and liaison work, and as an ambulance fitted with external litters of MASH fame. Over 5600 Bell 47s were built by Bell, Westland, Agusta, and Kawasaki. Some models, including the Bell 47J Ranger, had convential cabins rather than the trademark 'fish bowl'.

 

 
47G-3B
fuselage length 9.63 m
  (31 ft 7 in)
rotor diam 11.32 m (37 ft 2 in)
engine 1 × Lycoming O-435, 280 hp
max take-off weight 1340 kg (2950 lb)
max speed 169 km/h (105 mph)
capacity 3 persons
 
204 / H-1 Huey
FIRST FLIGHT 1956
Benefitting from a light, yet powerful turboshaft engine, the Bell 204 was developed for the US Army, which successively designated it H-40, HU-1, and UH-1. The nickname 'Huey' prevailed over the official Army name, Iroquois. Hundreds of UH-1As, -Bs and -Cs were used in Vietnam, though the larger UH-1D/-H was much more numerous. The 204 was also built by Fuji and Agusta, Italian models including the AB.204AS naval helicopter.

 

 
204B
fuselage length 12.31 m
  (40 ft 4 in)
rotor diam 14.63 m (48 ft 0 in)
engine 1 × Lycoming T53, 1100 hp
max take-off weight 4310 kg (9500 lb)
max speed 222 km/h (138 mph)
capacity 10 persons
 
205 / H-1D/-H Huey
FIRST FLIGHT 1960
An enlarged 204, the Bell 205 was designed to carry a squad of ten soldiers plus two gunners. The military designation of this H-1 model was UH-1D, or UH-1H with an uprated engine. 7000 were built for the US Army, which lost thousands of Hueys in Vietnam. Others were produced in Germany, Italy, Japan, and Taiwan. Many remain in service. The 212 is a twin-engined variant.

 

 
UH-1H
fuselage length 12.77 m
  (41 ft 11 in)
rotor diam 14.63 m (48 ft 0 in)
engine 1 × Lycoming T53, 1400 hp
max take-off weight 4765 kg (10 500 lb)
max speed 204 km/h (127 mph)
capacity 15 persons
 
212 / H-1N Twin Huey
FIRST FLIGHT 1968
Offering enhanced safety, the Bell 212 is a twin-engined variant of the 205. Developed for the Canadian military, it also found its way to the US armed forces as the UH-1N, and to other military and civil customers. Agusta-built AB.212 models include the AB.212ASW naval helicopter. The US Marines' UH-1Y, with much more powerful T700 engines, has a four-bladed rotor, as does the Bell 412.

 

 
212
fuselage length 12.92 m
  (42 ft 5 in)
rotor diam 14.69 m (48 ft 2 in)
engine 2 × Pratt & Whitney Canada PT6, 2 × 900 hp
max take-off weight 5080 kg (11 200 lb)
max speed 241 km/h (150 mph)
capacity 15 persons
 
412
FIRST FLIGHT 1979
An updated version of the Bell 212, the 412 features a composite four-bladed rotor to improve performance and reduce noise and vibration. Military models are named CH-136 Griffon by the Canadian Forces, Griffin by Britain's RAF, and Grifone by Agusta, which again manufactures its own versions of this ultimate Huey model. Bell 412s are also being produced in Indonesia.
 
 
412SP
fuselage length 12.70 m
  (41 ft 9 in)
rotor diam 14.02 m (46 ft 0 in)
engine 2 × Pratt & Whitney Canada PT6, 2 × 900 hp
max take-off weight 5397 kg (11 900 lb)
max speed 259 km/h (161 mph)
capacity 15 persons
 
206 / H-58 Kiowa
FIRST FLIGHT 1962
Designed as an observartion helicopter for the US Army, the Bell 206/OH-4 lost out to the Hughes 500/OH-6, but achieved success on the civil market as the JetRanger. It was yet selected by the US Army as the OH-58 Kiowa, the latest model being the OH-58D with a sight system mounted on the rotor head. The 206L LongRanger is a stretched seven-seater. The twin-engined 206LT was unsuccesful. The 206 was also built by Agusta in Italy.

 
206B-3 JetRanger III
fuselage length 9.50 m
  (31 ft 2 in)
rotor diam 10.16 m (33 ft 4 in)
engine 1 × Allison 250, 420 hp
max take-off weight 1451 kg (3200 lb)
max speed 224 km/h (139 mph)
capacity 5 persons
 
  BOEING – United States
William Boeing incorporated an aircraft factory in Seattle in 1916. In 1933 the company introduced its Boeing 247, the first airliner to have a modern metal construction. Boeing built mostly bombers during the 1940s and 1950s; then the revolutionary Boeing 707 jetliner gave it a leading position on the airliner market. Finally in 1997 Boeing took over its great rival, McDonnell Douglas.
 
C-135 Stratolifter/Stratotanker
FIRST FLIGHT 1956
The US Air Force's first jet-powered in-flight refuelling tanker, the KC-135 Stratotanker was developed directly from the Boeing 367-80 prototype which also led to the 707 airliner. Over 800 C-135s were built, small numbers serving as Stratolifter transport aircraft and in specialist roles such as electronic reconaissance. Re-engined , 450 aircraft remain in service, now all over 45 years old.
 
 
KC-135A
length 41.53 m (136 ft 3 in)
span 39.87 m (130 ft 10 in)
engine 4 × Pratt & Whitney J57, 4 × 6237 kg (13 750 lb) thrust
max take-off weight 134 717 kg (297 000 lb)
max speed 941 km/h (585 mph)
capacity 126 passengers
 
707 / 720
FIRST FLIGHT 1957
Though related to the military C-135, the 707 jetliner was given a slightly wider fuselage to accomodate six seats abreast . Early models, with thirsty, dirty and noisy JT3C turbojets, had limited range, but the type matured as the 707-300B Intercontinental, with JT3D turbofans. A better shorter-range variant was also built as the Boeing 720. Just over 1000 707s and 154 720s were constructed..
 
 
707-300B
length 46.61 m (152 ft 11 in)
span 44.42 m (145 ft 9 in)
engine 4 × Pratt & Whitney JT3D, 4 × 8618 kg (19 000 lb) thrust
max take-off weight 151 315 kg (333 600 lb)
max cruising speed 966 km/h (600 mph)
capacity 189 passengers
 
E-3 Sentry
FIRST FLIGHT 1972
Like the smaller C-135, the Boeing 707-300 is in military service as a tanker and transport aircraft with a number of nations. It also spawned some specialized military variants, including the E-3 Sentry or AWACS, an airborne air combat control station fitted with a powerful radar in a rotating saucer on its back. 68 E-3s were built, powered by either old TF33 (JT3D) or modern CFM56 turbofans.
 
 
E-3A
length 46.61 m (152 ft 11 in)
span 44.42 m (145 ft 9 in)
engine 4 × Pratt & Whitney TF33, 4 × 9525 kg (21 000 lb) thrust
max take-off weight 147 420 kg (325 000 lb)
max speed 853 km/h (530 mph)
capacity 17-23 persons
 
727
FIRST FLIGHT 1963
To complement the long-range Boeing 707 and replace its lighter Model 720 variant, Boeing designed a jetliner with the same fuselage width but three tail-mounted engines. The initial 727-100, seating 131 passengers, was followed by the stretched 727-200, and over 1800 examples of this major airliner were built. Production ended in 1984. The 727 remains in service with smaller operators, often fitted with noise-reducing modfications.
 
 
727-200
length 46.69 m (153 ft 2 in)
span 32.92 m (108 ft 0 in)
engine 3 × Pratt & Whitney JT8D, 3 × 7258 kg (16 000 lb) thrust
max take-off weight 95 030 kg (209 500 lb)
max cruising speed 953 km/h (592 mph)
capacity 189 passengers
 
737-100 / -200
FIRST FLIGHT 1967
Several years behind the BAC One-Eleven and DC-9, Boeing launched a 'baby Boeing' featuring the same fuselage width as the 707 and 727. The initial 737-100 model, accomodating from 100 to 115 passengers,
was quickly followed by the slightly stretched 737-200. Thirty 737-100s and just over 1000 737-200s were built.
 
 
737-200
length 30.48 m (100 ft 0 in)
span 28.30 m (93 ft 0 in)
engine 2 × Pratt & Whitney JT8D, 2 × 7258 kg (16 000 lb) thrust
max take-off weight 53 070 kg (117 000 lb)
max speed 876 km/h (544 mph)
capacity 115-130 passengers
 
737-300
FIRST FLIGHT 1984
The first of the second generation of 737s, the 737-300 introduced the new Franco-American CFM56 turbofan.
To ensure sufficient ground clearance, the engines were installed forward of, rather than below the wing, and the nacelles were flattened on the bottom, hence their oval shape. 1113 examples of the 737-300 were built. The 743-400 is a stretched and the -500 a shortened model.
 
 
737-300
length 33.40 m (109 ft 7 in)
span 28.90 m (94 ft 9 in)
engine 2 × CFM56, 2 × 9072 kg (20 000 lb) thrust
max take-off weight 61 236 kg (135 000 lb)
max speed 876 km/h (544 mph)
capacity 128-149 passengers
 
737-400
FIRST FLIGHT 1988
The 737-400 is a 737-300 derivative stretched by 1.8 m (6 ft) forward and 1.2 m (4 ft) aft of the wing, enabling it
to transport as many passengers as the old Boeing 727 at lower operating costs. A tail bumper guards against scraping the longer rear fuselage against the runway during take-off. Despite competition from Airbus' new A320, almost 500 examples of the 737-400 were built.
 
 
737-400
length 36.45 m (119 ft 7 in)
span 28.90 m (94 ft 9 in)
engine 2 × CFM56, 2 × 9979 kg (22 000 lb) thrust
max take-off weight 62 820 kg (138 500 lb)
max speed 876 km/h (544 mph)
capacity 146-188 passengers
 
737-500
FIRST FLIGHT 1989
The 737-500 is similar in size to the old 737-200, which it was intended to replace. Being based on the larger 737-300 it is in some respects heavier than necessary,
but this may be offset by standardization advantages for airlines operating several variants of the same aircraft. Production of the 737-500 model totalled 389 airframes.
 
 
737-500
length 31.01 m (101 ft 9 in)
span 28.90 m (94 ft 9 in)
engine 2 × CFM56, 2 × 8391 kg (18 500 lb) thrust
max take-off weight 52 390 kg (115 500 lb)
max speed 876 km/h (544 mph)
capacity 108-132 passengers
 
737-700
FIRST FLIGHT 1997
The third or Next Generation of 737s, with a completely new, larger wing, new tail surfaces, and a modernized cockpit, comes in four sizes as the 737-600, -700, -800 and -900; the 737-700 was the first to fly. Like its larger brothers, the -700 is often fitted with winglets to reduce fuel burn during cruise flight. Based on the -700 is the BBJ, which in turn spawned the long-range 737-700ER.
 
 
737-700
length 33.63 m (110 ft 4 in)
span 34.31 m (112 ft 7 in)
engine 2 × CFM56, 2 × 9344 kg (20 600 lb) thrust
max take-off weight 60 330 kg (133 000 lb)
max speed 876 km/h (544 mph)
capacity 126-149 passengers
 
BBJ
FIRST FLIGHT 1998
The Boeing Business Jet is an executive version of the 737-700, with intercontinental range thanks to powerful engines enabling extra fuel to be carried. Luxury options
include a bedroom, washroom with shower, and dining and conference room. The BBJ may also be configured as a 63-seat first-class airliner. If a BBJ is too cramped, the BBJ2 and BBJ3 are based on the 737-800 and -900.
 
 
BBJ
length 33.63 m (110 ft 4 in)
span 35.79 m (117 ft 5 in)
engine 2 × CFM56, 2 × 11 975 kg (26 400 lb) thrust
max take-off weight 77 560 kg (171 000 lb)
max speed 876 km/h (544 mph)
capacity 24-63 passengers
 
737-800
FIRST FLIGHT 1997
Six metres (19 ft) longer than the -700, the 737-800
carries some 40 extra passengers, and is the best- selling Next Generation model, with over 2000 orders. The 6000th Boeing 737 built, a 737-800, was delivered in 2009. Its business jet model is the BBJ2. The P-8 maritime patrol aircraft is being based on the 737-800.
 
 
737-800
length 39.47 m (129 ft 6 in)
span 34.31 m (112 ft 7 in)
engine 2 × CFM56, 2 × 10 977 kg (24 200 lb) thrust
max take-off weight 70 535 kg (155 500 lb)
max speed 876 km/h (544 mph)
capacity 162-189 passengers
 
737-600
FIRST FLIGHT 1998
The smallest member of the 737 Next Generation family, the 737-600 does not actually require the larger wing and tail surfaces, and like its Airbus counterpart, the A318, is relatively expensive to operate and unsuccesful.
69 aircraft have been delivered, 35 of which went to the launch customer, SAS, and there are no further orders.
 
 
737-600
length 31.24 m (102 ft 6 in)
span 34.31 m (112 ft 7 in)
engine 2 × CFM56, 2 × 8845 kg (19 500 lb) thrust
max take-off weight 56 245 kg (124 000 lb)
max speed 876 km/h (544 mph)
capacity 110-132 passengers
 
737-900
FIRST FLIGHT 2000
The 737-900 is probably the ultimate 737 in length. The original 737-900 does offer an increase in cabin space over the 737-800, but not in passenger capacity or gross weight, and only 50 aircraft were delivered. The-900ER, however, can seat up to 215 passengers, or over twice the number of the original 737. The -900ER version has winglets as standard. The BBJ3 is the executive version.
 
 
737-900ER
length 42.11 m (138 ft 2 in)
span 35.79 m (117 ft 5 in)
engine 2 × CFM56, 2 × 12 383 kg (27 300 lb) thrust
max take-off weight 85 139 kg (187 700 lb)
max speed 876 km/h (544 mph)
capacity 180-215 passengers
 
  BOMBARDIER – Canada
Joseph-Armand Bombardier was an inventor of snowmobiles. The Bombardier industrial group purchased Canadair in 1986. Bombardier Aerospace continues to construct Canadair aircraft, including the CRJ regional jet family. Bombardier has also taken over Short Brothers, Learjet and De Havilland Canada. A new jetliner, the CS100/C300, is under development.
 
BD-700 Global Express
FIRST FLIGHT 1996
Although using the same fuselage cross section as the CL-600 Challenger, the Global Express is a larger and faster, ultra-long-range business jet that can fly between any two points on the globe with just one refuelling stop. A military model carrying a battlefield monitoring radar system is now in British service, named Sentinel R.1.

 
 
Global Express XRS
length 30.30 m (99 ft 5 in)
span 28.65 m (94 ft 0 in)
engine 2 × Rolls-Royce BR710, 2 × 6690 kg (14 750 lb) thrust
max take-off weight 44 452 kg (98 000 lb)
max cruising speed 950 km/h (590 mph)
capacity 8-19 passengers
 
BD-700 Global 5000
FIRST FLIGHT 2003
A variant of the Global Express, the Global 5000 has its fuselage shortened by 0.8 m (2 ft 9 in) and has less fuel capacity in its tail and wings, thus reducing range with eight passengers to 8890 km (5523 miles), still plentiful
for Atlantic crossings. First deliveries took place in 2005.
 
 
Global 5000
length 29.49 m (96 ft 8 in)
span 28.65 m (94 ft 0 in)
engine 2 × Rolls-Royce BR710, 2 × 6690 kg (14 750 lb) thrust
max take-off weight 39 780 kg (87 700 lb)
max cruising speed 950 km/h (590 mph)
capacity 8-19 passengers
 
BD-100 Challenger 300
FIRST FLIGHT 2001
Bombardier's first all-new aircraft design, initially known as the Continental but renamed Challenger 300 in 2002, is intended to bridge the gap in the company's business jet range between the Learjet and the Challenger 600. It was designed to cover just under 5500 km (3418 miles) with eight people. 200 examples had been built by 2008.
 
 
Challenger 300
length 20.93 m (68 ft 8 in)
span 19.46 m (63 ft 10 in)
engine 2 × Honeywell AS907, 2 × 3096 kg (6825 lb) thrust
max take-off weight 17 622 kg (38 850 lb)
max cruising speed 870 km/h (541 mph)
capacity 8-15 passengers
 
  BRITTEN-NORMAN – United Kingdom
Britten-Norman is a small British aircraft company. It is based in Bembridge on the Isle of Wight.
 
BN-2 Islander
FIRST FLIGHT 1965
Designed by John Britten and Desmond Norman, the Islander is a short take-off and landing (STOL) light transport aircraft with fixed undercarriage, often used to provide air services to small islands. The cabin has no aisle but six doors instead. The Defender is a military version. The BN-2T Turbine Islander has Allison 250 turboprops, whereas the Trislander derivative has three piston engines, one of which is mounted on the tailfin.

 

 
BN-2B-20
length 10.86 m (35 ft 8 in)
span 14.94 m (49 ft 0 in)
engine 2 × Lycoming O-540, 2 × 300 hp
max take-off weight 2993 kg (6600 lb)
max speed 280 km/h (174 mph)
capacity 10 persons
 
  BÜCKER – Germany
A German naval pilot in World War I, Carl Bücker led the Swedish aircraft factory Svenska Aero during the 1920s. Taking his chief engineer, Anders Andersson, Bücker returned to Germany
to establish Bücker Flugzeugbau in 1933. Based in Berlin-Johannistal, and later in Rangsdorf,
the company created three renowned training aircraft. After the end of the war Bücker was dismantled by the Russians.
 
Bü 131 Jungmann
FIRST FLIGHT 1934
An elementary trainer designed by Andersson, the Jungmann (Junior) was soon adopted by the Luftwaffe.
When the Bestmann began to replace them with the flying schools, many Jungmanns were sent to the Eastern Front to serve as light nocturnal attack aircraft.
Bü 131s were also built in Switzerland, in Spain (as the C.1.31), in Japan (Ki-86/K9W), and in Czechoslovakia.

 

 
Bü 131B
length 6.60 m (21 ft 8 in)
span 7.40 m (24 ft 3 in)
engine 1 × Hirth HM 504, 105 hp
max take-off weight 680 kg (1499 lb)
max speed 183 km/h (114 mph)
capacity 2 persons
 
Bü 133 Jungmeister
FIRST FLIGHT 1935
A smaller, single-seat Jungmann derivative with a more powerful engine, the Jungmeister was a world-class aerobatic aircraft, but was built mainly as a single-seat advanced trainer for future fighter pilots. In the most important version, the Bü 133C, the Hirth inline engine was replaced by a Siemens radial. Switzerland and Spain each built some 50 Jungmeisters under licence.

 

 
Bü 133C
length 6.00 m (19 ft 8 in)
span 6.60 m (21 ft 8 in)
engine 1 × Siemens Sh 14, 160 hp
max take-off weight 585 kg (1290 lb)
max speed 220 km/h (137 mph)
capacity 1 person
 
Bü 181 Bestmann
FIRST FLIGHT 1939
To modernize elementary training, Andersson designed a monoplane with side-by-side seating, the Bestmann, which was put into production for the Luftwaffe at Bücker, Fokker in occupied Holland and Zlín in Czcechoslovakia, while It was licence-built in Sweden as the Sk 25. Zlín continued to manufacture it after the war, and Egypt acquired a Czech licence to build it as the Gomhouria.

 

 
Bü 181A
length 7.85 m (25 ft 9 in)
span 10.60 m (34 ft 9 in)
engine 1 × Hirth HM 504, 105 hp
max take-off weight 750 kg (1058 lb)
max speed 215 km/h (134 mph)
capacity 2 persons
 
  CANADAIR – Canada
Canadair's origins lie in a Canadian Vickers plant in Montreal. The firm proved adept in modifying other manufacturers' aircraft, but also produced some original designs. In 1986 it was bought
by Bombardier, although the Canadair brand remained in use for some time.
 
CL-41 Tutor
FIRST FLIGHT 1960
The Canadian variation on the 1960s basic jet trainer theme, the Tutor served in the Royal Canadian Air Force as the CT-114. Today it is still flown by the Snowbirds aerobatic team. In addition to 190 CL-41As for the RCAF, 20 CL-41G Tebuan (Wasp) aircraft with an uprated J85 engine and armament options were built for Malaysia.
 
 
CL-41A
length 9.75 m (32 ft 0 in)
span 11.13 m (36 ft 6 in)
engine 1 × General Electric J85, 1 × 1195 kg (2633 lb) thrust
max take-off weight 3 355 kg (7 397 lb)
max speed 801 km/h (498 mph)
capacity 2 persons
 
CL-215
FIRST FLIGHT 1967
Although it can also fly as a rescue or transport aircraft, the CL-215 amphibian flying boat is unique in having been designed as a water bomber, to extinguish (forest) fires. It can carry, and dump, 5346 litres (1176 Imp gal) of water and using retractable probes can scoop fresh loads from any nearby lake or sea, without the need to land. 125 CL-215s were built before the production line switched to the turboprop-powered variant, the CL-415.
 
 
CL-215
length 19.82 m (65 ft 0 in)
span 28.61 m (93 ft 10 in)
engine 2 × Pratt & Whitney R-2800 Double Wasp, 2 × 2100 hp
max take-off weight 19 731 kg (43 500 lb)
max cruising speed 291 km/h (181 mph)
capacity 8-26 passengers
 
CL-415
FIRST FLIGHT 1993
Essentially a CL-215 amphibian with modern turboprop engines, the CL-415 also features modernized systems, and can carry 6140 litres (1350 Imp gal) of water and fire-retarding chemicals. By 2007, 60 CL-415s were serving in Canada and Southern Europe. 17 CL-215s have been upgraded to a similar standard as CL-215Ts.
 
 
CL-215
length 19.82 m (65 ft 0 in)
span 28.61 m (93 ft 10 in)
engine 2 × Pratt & Whitney Canada PW123, 2 × 2380 hp
max take-off weight 19 890 kg (43 850 lb)
max speed 377 km/h (223 mph)
capacity 8-26 passengers
 
CL-600 Challenger
FIRST FLIGHT 1978
The LearStar 600 design by Bill Lear, of Learjet fame, was bought by Canadair and built, with a T-tail, as the CL-600 Challenger. It became a succesful business jet, especially after the original Lycoming ALF502 turbofans were replaced on the Challenger 601, which also got winglets. The 604 model has a new undercariage, and the 605 adds a new tailcone and larger cabin windows. The larger Challenger 850 is based on the CRJ200.
 
 
CL-600 Challenger 601
length 20.85 m (68 ft 5 in)
span 19.61 m (64 ft 4 in)
engine 2 × General Electric CF34, 2 × 4146 kg (9140 lb) thrust
max take-off weight 19 550 kg (43 100 lb)
max cruising speed 851 km/h (529 mph)
capacity 8-19 passengers
 
CRJ100 / -200
FIRST FLIGHT 1991
A stretched airliner variant of the CL-600 Challenger business jet, the Canadair Regional Jet was hugely succesful in a market segment previously dominated by turboprop aircraft. The CRJ200, with more efficient engines, supplanted the original CRJ100 model, the CRJ440 being a lighter version seating up to 44. Over 1000 of these aircraft have been built, but high fuel prices have turned the tide against the small jet again.
 
 
CL-600 CRJ100
length 26.77 m (87 ft 10 in)
span 21.21 m (69ft 7 in)
engine 2 × General Electric CF34, 2 × 4182 kg (9220 lb) thrust
max take-off weight 21 523 kg (47 450 lb)
max cruising speed 851km/h (529 mph)
capacity 50-52 passengers
 
CRJ700
FIRST FLIGHT 1999
The CRJ700 is a CRJ stretched and modified to carry 70 passengers - the cabin floor has also been lowered and the ceiling raised to provide increased headroom, and the increased-span wing has leading edge slats. There are three near-identical versions, the 700, 701 and 702, with up to 68, 70 and 78 seats, respectively. The CRJ705 is a variant of the even longer CRJ900.
 
 
CL-600 CRJ701
length 32.51 m (106 ft 8 in)
span 23.24 m (76 ft 3 in)
engine 2 × General Electric CF34, 2 × 5747 kg (12 670 lb) thrust
max take-off weight 32 995 kg (72 742 lb)
max cruising speed 876 km/h (544 mph)
capacity 70 passengers
 
CRJ900
FIRST FLIGHT 2001
A CRJ700 variant stretched by another 3.86 m (6 ft 8 in), the CRJ900 seats 86 passengers, or 90 with reduced room for baggage. A version seating 75 in a two-class configuration is designated CRJ705. Yet another stretch, the CRJ1000 100-seater, first flew in September 2008, in spite of the development of the Bombardier CS100.
 
 
CL-600 CRJ900
length 36.40 m (119 ft 4 in)
span 24.85 m (81 ft 6 in)
engine 2 × General Electric CF34, 2 × 6466 kg (14 255 lb) thrust
max take-off weight 36 514 kg (80 500 lb)
max cruising speed 881 km/h (547 mph)
capacity 80-90 passengers
 
  CESSNA – United States
Clyde Cessna, a farmer from Kansas, built his first aircraft in 1911, but not until after World War II did Wiichita-based Cessna Aircraft become a significant producer of light aircraft in particular. Cessna halted manufacture of all light propeller aircraft in 1985 due to product liability problems, but production of several light types resumed in its Indepencence, Kansas plant in the 1990s.
 
120 / 140
FIRST FLIGHT 1945
Immediately after Word War II Cessna produced a new two-seat aircraft for the private market, the 120, and a more luxurious variant, the 140. Although the wings were originally fabric-clad, the fuselage was a modern metal monocoque structure, maintainable and durable. This was the key to success: despite the availability of war surplus light aircraft, 7664 Model 120 / 140s were sold.

 

 
120 / 140
length 6.56 m (21 ft 6 in)
span 10.25 m (33 ft 4 in)
engine 1 × Continental C85, 85 hp
max take-off weight 658 kg (1450 lb)
max speed 203 km/h (125 mph)
capacity 2 persons
 
170
FIRST FLIGHT 1947
A larger, four-seat derivative of the Cessna 120 / 140, the initial 170 was soon supplanted by the improved 170A with metal-clad wings. In 1952 the refined 170B model introduced the O-1's wing dihedral and flaps. Over 5000 Cessna 170s were built until the introduction of the nosewheel gear 172, and many 170s are still airworthy.

 

 
170B
length 7.61 m (25 ft 0 in)
span 10.97 m (36 ft 0 in)
engine 1 × Continental O-300, 145 hp
max take-off weight 998 kg (2200 lb)
max speed 230 km/h (143 mph)
capacity 4 persons
 
O-1 Bird Dog
FIRST FLIGHT 1949
The durable metal construction of Cessna's light aircraft appealed to the US Army, and Cessna was selected to produce the L-19 (later O-1) liaison and observation aircraft. Some 3500 Bird Dogs were built, seeing action in Korea and later in Vietnam, where 469 were lost to all causes. SIAI-Marchetti's SM.1019 is an O-1 derivative.

 

 
O-1E
length 7.89 m (25 ft 10 in)
span 10.97 m (36 ft 0 in)
engine 1 × Continental O-470, 213 hp
max take-off weight 1090 kg (2400 lb)
max speed 184 km/h (115 mph)
capacity 2 persons
 
180 / 185 Skywagon
FIRST FLIGHT 1952
Initially just a Cessna 170 with a more powerful engine, the 180 was later built as a six-seater with a third side window, the 185 model being identical except for a still more powerful engine and a larger tailfin. The U-17 military version of the 185 was supplied to several countries. Over 10 000 Skywagons were produced.

 

 
180G
length 7.77 m (25 ft 6 in)
span 11.02 m (36 ft 2 in)
engine 1 × Continental O-470, 230 hp
max take-off weight 1270 kg (2800 lb)
max speed 273 km/h (170 mph)
capacity 6 persons
 
310
FIRST FLIGHT 1953
The first twin-engined Cessna to be put into production after World War II, the sleek, modern-looking 310 seated five to six people. 6300 examples were built in 26 years, mainly as air taxis and light corporate aircraft, including Model 320 Skynights which had supercharged engines, as did the later T310 version. US military Model 310s were designated U-3s, and nicknamed Blue Canoes.

 

 
310R
length 9.74 m (32 ft 0 in)
span 11.25 m (36 ft 11 in)
engine 2 × Continental O-520, 2 × 285 hp
max take-off weight 2495 kg (5500 lb)
max speed 383 km/h (238 mph)
capacity 6 persons
 
172 Skyhawk
FIRST FLIGHT 1955
The most-produced aircraft ever, with over 40 000 built, the Cessna 172 was developed from the tailwheel 170 and initially had no window aft of the cabin and a square tailfin. F172 models were built at Reims in France. The Cessna 175 Skylark, FR172 Rocket, R172 Hawk XP, and 172Q Cutlass variants had more powerful engines. The T-41 Mescalero was a military trainer. Production resumed in 1996 with the new 172R and S versions.

 

 
172N Skyhawk
length 8.21 m (26 ft 11 in)
span 10.92 m (35 ft 10 in)
engine 1 × Lycoming O-320, 160 hp
max take-off weight 1043 kg (2300 lb)
max speed 232 km/h (144 mph)
capacity 4 persons
 
172 Cutlass RG
FIRST FLIGHT 1979
The 172RG or Cutlass RG is a Cessna 172 utilizing the retractable gear of the 182 Skylane RG, the main wheels retracting backwards into the fuselage. The Cutlass RG was not very popular by Cessna standards; some 1200 examples were built, and production was not resumed in the 1990s. 172RGs are often used as training aircraft.

 

 
172RG Cutlass
length 8.36 m (27 ft 5 in)
span 10.92 m (35 ft 10 in)
engine 1 × Lycoming O-360, 180 hp
max take-off weight 1202 kg (2650 lb)
max speed 267 km/u (166 mph)
capacity 4 persons
 
182 Skylane
FIRST FLIGHT 1956
The Cessna 182 was developed from the tailwheel 180. Compared to the 172 it's a faster four-seater with more room for luggage or two additional child's seats. Like the 172, the 182 initally had no aft window and a non-swept tailfin, was licence-built at Reims (as the F182), was also built with retractable landing gear (as the R182 Skylane RG) and was returned to production in 1996.

 

 
182T
length 8.84 m (29 ft 0 in)
span 10.97 m (36 ft 0 in)
engine 1 × Lycoming O-540, 230 hp
max take-off weight 1406 kg (3100 lb)
max speed 278 km/h (173 mph)
capacity 4 persons
 
150
FIRST FLIGHT 1957
The successor to the Cessna 140, the 150 two-seat private and training aicraft entered production in 1958. The 150D model introduced a cut-back rear fuselage coupled with a window aft of the cabin, which proved popular despite a slight decrease in performance. The facelift was completed with a swept tailfin on the 150F.

 

 
150B
length 6.55 m (21 ft 6 in)
span 10.16 m (33 ft 4 in)
engine 1 × Continental O-200, 100 hp
max take-off weight 680 kg (1500 lb)
max speed 204 km/h (127 mph)
capacity 2 persons
 
150F / 152
FIRST FLIGHT 1965
Starting with the F model the Cessna 150 was produced with both a rear window and a swept tailfin, and built also by Reims in France as the F150. From 1977 the 152 model, powered by a Lycoming O-235 engine, was built. Over 30 000 Cesnna 150 / 152s were produced, including the early models and 2347 F150 / F152s.

 

 
150M
length 7.29 m (23 ft 11 in)
span 10.11 m (33 ft 2 in)
engine 1 × Continental O-200, 100 hp
max take-off weight 726 kg (1600 lb)
max speed 201 km/h (125 mph)
capacity 2 persons
 
210 Centurion
FIRST FLIGHT 1957
The Cessna 210 originated as an early retractable gear variant of the 182, as illustrated, but in 1967 the 210G introduced a new, cantilever wing - without struts - and from the 210K model onwards six adults can be carried. T210s featrure a turbocharged engine and P210s also have a pressurized cabin. 9240 Centurions were built.

 

 
210L Centurion II
length 8.59 m (28 ft 2 in)
span 11.15 m (36 ft 9 in)
engine 1 × Lycoming O-520, 300 hp
max take-off weight 1725 kg (3800 lb)
max speed 324 km/h (201 mph)
capacity 6 persons
 
205
FIRST FLIGHT 1962
The Cessna 205 was developed from the 210, reverting to a fixed underrcarriage and seating six adults or more luggage. A sizeable door was provided in the rear left side of the cabin. The 205 was soon supplanted by the more powerful 206, and the type remained in production for only two years. 576 Cessna 205s were constructed.

 

 
205
length 8.46 m (27 ft 9 in)
span 11.15 m (36 ft 7 in)
engine 1 × Continental O-470, 260 hp
max take-off weight 1497 kg (3300 lb)
max speed 278 km/u (172 mph)
capacity 6 persons
 
206
FIRST FLIGHT 1964
Developed from the Cessna 205, the206 came in two models, the passenger P206 Super Skylane and the rear cargo door-equipped U206 Super Skywagon, later renamed Stationair. In 1998 the Stationair re-entered production as the 206H. Turbocharged versions are designated TP206, TU206 and T206H. An Allison 250 turbine engine powers the converted Soloy Turbine 206.

 

 
206H Stationair
length 8.62 m (28 ft 3 in)
span 10.92 m (35 ft 10 in)
engine 1 × Lycoming O-540, 300 hp
max take-off weight 1640 kg (3614 lb)
max speed 285 km/h (177 mph)
capacity 6 persons
 
207
FIRST FLIGHT 1968
First flown on 11 May 1968, the Cessna 207 is a 206 stretched by 1 m (3 ft) to seat seven occupants, or eight in the case of the 207A Stationair 8 model, which was introduced in 1980. T207 versions have a turbocharged piston engine. The Soloy corporation provides a turbine engine conversion option for the 207 as well as the 206.

 

 
207A Stationair 8
length 9.68 m (32 ft 9 in)
span 10.92 m (35 ft 10 in)
engine 1 × Continental O-520, 300 hp
max take-off weight 1640 kg (3614 lb)
max speed 278 km/h (173 mph)
capacity 8 persons
 
411 / 401 / 402
FIRST FLIGHT 1962
Larger than the Cessna 310, the 411 seats four or six people in its cabin and two up front. It was in production until 1978, but from 1965 it was joined by two cheaper, simplified variants, the 401 and 402. The 402 transports up to nine passengers in its Utiliner form, or up to seven in the Businessliner layout. 402s built from 1972 have five rectangular cabin windows replacing four oval ones. 2237 examples of the 411 / 401 / 402 were constructed.

 

 
402C
length 11.09 m (36 ft 5 in)
span 13.45 m (44 ft 2 in)
engine 2 × Continental O-520, 2 × 325 hp
max take-off weight 3107 kg (6850 lb)
max speed 428 km/h (266 mph)
capacity 6-10 persons
 
208
FIRST FLIGHT 1982
Larger than Cessna's previous single-engined propeller aircraft, the 208 Caravan I can carry 14 passengers, although it is normally certified to carry only nine. A cargo version, the 208A Cargomaster was built for the FedEx courier company. The Caravan 675 is powered by the 675 hp engine first introduced on the stretched 208B.

 

 
208 Caravan I
length 11.46 m (37 ft 7 in)
span 15.88 m (52 ft 1 in)
engine 1 × Pratt & Whitney Canada PT6, 600 hp
max take-off weight 3310 kg (7300 lb)
max cruising speed 340 km/h (211 mph)
capacity 9-14 passengers
 
208B
FIRST FLIGHT 1986
A Cessna 208 stretched by 1.20 m (4 ft), the 208B was originally developed as a cargo aircraft for the FedEx company, named Super Cargomaster. FedEx owns a
fleet of some 250 Super Cargomasters. A passenger variant named Grand Caravan was introduced in 1990, and it is certified to carry 14 passengers as standard.

 

 
208B Grand Caravan
length 12.67 m (41 ft 7 in)
span 15.88 m (52 ft 1 in)
engine 1 × Pratt & Whitney Canada PT6, 675 hp
max take-off weight 3970 kg (8750 lb)
max cruising speed 317 km/h (197 mph)
capacity 14 passengers
 
  DASSAULT – France
French aircraft constructor Marcel Bloch refused to work for the Germans during World War II, and being a Jew, was sent to Buchenwald concentration camp, which he survived. He changed his name to Dassault, his brother Paul's pseudonym in the Resistance; a name now synonymous with French jet fighters and a succesful series of business jets. In 1971 Dassault purchased Breguet. Assembly of Dassault aircraft takes place at Bordeaux-Mérignac airport.
 
Flamant
FIRST FLIGHT 1947
Dassault's first post-war aircraft, the Flamant (Flamingo) was built in three versions for the French armed forces: the MD.311 bombing and navigation trainer, featuring a glazed nose; the MD.312 liaison aircraft and multi-engine pilot trainer; and the MD.315 light transport and ambulance for colonial use. Some 320 Flamants were produced, the last example retiring from service in 1982.

 

 
MD.315
length 12.50 m (41 ft 0 in)
span 20.68 m (67 ft 10 in)
engine 2 × Renault 12, 2 × 580 hp
max take-off weight 6400 kg (14 110 lb)
max speed 300 km/h (190 mph)
capacity 12 persons
 
Ouragan
FIRST FLIGHT 1949
The Ouragan (Hurricane) was France's first jet fighter and though a relatively straightforward, straight-winged aircraft, it was adopted by the air forces of France, India and Israel, the Israeli aircraft seeing combat particularly in the 1956 Suez War. 18 were sold to El Salvador, and were involved in that country's civil war during the 1980s.
 
 
MD.450B Ouragan
length 10.73 m (35 ft 2 in)
span 13.16 m (43 ft 2 in)
engine 1 × Rolls-Royce Nene, 2268 kg (5000 lb) thrust
max take-off weight 7900 kg (17 416 lb)
max speed 940 km/h (584 mph)
capacity 1 person
 
Mystère II
FIRST FLIGHT 1951
Essentially a swept-winged Ouragan, the Mystère was the first French aircraft to exceed the speed of sound in
a dive. Mystère I and II prototypes were followed by 160 Mystère IIC fighters, but they were quickly superseded by the more advanced Mystère IV. The Mystère IIIN two-seat night fighter derivative was built only in prototype form.
 
 
MD.452 Mystère IIC
length 12.25 m (40 ft 2 in)
span 11.32 m (37 ft 2 in)
engine 1 × Snecma Atar 101, 2950 kg (6504 lb) thrust
max take-off weight 8570 kg (18 894 lb)
max speed 1030 km/h (640 mph)
capacity 1 person
 
Mystère IV
FIRST FLIGHT 1952
Following on the heels of the Mystère, the Mystère IVA was a fresh, more advanced design, powered by the Rolls-Rocye Tay engine or its French-built version, the Verdon. Over 400 Mystère IVAs were built, including 60 exported to Israel and over 100 to India, these seeing action in four wars. The Mystère IVB with afterburning engine and IVN night fighter remained prototypes only.
 
 
MD.454 Mystère IVA
length 12.89 m (42 ft 4 in)
span 11.12 m (36 ft 6 in)
engine 1 × Hispano-Suiza Verdon, 3500 kg (7716 lb) thrust
max take-off weight 8210 kg (18 100 lb)
max speed 1110 km/h (690 mph)
capacity 1 person
 
Super Mystère
FIRST FLIGHT 1955
Fitted with a new, thin wing with 45 degrees of sweep, the prototype Super Mystère was the first West European aircraft to exceed the speed of sound in level flight, thus equalling the F-100 and MiG-19. 180 Super Mystère B2 production aircraft were built, 36 of which went to Israel. Sold to Honduras, the last of these were retired in 1989. The Super Mystère B4 reached Mach 1.4 in 1959, but this variant was abandoned in favour of the Mirage III.
 
 
Super Mystère B2
length 14.04 m (46 ft 1 in)
span 10.50 m (34 ft 6 in)
engine 1 × Snecma Atar 101, 4500 kg (9920 lb) thrust
max take-off weight 10 000 kg (22 0460 lb)
max speed 1200 km/h (743 mph)
capacity 1 person
 
Mirage III
FIRST FLIGHT 1956
Developed from the lightweight MD.550 Mystère-Delta, or Mirage I, the Mirage III was Western Europe's first Mach 2-capable aircraft, and the Mirage IIIC interceptor fighter was ordered by France, South Africa, and Israel, its success in the 1967 Six Day War making the Mirage famous. The Mirage IIIB is the two-seat trainer version.
 
 
Mirage IIIC
length 14.73 m (48 ft 4 in)
span 8.22 m (27 ft 0 in)
engine 1 × Snecma Atar 9, 1 × 6000 kg (13 225 lb) thrust
max take-off weight 9727 kg (21 444 lb)
max speed Mach 2.2 (2350 km/h / 1460 mph)
capacity 1 person
 
Mirage IIIE / 5
FIRST FLIGHT 1962
The Mirage IIIE is a heavier, fighter-bomber variant of the IIIC, versions including the IIIR reconnaissance aircraft. The simplified Mirage 5 carries no radar, but heavier loads. When its delivery to Israel was blocked by Paris, Israel built a Mirage clone, the Nesher, and the Kfir, with a US J79 engine. Like the Kfir, some III/5 versions have later been fitted with canard foreplanes. These include the Swiss IIIS and Chile's Atar 9K-powered Mirage 50.
 
 
Mirage IIIE
length 15.03 m (49 ft 4 in)
span 8.22 m (27 ft 0 in)
engine 1 × Snecma Atar 9, 1 × 6200 kg (13 670 lb) thrust
max take-off weight 12 000 kg (26 455 lb)
max speed Mach 2.2 (2350 km/h / 1460 mph)
capacity 1 person
 
Mirage IIIV
FIRST FLIGHT 1965
Worries about the vulnerability of runways in the 1960s aroused an interest in jet fighters with vertical take-off and landing (VTOL) capability. In France, the Balzac test aircraft was developed into the Mirage IIIV, although with its battery of eight separate lift engines - a heavy burden in normal flight - this was never going to be a practical combat aircraft. Only two prototypes of the IIIV were built.
 
 
Mirage IIIV-02
length 18.00 m (59 ft 1 in)
span 8.72 m (28 ft 7 in)
engine 1 × Pratt & Whitney TF30, 1 × 8400 kg (18 519 lb) thrust
  8 × Rolls-Royce RB.162, 8 × 2200 kg (4850) lb thrust
max take-off weight 13 440 kg (29 630 lb)
max speed Mach 2.0 (2125 km/h / 1320 mph)
capacity 1 person
 
Mirage IV
FIRST FLIGHT 1959
A twin-engined extrapolation of the Mirage fighters, the Mirage IV constituted a relatively cheap solution to give France a strategic jet bomber. 62 Mirage IVAs were built.
Due to their limited range, the planned nuclear strikes against Russia required aerial refuelling by France's
C-135s or 'buddy' Mirage IVs, and allegedly, missions with no return. The modernized Mirage IVP remained
in use as a strategic reconnaissance aircraft until 2005.
 
 
Mirage IVA
length 23.49 m (77 ft 1 in)
span 11.85 m (38 ft 11 in)
engine 2 × Snecma Atar 9K, 2 × 7000 kg (15 432 lb) thrust
max take-off weight 33 475 kg (73 800 lb)
max speed Mach 2.2 (2350 km/h / 1460 mph)
capacity 2 persons
 
Mirage F1
FIRST FLIGHT 1966
The Mirages' tailless delta wings caused high drag and poor controllability at low speeds and altitudes, and a swept wing was adopted for the two-seat Mirage F2 and the smaller F1, which was selected. Over 700 F1s were built for France and export customers including Iraq, Libya and South Africa. Variants are the F1C fighter, F1B trainer, F1A and E fighter-bombers and F1CR photo- recce aircraft. The F1CT fighter-bombers are converted F1Cs. A Snecma M53-powered version failed to sell.
 
 
Mirage F1C
length 15.30 m (50 ft 2 in)
span 8.40 m (27 ft 7 in)
engine 1 × Snecma Atar 9K, 1 × 7200 kg (15 873 lb) thrust
max take-off weight 16 200 kg (35 715 lb)
max speed Mach 2.2 (2350 km/h / 1460 mph)
capacity 1 person
 
Mercure
FIRST FLIGHT 1971
Larger than the Boeing 737 but powered by the same JT8D engines, Dassault's Mercure jetliner turned into a commercial disaster, due mainly to its limited range of 1700 km (1056 miles). Ordered only by French domestic airline Air Inter, which bought ten, the Mercure gave faithful service until 1995. The propopsed Mercure 200 development, to be powered by CFM56 engines, would have looked remarkably like the succesful Airbus A320.
 
 
Mercure
length 34.84 m (114 ft 3 in)
span 30.55 m (100 ft 3 in)
engine 2 × Pratt & Whitney JT8D, 2 × 7031 kg (15 500 lb) thrust
max take-off weight 56 500 kg (124 560 lb)
max cruising speed 870 km/h (540 mph)
capacity 150-162 passengers
 
Falcon 20 / 200
FIRST FLIGHT 1963
Resulting from of a joint study by Dassault and Sud, the succesful Mystère 20 business jet was renamed Falcon by its US distributor, Pan Am, and this name stuck. The improved Falcon 20H, powered by Garrett ATF3 engines, was renamed Falcon 200. Over 500 Falcon 20 / 200s were built, including the HU-25 Guardian and Gardian maritime patrol aircraft. Military Falcons also perform VIP transport, special training and electronic warfare duties.
 
 
Falcon 20F
length 17.15 m (56 ft 3 in)
span 16.32 m (53 ft 7 in)
engine 2 × General Electric CF700, 2 × 2041 kg (4500 lb) thrust
max take-off weight 13 000 kg (28 660 lb)
max cruising speed 863 km/h (536 mph)
capacity 8-14 passengers
 
Falcon 10 / 100
FIRST FLIGHT 1970
The second and smallest of the Falcon business jets, the Falcon 10 was a new design. 226 Falcon 10s and 100s were built between 1973 and 1990, the Falcon 100 model incorporating small improvements. Seven of the Falcon 10s, known as Falcon 10MERs, were delivered to the French Navy for training and light transport roles.
 
 
Falcon 10
length 13.86 m (45 ft 6 in)
span 13.08 m (42 ft 11 in)
engine 2 × Honeywell TFE731, 2 × 1465 kg (3230 lb)
take-off weight 8500 kg (18 740 lb)
max speed 912 km/h (566 mph)
capacity 4-7 passengers
 
Falcon 50
FIRST FLIGHT 1976
The Falcon 50 uses the front fuselage of the Falcon 20, but is a heavier aircraft with transatlantic range, featuring a new wing and three engines in a new rear fuselage. Although having two larger engines is theoretically more efficient, having three is theoretically safer during take-off and long overwater flights. First flown in 1996, the 50EX model has even longer range and a modernized cockpit.
 
 
Falcon 50
length 18.50 m (60 ft 8 in)
span 18.85 m (61 ft 11 in)
engine 3 × Honeywell TFE731, 3 × 1678 kg (3700 lb) thrust
max take-off weight 17 600 kg (38 800 lb)
max cruising speed 880 km/h (547 mph)
capacity 8-19 passengers
 
Falcon 900
FIRST FLIGHT 1984
The Falcon 900 mated the wing of the Falcon 50, with a slightly increased span, to a new fuselage with a larger cross-section, to compete with the Gulfstream IV at the high end of the business jet market. Several versions exist, including the Falcon 900EX, which has a range of over 8,000 km (4971 miles) carrying eight passengers.
 
 
Falcon 900EX
length 20.21 m (66 ft 4 in)
span 19.33 m (63 ft 5 in)
engine 3 × Honeywell TFE731, 3 × 2155 kg (4750 lb) thrust
max take-off weight 20 640 kg (45 500 lb)
max cruising speed 927 km/h (576 mph)
capacity 8-18 passengers
 
Falcon 2000
FIRST FLIGHT 1993
A lighter variant of the Falcon 900, with a shorter cabin and shorter range, the Falcon 2000 reverts to a twin- engined layout, and with its redesigned rear fuselage is actually slightly longer for aerodynamic reasons. The latest versions, the Falcon 2000EX and -DX, are fitted with more powerful Pratt & Whitney PW308 engines.
 
 
Falcon 2000
length 20.23 m (66 ft 5 in)
span 19.33 m (63 ft 5 in)
engine 2 × CFE 7381, 2 × 2597 kg (5725 lb) thrust
max take-off weight 16 238 kg (35 800 lb)
max cruising speed 891 km/h (554 mph)
capacity 8-12 passengers
 
Falcon 7X
FIRST FLIGHT 2005
Taking over as the flagship of the Falcon business jet range, the 7X retains the three-engined layout and the fuselage diameter of its predecessor, the Falcon 900, but is a new, advanced design. The Falcon 7X's range is 11 000 km ( 6835 miles) at a 900 km/h (559 mph) cruise speed, at a high altutidue, in non-congested airspace.
 
 
Falcon 7X
length 23.19 m (76 ft 1 in)
span 26.21 m (86 ft 0 in)
engine 3 × Pratt & Whitney Canada PW307,
   3 × 2903 kg (6400 lb) thrust
max take-off weight 31 751 kg (70 000 lb)
max cruising speed 953 km/h (593 mph)
capacity 8-19 passengers
 
  DASSAULT / DORNIER – France / Germany  
Alpha Jet
FIRST FLIGHT 1973
With the Franco-British Jaguar ending up too heavy and expensive for use as a training aircraft, France undertook to build a new basic and andvanced trainer with Germany, which decided to put it into use as a light attack aircraft, however. Each country ordered 175, and 130 more Alpha Jets were produced for other nations.
 
 
Alpha Jet E
length 12.29 m (40 ft 3 in)
span 9.11 m (29 ft 11 in)
engine 2 × Snecma / Turboméca Larzac,
   2 × 1345 kg (2960 lb) thrust
max take-off weight 7250 kg (15 983 lb)
max speed 1020 km/h (633 mph)
capacity 2 persons
 
  DE HAVILLAND CANADA Canada
DHC was founded at Toronto-Downsview in 1928 as subsidiary of the British De Havilland firm. After building the DH.98 Mosquito during World War II, DHC started producing its own designs, specializing in rugged transport aircraft. DHC has been absorbed by Bombardier; Canadian company Viking Air bought the manufacturing rights for the DHC-1 through DHC-7.
 
DHC-1 Chipmunk
FIRST FLIGHT 1946
Created by former PZL designer Wsiewolod Jakimiuk , the Chipmunk was a succesful elementary trainer, replacing the DH.82 Tiger Moth not only in the Canadian Air Force, but also in the British RAF, and 1000 of the 1230 aircraft built were turned out by the British DH works. Hundreds are kept airworthy by private pilots.

 

 
Chipmunk T.10
length 7.75 m (25 ft 5 in)
span 10.46 m (34 ft 4 in)
engine 1 × De Havilland Gypsy Major, 145 hp
max take-off weight 953 kg (2100 lb)
max speed 222 km/h (138 mph)
capacity 2 persons
 
DHC-2 Beaver
FIRST FLIGHT 1947
Rugged and practical, the DHC-2 light transport aircraft excels in wilderness areas, operated on wheels, floats or skis. Out of 1657 produced, almost 1000 went to the US military under the L-20 and U-6 designations. Today these old aircraft are much sought after, turboprops sometimes replacing their antiquated Wasp radials.

 

 
DHC-2
length 9.24 m (30 ft 4 in)
span 14.64 m (48 ft 0 in)
engine 1 × Pratt & Whitney R-985 Wasp Junior, 450 hp
max take-off weight 2313 kg (5100 lb)
max speed 225 km/h (140 mph)
capacity 8 persons
 
DHC-3 Otter
FIRST FLIGHT 1951
An extrapolation of the DHC-2 formula, the DHC-3 Otter carries about ten people. Some 460 Otters were built, including 184 for the US Army as U-1s. The Wasp radial engine is sometimes replaced by a Polish PZL radial or a turboprop engine. Illustrated is a floatplane version powered by a PT6 turbine engine in a lengthened nose.

 

 
DHC-3
length 12.80 m (41 ft 10 in)
span 17.69 m (58 ft 0 in)
engine 1 × Pratt & Whitney R-1340 Wasp, 600 hp
max take-off weight 3629 kg (8000 lb)
max speed 257 km/h (160 mph)
capacity 12 persons
 
DHC-4 Caribou
FIRST FLIGHT 1958
A short take-off and landing (STOL) military transport aircraft, the DHC-4 was first ordered by the US Army and used in Vietnam. The US Army aircraft were transferred to the US Air Force as C-7s. Other nations also operated Caribous; 307 were built. Along the same lines, DHC developed the DHC-5 Buffalo with T64 turbine engines and a T-tail, 122 examples of which were produced.

 

 
DHC-4A
length 22.13 m (72 ft 7 in)
span 29.15 m (95 ft 8 in)
engine 2 × Pratt & Whitney R-2000, 2 × 1450 hp
max take-off weight 12 928 kg (28 500 lb)
max speed 347 km/h (216 mph)
capacity 32 passengers
 
DHC-6 Twin Otter
FIRST FLIGHT 1965
Widely used as a 19-seat regional airliner and light transport aircraft, the 'Twotter' is, like its predecessors, a rugged short take-off and landing (STOL) machine. The landing gear is fixed and a floats and skis can be fitted. DHC-6 production ceased in 1988 after 844 aircraft, but there's nothing to replace the type. Viking Air has flown an upgraded aircraft, and intends to restart production.

 

 
DHC-6-300
length 15.77 m (51 ft 9 in)
span 19.81 m (65 ft 0 in)
engine 2 × Pratt & Whitney Canada PT6, 2 × 620 hp
max take-off weight 5670 kg (12 500 lb)
max cruising speed 338 km/h (210 mph)
capacity 20 passengers
 
DHC-7 Dash 7
FIRST FLIGHT 1975
A dedicated 50-seat airliner possessing the formidable short take-off and landing (STOL) of earlier DHC aircraft, the DHC-7 filled a small niche in the market, and with four engines is relatively expensive to run. Consequently only 113 Dash 7s were built, production ending in 1988.

 

 
DHC-7-100
length 24.58 m (80 ft 8 in)
span 28.35 m (93 ft 0 in)
engine 4 × Pratt & Whitney Canada PT6, 4 × 1120 hp
max take-off weight 19 731 kg (43 500 lb)
max cruising speed 426 km/h (265 mph)
capacity 50 passengers
 
DHC-8 Dash 8
FIRST FLIGHT 1983
In a departure from previous DHC designs, the DHC-8 regional airliner was built for efficiency in cruise rather than handling austere airstrips. The initial Dash 8-100 was followed by the -200, with more powerful PW123 engines. These also power the -300, which incorporates a 3.43 m (11 ft 3 in) stretch to seat 50 passengers. 660 aircraft of these versions were built, including the -Q200 and -Q300 models, which are equipped with a propeller
noise and vibration suppresion system for the cabin.

 

 
DHC-8-100
length 22.25 m (73 ft 0 in)
span 25.91 m (85 ft 0 in)
engine 2 × Pratt & Whitney Canada PW120, 2 × 1800 hp
max take-off weight 14 968 kg (33 000 lb)
max cruising speed 497 km/h (309 mph)
capacity 36-40 passengers
 
DHC-8-Q400 Dash 8
FIRST FLIGHT 1998
One and a half times as long and twice as heavy as the original DHC-8-100, and fitted with much more powerful engines driving six-blade propellers, the Dash 8-Q400 carries twice as many passengers at greater speed, to compete with jets over short distances. A further stretch to accommodate 90 passengers is under consideration.

 

 
DHC-8-Q400
length 32.84 m (107 ft 9 in)
span 28.42 m (93 ft 3 in)
engine 2 × Pratt & Whitney Canada PW150, 2 × 4850 hp
max take-off weight 29 260 kg (64 500 lb)
max cruising speed 648 km/h (403 mph)
capacity 70-78 passengers
 
  DORNIER – Germany
In 1914 Claude Dornier (1884-1969) , the son of a French wine importer and his German wife, was put in charge of the Zeppelin company's aeroplane division in Friedrichshafen, which he took over in the early 1920s. His aircraft included the enormous Do flying boat. After World War II Dornier built light transport aircraft. It was taken over by Fairchild in 1996, but Fairchild Dornier collapsed in 2002, having run out of money for its Fairchild Dornier 728 jetliner, which was built, but never flown.
 
Do 24
FIRST FLIGHT 1937
Praised for its seaworthiness, the three-engined Do 24 was designed as a patrol flying boat for the Netherlands Navy in the Indonesian archipelago, but was also used by the Luftwaffe as a rescue aircraft. 279 were produced, mainly in occupied Holland and France. A few supplied to Spain served into the 1970s. One of these has been rebuilt as a Do 24TT, with a new wing and PT6 engines.

 

 
Do 24T
length 21.95 m (72 ft10 in)
span 27.00 m (88 ft 7 in)
engine 3 × Bramo 323, 3 × 1000 hp
max take-off weight 18 400 kg (40 565 lb)
max speed 340 km/h (211 mph)
capacity 4-6 persons
 
Do 27
FIRST FLIGHT 1955
Working in Spain to avoid a ban on aircraft construction in Germany, Claude Dornier designed the Do 25 short take-off and landing (STOL) light transport aircraft, which was put into production as the Do 27 or CASA C.127 for Franco's air force. Production also started at Dornier's reopened Oberpfaffenhofen plant for the new Luftwaffe and other customers. Some 600 Do 27s were built.

 

 
Do 27Q-5
length 9.60 m (31 ft 6 in)
span 12.00 m (39 ft 5 in)
engine 1 × Lycoming O-480, 270 hp
max take-off weight 1848 kg (4070 lb)
max speed 232 km/h (144 mph)
capacity 6-8 passengers
 
Do 29
FIRST FLIGHT 1958
Derived from the Do 27, the Do 28 was an experimental vertical take-off and landing (VTOL) aircraft with two engines driving pusher propellers that could swivel through 90 degrees. The two Do 29s constructed were utilized for research in support of the Do 31, a very different, larger, jet-powered VTOL transport aircraft.

 

 
Do 29
length 9.50 m (31 ft 2 in)
span 13.20 m (43 ft 4 in)
engine 2 × Lycoming O-480, 2 × 270 hp
max take-off weight 2500 kg (5512 lb)
max speed 230 km/h (143 mph)
capacity 1 person
 
Do 28
FIRST FLIGHT 1959
A Do 27 development, the Do 28 featured two engines mounted on a stub wing on both sides of the cockpit. Like its single-engined forebear, the Do 28 was a good, rugged STOL aircraft, and 120 examples were built. However, it offered no increase in cabin space, and was superseded by the wholly new Do 28D Skyservant.

 

 
Do 28B-1
length 9.00 m (29 ft 6 in)
span 13.80 m (45 ft 3 in)
engine 2 × Lycoming O-540, 2 × 290 hp
max take-off weight 2720 kg (5996 lb)
max speed 302 km/h (188 mph)
capacity 6-8 persons
 
Do 28D Skyservant
FIRST FLIGHT 1966
Though posessing excellent STOL capabilities like the Do 28, the Do 28D is a larger, more angular and wholly different aircraft, despite its designation. Some 150 were built, mostly as light transports for the German Air Force and Navy. A few were fitted with turboprop propulsion, those with PT6 engines being designated Do 128-6.

 

 
Do 28D-2
length 11.60 m (38 ft 1 in)
span 15.55 m (51 ft 0 in)
engine 2 × Lycoming O-540, 2 × 380 hp
max take-off weight 4015 kg (8853 lb)
max speed 325 km/h (202 mph)
capacity 14 persons
 
Do 228
FIRST FLIGHT 1981
Larger again than the Do 28D and powered by turboprop engines, the Do 228 was intended to be a true airliner as well as a transport aircraft, seating 15 passengers in its Do 228-100 form and 19 in its stretched -200 form. German production ceased in 1998 after 250 aircraft, but licence production at HAL in India continued. A new German assembly line using Indian parts is planned, focussing on maritime surveillance and similar roles.

 

 
Do 228-200
length 16.56 m (54 ft 3 in)
span 16.97 m (55 ft 7 in)
engine 2 × Garrett TPE331, 2 × 715 hp
max take-off weight 5700 kg (12 570 lb)
max speed 434 km/h (271 mph)
capacity 19 passengers
 
Do 328
FIRST FLIGHT 1991
The Do 328 was designed as a fast regional airliner,
comfortably seating 30 passengers three-abreast, or seating 39 four-abreast. Despite good characteristics the Do 328 had a difficult time breaking into a crowded market that was looking for even faster regional jet aircraft. Production ceased in 1999 after 112 examples, in favour of the Dornier 328JET jet-powered derivative.

 

 
Do 328-110
length 21.28 m (69 ft 10 in)
span 20.98 m (68 ft 10 in)
engine 2 × Pratt & Whitney Canada PW119B, 2 × 2180 hp
max take-off weight 13 990 kg (30 842 lb)
max cruising speed 620 km/h (385 mph)
capacity 30-39 passengers
 
328JET
FIRST FLIGHT 1998
Regional airlines frowned upon propellers in the 1990s, and to revitalize the Do 328 a jet-powered derivative was built, the Do 328-300, later renamed 328JET. Changes were minimal, but retention of a straight wing meant relatively low speeds. After Fairchild Dornier's collapse continuation of the programme by the AvCraft company was short-lived. 110 328JET aircraft were constructed.

 

 
Do 328JET
length 21.28 m (69 ft 10 in)
span 20.98 m (68 ft 10 in)
engine 2 × Pratt & Whitney Canada PW306,
  2 × 2744 kg (6050 lb) thrust
max take-off weight 15 200 kg (33 510 lb)
max cruising speed 750 km/h (466 mph)
capacity 32-34 passengers
 
  DOUGLAS United States
Douglas Aircraft was founded at Santa Monica, California in 1921 by former Glenn Martin chief engineer Donald Douglas (1892-1981). Famous for its DC (Douglas Commercial) series airliners, the company also produced military aircraft. It merged to form McDonnell Douglas in 1967.
 
DC-2
FIRST FLIGHT 1934
The Boeing Model 247, the first true airliner with a metal monocoque construction and retractable landing gear, was trumped by the slightly larger, more efficient DC-2, which was derived from the DC-1 prototype. It was the first airliner that could operate profitably. 156 were built for US airlines and some foreign companies, notably KLM. The famous DC-3 was developed from the DC-2.

 

 
DC-2
length 18.89 m (62 ft 0 in)
span 25.91 m (85 ft 0 in)
engine 2 × Wright R-1820 Cyclone, 2 × 730 hp
max take-off weight 8420 kg (18 560 lb)
max speed 338 km/h (210 mph)
capacity 14 passengers
 
DC-3 / C-47 Skytrain / Dakota
FIRST FLIGHT 1935
Conceived as the DST sleeper aircraft with 14 beds, the DC-3 was already the world's most important airliner by the outbreak of World War II, when vast numbers were ordered by the military as C-53 Skytroopers and C-47 Skytrains, the latter having cargo doors. Dakota was the name given by the British. Over 10 000 examples were built, not including Japanese-built L2Ds and Russian
Li-2s . With their legendary strength, many continued
in airline and military service for decades after the war.

 

 
C-47A
length 19.66 m (62 ft 0 in)
span 29.98 m (85 ft 0 in)
engine 2 × Pratt & Whitney R-1830 Twin Wasp, 2 × 1200 hp
max take-off weight 11 793 kg (26 000 lb)
max speed 369 km/h (229 mph)
capacity 28 passengers
 
  ECLIPSE United States
Founded by former Microsoft executive Vern Raburn, Eclipse Aviation produced its Eclipse 500 Very Light Jet (VLJ) aircraft at Albuquerque, New Mexico, but entered bankrupcy in late 2008.
 
500
FIRST FLIGHT 2002
Belonging to a new class of Very Light Jet (VLJ) aircraft , the Eclipse 500 evolved from the Williams V-Jet II, designed by Burt Rutan as a testbed and demonstrator for the Williams FJX-2 engine. Eclipse reworked it as a slightly larger aircraft of metal rather than composite construction. Service entry occured in 2007. Production was halted in October 2008 after some 260 examples..

 
500
length 10.20 m (33 ft 5 in)
span 11.60 m (37 ft 9 in)
engine 2 × Pratt & Whitney Canada PW610,
  2 × 408 kg (900 lb) thrust
max take-off weight 2722 kg (6000 lb)
max speed 685 km/h (425 mph)
capacity 6 persons
 
  EMBRAER Brazil
Created by the Brazilian government in 1969, Embraer has managed to develop into a major and succesvol aircraft manufacturer building a range of airliners and business jets as well as military and light aircraft. The company was privatized in 1994, and is based in São José dos Campos, São Pauo state.
 
E-170 / -175
FIRST FLIGHT 2002
Embraer's greatest achievement yet, the E-170 is an all- new jetliner for 70 passengers, with the enlarged E-190 accommodating over 100. The E-175, also designated E-170-200, is an intermediate 'stretch' by 1.8 m (6 ft), seating up to 88 passengers. Seating is four-abreast. The E-170 entered service with LOT of Poland in 2004. 300 E-170s and E-175s were in service by July 2010.

 
E-170
length 29.90 m (98 ft 1 in)
span 26.00 m (85 ft 4 in)
engine 2 × General Electric CF34, 2 × 6260 kg (13 800 lb) thrust
max take-off weight 35 990 kg (79 300 lb)
max cruising speed 890 km/h (553 mph)
capacity 70-80 passengers
 
E-190 / -195
FIRST FLIGHT 2004
The E-190 and -195 are enlarged variants of the E-170, the E-195 having a fuselage length of 38.7 m (127 ft) and seating up to 122 passengers. Ordered by many major airlines, these are hardly 'regional' airliners, but rivals to the smallest Boeing and Airbus aircraft, though development of a still larger variant has been cancelled following concerns that its range would fall short. Some 300 E-190s and 50 E-195s were in service by July 2010.

 
E-190
length 36.24 m (118 ft 11 in)
span 28.72 m (94 ft 3 in)
engine 2 × General Electric CF34, 2 × 8392 kg (18 500 lb) thrust
max take-off weight 47 790 kg (105 400 lb)
max cruising speed 890 km/h (553 mph)
capacity 94-114 passengers
 
  EUROCOPTER France / Germany
One of the world's largest helicopter manufacturers, Eurocopter was formed in 1992 from the merger of the helicopter divisions of Aérospatiale, located at Marseille-Marignane airport, and MBB in Donauwörth, Bavaria. Like Airbus, Eurocopter is a subsidiary of EADS.
 
EC.665 Tiger / Tigre
FIRST FLIGHT 1991
After some 20 years of development, the Tiger combat helicopter finally became operational with the French Army in 2008. The French Tigre HAP version lacks the sight mounted on the German Tiger UH's rotor mast, while the latter presently does not have a nose-mounted cannon. The Tigre HAD is an uprated HAP for the French and Spanish armies, while the Tiger ARH version has been ordered by Australia. An unusal feature is that the Tiger's pilot is seated in front and the gunner in the back.

 

 
EC.665 Tigre HAP
fuselage length 14.08 m
  (46 ft 2 in)
rotor diam 13.00 m (42 ft 8 in)
engine 2 × MTU / Turboméca / Rolls-Roye MTR390, 2 × 1170 hp
max take-off weight 6100 kg (13 448 lb)
max speed 290 km/h (181 mph)
capacity 2 persons
 
EC.135
FIRST FLIGHT 1994
Developed from the MBB Bo 108 advanced technology helicopter, the EC.135 was given a enclosed fenestron tail rotor, and together with the roomy cabin this safety-enhancing feature has made the EC.135 popular as an ambulance helicopter. Two stretchers can be loaded though the rear doors. The EC.135P is powered by PW206 engines, and the EC.635 is a military variant.

 

 
EC.135T-1
fuselage length 10.20 m
  (33 ft 6 in)
rotor diam 10.20 m (33 ft 6 in)
engine 2 × Turboméca Arrius, 2 × 583 hp
max take-off weight 2900 kg (6393 lb)
max speed 259 km/h (162 mph)
capacity 7-8 persons
 
EC.120 Colibri
FIRST FLIGHT 1995
An all-new single-engined light helicopter developed
in France and aimed mainly at civilian customers, the Colibri (Hummingbird) is constructed mostly from composite materials and is characterized by its low noise levels. China took a 24% share in the EC-120 project, the HC-120 version being manufactured at Harbin as a training helicopter for the Chinese Army.
 
 
EC.120
fuselage length 9.60 m
  (31 ft 6 in)
rotor diam 10.00 m (32 ft 10 in)
engine 1× Turboméca Arrius, 450 hp
max take-off weight 1715 kg (3773 lb)
max speed 280 km/h (172 mph)
capacity 5 persons
 
EC.155
FIRST FLIGHT 1997
Initially designated AS.365N-4, the EC.155 was developed from the Aérospatiale Dauphin, the prototype being a converted Dauphin. The EC.155 has an enlarged cabin and a five-blade composite main rotor. Among its roles are passenger transport, including VIP transport and offshore operation, and police work. An EC.175 variant will be built in China as the Harbin Z-15.

 

 
EC.155
fuselage length 12.70 m
  (41 ft 8 in)
rotor diam 12.60 m (41 ft 4 in)
engine 2 × Turboméca Arriel, 2 × 948 hp
max take-off weight 5000 kg (11 023 lb)
max speed 324 km/h (201 mph)
capacity 14 persons
 
EC.145 / H-72 Lakota
FIRST FLIGHT 1999
Initially known as BK 117C-2, the EC.145 is an enlarged deritavitve of the MBB-Kawaki BK 117, incorporating advanced technology from the EC.135. The EC.145 is popular for ambulance and law enforcement duties, and is being adopted by the US Army as an ambulance and unarmed utlity helciopter, designated UH-72 Lakota.

 

 
EC.145
fuselage length 10.20 m
  (33 ft 6 in)
rotor diam 11.00 m (36 ft 1 in)
engine 2 × Turboméca Arriel, 2 × 738 hp
max take-off weight 3585 kg (7903 lb)
max speed 268 km/h (167 mph)
capacity 10-12 persons
 
EC.130
FIRST FLIGHT 1999
A development from the Aérospatiale AS.350 Ecureuil, the EC.130 features the French-engineerd fenestron or enclosed tail rotor, which enhances bystanders' safety and reduces noise. The EC.130 also has an enlarged cabin with larger windows, as well as landing skids that were first fitted to its smaller stablemate, the EC.120.

 

 
EC.130
fuselage length 10.68 m
  (35 ft 0 in)
rotor diam 10.69 m (35 ft 1 in)
engine 1× Turboméca Arriel, 847 hp
max take-off weight 2800 kg (6173 lb)
max speed 287 km/h (178 mph)
capacity 7-8 persons
 
  EUROFIGHTER – United Kingdom / Germany / Italy / Spain
Eurofighter is a company formed to produce the Typhoon fighter. EADS Deutschland and BAE each have a 33 per cent share, Alenia holds a 21 per cent share and EADS CASA, 13 per cent.
 
Typhoon
FIRST FLIGHT 1994
Four European nations decided to go ahead with a new collaborative fighter aircraft in 1985, with France opting for its own Rafale. Based on the British EAP prototype, the EFA or EF2000 was eventually named Typhoon. The first deliveries finally took place in 2003. 559 single-seat Typhoon S and two-seat Typhoon T aircraft are on order for the four partner nations, Austria, and Saudi Arabia.
 
 
Typhoon S
length 15.96 m (52 ft 5 in)
span 10.95 m (35 ft 11 in)
engine 2 × Eurojet EJ200, 2 × 9185 kg (20 250 lb) thrust
max take-off weight 20 800 kg (45 856 lb)
max speed Mach 2.0 (2125 km/h / 1320 mph)
capacity 1 person
 
  FAIRCHILD – United States
Sherman Fairchild, an inventor and entrepeneur, worked in aerial photography in the 1920s, and founded an aircraft manufacturing company to build a specialized survey aircraft. He acquired Kreider-Reisner Aircraft in Hagerstown, Maryland and renamed it Fairchild Aircraft. Later the firm bought and resold Hiller, and acquired Republic and Swearingen. Its 1996 takeover of Dornier was a failure, and today's Fairchild Corporation no longer buids aircraft.
 
F-24 / Argus
FIRST FLIGHT 1932
First flown as a two-seater, the F-24 was produced as a three-seater and developed into a four-seater by 1937. A rugged and comfortable private aircraft, it was powered by a Ranger inline engine or Scarab radial. The US Army ordered it as the UC-61 Forwarder light transport aircraft. Most UC-61s were delivered to the British, however, who named them Argus. Almost 2000 F-24s were produced.

 

 
UC-61
length 7.27 m (23 ft 10 in)
span 11.08 m (36 ft 4 in)
engine 1 × Warner R-500 Super Scarab, 165 hp
max take-off weight 1307 kg (2882 lb)
max speed 200 km/h (124 mph)
capacity 4 persons
 
  FOKKER – Germany
Dutchman Anthony Fokker (1890-1939) built his first aircraft in Germany in 1910. His Schwerin- based company manufactured 3,350 aircraft for the German Army throughout World War I. Fokker managed to move to Holland in 1918, smuggling trainloads of aircraft, materials and tools.
 
D.VII
FIRST FLIGHT 1917
Considered the finest German fighter of World War I, the D.VII was the winner of a January 1918 German Army competition. An estimated 1700 D.VIIs were completed by Fokker and Albatros, the Albatros firm building better quality aircraft, despite the hands-on Fokker company not being able to supply any drawings. D.VIIs were used by many nations after 1918, including the United States.

 

 
D.VII
length 6.95 m (22 ft 10 in)
span 8.90 m (29 ft 2 in)
engine 1 × Mercedes D.III, 160 hp
max take-off weight 910 kg (2006 lb)
max speed 185 km/h (115 mph)
capacity 1 person
 
  FOKKER – Netherlands
Established in Amsterdam in 1919, the Dutch Fokker company continued to build military aircraft, but was particularly succesful with its monoplane airliners, using its familiar construction method of tubular frames covered with linen. Fokker was slow to make the transition to all-metal aircraft, and only resumed building airliners in the 1950s. The company collapsed under its debts in 1996.
 
S.11 Instructor
FIRST FLIGHT 1947
After World War II Fokker resumed its S series of training aircraft with the S.11, in which the instructor and trainee pilot sat side by side. 360 S.11s were manufactured for the air forces of the Netherlands, Israel, Italy (under the Macchi M.416 name) and Brazil (designated T-21). Also manufactured in Brazil were 59 examples of the S.12
(T-22) variant, which featured a nosewheel landing gear.

 

 
S.11
length 8.18 m (26 ft 8 in)
span 11.00 m (36 ft 1 in)
engine 1 × Lycoming O-435, 190 hp
max take-off weight 1100 kg (2425 lb)
max speed 209 km/h (130 mph)
capacity 2-3 persons
 
  FOUGA – France
A repair company for railroad cars, Fouga started building aircraft in 1936. Its name has become synonymous with the famous Magister, though the company was dissolved into Potez in 1953.
 
CM.170 Magister
FIRST FLIGHT 1952
Designed by Robert Castello and Pierre Mauboussin, the CM.170, noted for its unusual V tail, was a succesful little jet trainer for basic flying tuition, of which almost 1000 examples were produced for France and other countries, including Germany, Belgium and Israel, which used the type for ground attack in the 1967 Six Day War. Aircraft modernized in Israel received the name Tzukit.

 

 
CM.170-1
length 10.05 m (33 ft 0 in)
span 12.15 m (39 ft 10 in)
engine 2 × Turboméca Marboré, 2 × 400 kg (880 lb) thrust
max take-off weight 3260 kg (7055 lb)
max speed 715 km/h (444 mph)
capacity 2 persons
 
CM.175 Zéphyr
FIRST FLIGHT 1956
Originally designated CM.170M, the CM.175 Zéphyr was a naval variant of the Magister for carrier flying training, with an arrester hook, a strengthed structure and new,
sliding cockpit canopies which were open during carrier take-offs and landings, since the Fougas did not have ejection seats. The French Navy received 30 examples.

 

 
CM.175
length 10.05 m (33 ft 0 in)
span 12.15 m (39 ft 10 in)
engine 2 × Turboméca Marboré, 2 × 400 kg (880 lb) thrust
max take-off weight 3200 kg (7055 lb)
max speed 715 km/h (444 mph)
capacity 2 persons
 
  GRUMMAN – United States
A former Loening employee, Leroy Grumman started his own aircraft company on Long Island, New York, in 1929. From the outset, Grumman specialized in manufacturing metal aircraft for the US Navy, and it was known as The Ironworks because of their strength. After the F-14 Tomcat it failed to produce succesful new designs, and it was absorbed into Northrop Grumman in 1994.
 
TBF Avenger
FIRST FLIGHT 1941
The US Navy's standard carrier-borne torpedo bomber for much of World War II, the TBF made its combat debut in the Pacific just ten months after its first flight. Almost 10 000 Avengers were built, mostly by General Motors as TBMs. After the war the type continued in service as an anti-submarine aircraft. The TBM-3R conversion was a carrier-capable transport plane for seven passengers.

 

 
TBF-3
length 12.19 m (40 ft 0 in)
span 16.51 m (54 ft 2 in)
engine 1 × Wright R-2600 Cyclone, 1900 hp
max take-off weight 8278 kg (18 250 lb)
max speed 430 km/h (267 mph)
capacity 3 persons
 
HU-16 Albatross
FIRST FLIGHT 1947
An amphibious flying boat, the Albatross was designed for light transport, reconnaissance, and rescue work - with its good seaworthiness, it could often perform open sea landings. The HU-16 designation replaced the original US Navy and US Air Force designations, UF and SA-16. The Canadian version was designated CSR-110.

 

 
HU-16B
length 19.18 m (62 ft 10 in)
span 29.46 m (96 ft 8 in)
engine 2 × Wright R-1820 Cyclone, 2 × 1425 hp
max take-off weight 17 010 kg (37 500 lb)
max speed 379 km/h (236 mph)
capacity 22 passengers
 
S-2 Tracker
FIRST FLIGHT 1953
An anti-submarine warfare aircraft for aircraft carriers, the S-2 (originally designated S2F) was also produced as a carrier-capable transport plane, the C-1 Trader, and airborne early warning aircraft, the E-1 Tracer. Surviving Trackers operate as land-based maritime patrol aircraft or as water bombers, often fitted with turboprop engines.

 

 
S-2E
length 13.26 m (43 ft 6 in)
span 22.13 m (72 ft 13 in)
engine 2 × Wright R-1820 Cyclone, 2 × 1525 hp
max take-off weight 13 222 kg (29 150 lb)
max speed 426 km/h (265 mph)
capacity 4 persons
 
G-164 Ag-Cat
FIRST FLIGHT 1957
In the 1950s, Grumman felt the need to diversify into civil aviation and designed the G-164 agicultural aircraft, of biplane configuration like the Antonov An-2, and given a cat name like the Grumman fighters. It exists in different versions and conversions, powered by various engines. Ag-Cat production was carried out by Schweizer Aircraft.

 

 
G-164A
length 7.11 m (23 ft 4 in)
span 10.95 m (35 ft 11 in)
engine 1 × Pratt & Whitney R-985 Wasp Junior, 450 hp
max take-off weight 2040 kg (4500 lb)
max speed 237 km/h (147 mph)
capacity 1 person
 
E-2 Hawkeye
FIRST FLIGHT 1960
The world's only airborne early warning aircraft designed as such from scratch, the carrier-capable E-2 Hawkeye is operated by the US and French navies among other users. It replaced the E-1 variant of the S-2 Tracker in the US Navy. Developed from the E-2, the C-2A Greyhond
is a carrier-capable transport aircraft, replacing the C-1.

 

 
E-2C
length 17.56 m (57 ft 7 in)
span 24.58 m (80 ft 7 in)
engine 2 × Allison T56, 2 × 5100 hp
max take-off weight 23 391 kg (55 000 lb)
max speed 604 km/h (375 mph)
capacity 5 persons
 
  HAMBURGER FLUGZEUGBAU Germany
The Blohm & Voss shipyard established its aircraft subsidiary, Hamburger Flugzeugbau, in 1933, although in practice the parent company's name was used. Its chief designer was the innovative Richard Vogt. The company was resurrected after the war, and became a part of MBB in 1969.
 
HFB 320 Hansa Jet
FIRST FLIGHT 1964
In 1944 Hans Wocke designed the Junkers Ju 287, an experimental jet aircraft with a forward-swept wing. After working in Russia and East Germany, Wocke moved
to Hamburg and used forward sweep on the HFB 320 private jet, the advantage being an unobstructed cabin. Not helped by a number of accidents, production of this unusual machine ceased in 1973 after only 47 aircraft.

 

 
HFB 320
length 16.61 m (54 ft 6 in)
span 14.48 m (47 ft 6 in)
engine 2 × General Electric CJ610, 2 × 1406 kg (3100 lb) thrust
max take-off weight 9199 kg (20 280 lb)
max cruising speed 825 km/h (513 mph)
capacity 7-12 passengers
 
  HAWKER / HAWKER SIDDELEY – United Kingdom
After the liquidation of Sopwith Aviation in 1920, Thomas Sopwith and his Australian test pilot, Harry Hawker, staed a new company using Hawker's name. In 1925, Sydney Camm became chief designer. In 1935, Hawker merged with car and aircraft engine builder Armstrong Siddeley. Following absorption of Folland, De Havilland and Blackburn, the company rebranded its aircraft under the Hawker Siddeley name in 1963. Hawker Siddeley finally became part of BAE in 1977.
 
Hurricane
FIRST FLIGHT 1935
Markedly inferior to the Spitfire and Messerschitt Bf 109, Camm's Hurricane was, however, simpler to produce
in quantity than in its brother in arms, thus playing a vital role in the Battle of Britain. Later in the war the type was used as a fighter-bomber, and the Hurricane IID version was fitted with two heavy 40-mm anti- tank guns. A total of 14 000 examples was built in the UK and in Canada.

 

 
Hurricane Mk.I
length 9.55 m (31 ft 4 in)
span 12.19 m (40 ft 0 in)
engine 1 × Rolls-Royce Merlin, 1030 hp
max take-off weight 3021 kg (6661 lb)
max speed 508 km/h (316 mph)
capacity 1 person
 
  HINDUSTAN AERONAUTICS (HAL) – India
Hindustan Aircraft was established in Bangalore in 1940 to support the British-administered Indian Air Force. Since independence in 1947 HAL has produced several indigenous designs.
 
HJT-16 Kiran
FIRST FLIGHT 1964
In 1961 HAL started work on a jet trainer for basic flying instruction, named Kiran (Ray of Light). The indigenous
HJE-2500 turbojet did not materialize and the Kiran Mk.I, delivered to the Indian Air Force from March 1968, was powered by the Rolls-Royce Viper engine. From 1976
onwards, the Mk.I was followed by the Mk.II, featuring the more powerful Rolls-Royce Orpheus turbojet. A total of 190 Kirans were built for the Indian Air Force and Navy.
 
 
Kiran Mk.I
length 10.60 m (34 ft 9 in)
span 10.70 m (35 ft 1 in)
engine 1 × Rolls-Royce Viper, 1 × 1135 kg (2500 lb) thrust
max take-off weight 4200 kg (9259 lb)
max speed 695 km/h (432 mph)
capacity 2 persons
 
  HUGHES – United States
The Hughes Aircraft Company was established in Los Angeles by the eccentric millionaire, Howard Hughes, in 1932. After personally flying the massive H-4 Hercules, or 'Spruce Goose', flying boat for the first and only time in 1947, Hughes switched his attention to helicopters. Hughes Helicopters was sold to McDonnell Douglas in 1984, after designing the AH-64 Apache.
 
269 / 300
FIRST FLIGHT 1956
A three-seat light helicopter, the Hughes 269 has also been marketed as the Hughes 300. It is often used as a training helicopter, and the US Army adopted it as such as the TH-55 Osage. In the 1980s the design was sold to Schweizer Aircraft, which continues to manufacture it as the Schweizer 300. Total production is over 3400.

 

 
269C
fuselage length 6.80 m
  (22 ft 0 in)
rotor diam 8.18 m (26 ft 10 in)
engine 1 × Lycoming O-360, 190 hp
max take-off weight 975 kg (2150 lb)
max speed 176 km/h (109 mph)
capacity 3 persons
 
  ILYUSHIN– Russia
Based at Moscow-Khodynka airport, the design bureau of one of the great Russian aircraft constructors, Sergei Ilyushin (1894-1977), has predominantly produced bombers and airliners, although it also created the most imporant Russian aircraft of World War II, the Il-2 armoured attacker. The Ilyushin company is currently a division of OAK, the United Aircraft Corporation.
 
Il-12
FIRST FLIGHT 1945
When victory over Germany was certain, Stalin ordered the design of a new airliner to replace the DC-3 and Li-2. The Il-12's flight tests revealed numerous problems, and during their rectification the aircraft put on so much weight that its payload had to be reduced to a maximum of 21 passengers, rather than 32. It was thus grossly uneconomic, but 663 Il-12s were built nevertheless.

 

 
Il-12
length 21.31 m (69 ft 11 in)
span 31.70 m (104 ft 0 in)
engine 2 × Shvetsov ASh-82, 2 × 1850 hp
max take-off weight 17 250 kg (38 030 lb)
max speed 407 km/h (253 mph)
capacity 18-21 passengers
 
Il-14
FIRST FLIGHT 1950
Because of the Il-12's shortcomings, Ilyushin designed an all-new aircraft with the same dimensions, and this, the Il-14, became the standard airliner with Aeroflot
and with the airlines of all other communist countries.
It was licence-built in Czechoslowakia as the Avia 14, and in East Germany, deliveries exceeding 1000 aircraft.

 

 
Il-14P
length 21.31 m (69 ft 11 in)
span 31.70 m (104 ft 0 in)
engine 2 × Shvetsov ASh-82, 2 × 1900 hp
max take-off weight 17 250 kg (38 030 lb)
max speed 430 km/h (267 mph)
capacity 24-32 passengers
 
Il-18
FIRST FLIGHT 1957
First applied to a large passenger aircraft flown in 1946, the Il-18 designation was re-used for the Soviet Union's first turboprop-powered airliner. A succesful medium- range aircraft, the Il-18 carried 260 million passengers with Aeroflot. 565 were built, including 121 for export. Many were converted for cargo or military roles. The Il-38 maritime patrol aircraft was developed from the Il-18.

 

 
Il-18D
length 37.40 m (122 ft 8 in)
span 37.90 m (124 ft 4 in)
engine 4 × Ivchenko AI-20, 4 × 4250 hp
max take-off weight 64 000 kg (140 800 lb)
max crusiing speed 674 km/h (419 mph)
capacity 89 passengers
 
Il-62
FIRST FLIGHT 1963
The Soviet Union's first intercontinental jetliner, the Il-62 featured four tail-mounted engines, a configuration also chosen for the British VC10. The original NK-8 turbofans gave problems, but the Soloviev-powered Il-62M proved itself as a reliable airliner. Of some 270 Il-62s built, a few dozen remain in use, often as government aircraft.

 

 
Il-62M
length 53.12 m (174 ft 3 in)
span 43.20 m (141 ft 9 in)
engine 4 × Soloviev D-30K, 4 × 11 022 kg (24 300 lb) thrust
max take-off weight 165 000 kg (363 763 lb)
max cruising speed 900 km/h (559 mph)
capacity 186 passengers
 
  JODEL – France
Test pilot Edouard Joly and his son-in-law, engineer Jean Délémontez, combined their names to create Avions Jodel near Beaune in 1946, and developed a series of light aircraft of plywood construction. These were produced as homebuilds and by other companies, particularly CEA, which became Robin. Jodel still exists as a design bureau, selling licences to amateur builders.
 
D9 Bébé
FIRST FLIGHT 1948
On 22 January 1948 Edouard Joly first flew the single- seat D9. The tiny aeroplane had considerable anhedral on its outer wings, a characteristic of subsequent Jodel and Robin designs. Perfromance was adequate and over 500 Bébés were constructed, mostly by amateur builders. The D91 through D98 models are powered by various engines, the D92 being the most numerous.

 

 
D92
length 5.45 m (17 ft 11 in)
span 7.00 m (22 ft 11 in)
engine 1 × Volkswagen 1100, 26 hp
max take-off weight 272 kg (598 lb)
max speed 150 km/h (93 mph)
capacity 1 person
 
D11
FIRST FLIGHT 1950
After the single-seat D9 Jean Délémontez designed the three-seat D10, but shelved it in favour of the two-seat D11 on the request of the French government, which sought to encourage pilot training. A small government order enabled Délémontez to buy himself a Citroën 2CV. Originally powered by a 45 hp Salmon engine, the D11 has been built by both commercial manufacturers and amateurs in versions designated D111 through D128, fitted with engines ranging in power from 60 to 120 hp.

 

 
D112
length 6.36 m (20 ft 10 in)
span 8.20 m (26 ft 10 in)
engine 1 × Continental A65, 65 hp
max take-off weight 520 kg (1145 lb)
max speed 190 km/h (118 mph)
capacity 2 persons
 
D140
FIRST FLIGHT 1958
With a 180-hp engine, the D140 has good performance and is popular for use at mountain airfields. The D140 Mousquetaire (Musketeer) was produced to the extent of 215 examples by the SAN company, the D140C and E models having modified tail surfaces. There were also a number of homebuilds. In addition, SAN delivered 28 D140R Abeille (Bee) dedicated glider tugs from 1965.

 

 
D140
length 10.27 m (33 ft 8 in)
span 7.92 m (26 ft 0 in)
engine 1 × Lycoming O-360, 180 hp
max take-off weight 1200 kg (2646 lb)
max speed 240 km/h (149 mph)
capacity 5 persons
 
DR100 / DR1050
FIRST FLIGHT 1959
Working with Pierre Robin, Délémontez revamped his shelved D10 three-seater as the DR100, which was put into production by the CEA and SAN companies. With small changes it became the DR1050, which was named Sicile by CEA and Ambassadeur by SAN, and Excellence and Sicile Record, respectively, when fitted with a swept tailfin. The DR105 and DR1051 through DR1056 variants were powered by different engines.

 

 
DR1050
length 6.80 m (22 ft 4 in)
span 8.72 m (28 ft 7 in)
engine 1 × Continental O-200, 100 hp
max take-off weight 750 kg (1654 lb)
max speed 185 km/h (115 mph)
capacity 3-4 persons
 
DR200
FIRST FLIGHT 1964
A more powerful, more sophisticated development of the DR100, the DR200 was produced by CEA/Robin as the DR220 with a Continental O-200; the DR221 Dauphin with a Lycoming O-235; and the DR250 Capitaine with a Lycoming O-320 engine. A nosewheel gear derivative of the DR250, the DR253, evolved into the Robin DR300.

 

 
DR221 Dauphin
length 6.90 m (22 ft 7 in)
span 8.72 m (28 ft 7 in)
engine 1 × Lycoming O-235, 115 hp
max take-off weight 830 kg (1830 lb)
max speed 245 km/u (152 mph)
capacity 4 persons
 
  JUNKERS – Germany
During World War I Professor Hugo Junkers (1859-1935), whose firm in the town of Dessau manufactured boilers and radiators, built the world's first practical all-metal aircraft. His metal airliners achieved success in the 1920s, being heavier but more durable than their Fokker rivals. Junkers built mainly bombers during World War II, including the Ju 87 Stuka or dive bomber.
 
D.I
FIRST FLIGHT 1918
Following the relative successof its J.I attack biplane, Junkers built a new metal monoplane which eventually reached the German Army as the Junkers D.I single- seat fighter (company designation, J.9). Too heavy for a fighter but able to take some punishment, it was to be employed against heavily-defended Allied observation balloons; however, only 40 examples were completed.

 

 
D.I
length 7.25 m (23 ft 9 in)
span 9.00 m (29 ft 6 in)
engine 1 × Mercedes D.III, 160 hp
max take-off weight 834 kg (1839 lb)
max speed 225 km/h (140 mph)
capacity 1 person
 
Ju 52
FIRST FLIGHT 1930
The last Junkers aircraft to have a corrugated metal skin, the Ju 52 began life as a single-engined cargo aircraft. The three-engined Ju-52/3m, a succesful airliner, was employed by the Luftwaffe as a makeshift bomber. During the war 'Auntie Ju' served on all fronts as a transport, and was instrumental in the airborne landings in Holland and Crete. The Ju 52/3m was also built in France, as the AAC.1, and in Spain, as the CASA C-352.

 

 
Ju 52/3mg3e
length 18.90 m (62 ft 0 in)
span 29.25 m (104 ft 0 in)
engine 3 × BMW 132, 3 × 725 hp
max take-off weight 10 500 kg (23 149 lb)
max speed 275 km/h (171 mph)
capacity 18 passengers
 
  KAMAN – United States
Not to be confused with Kamov from Russia, Kaman is a helicopter builder based in Connecticut. The company was founded in 1945 by Charles Kaman, who also invented the Ovation guitar.
 
H-2 Seasprite
FIRST FLIGHT 1959
Initially designed a single-engined rescue helicopter for aircraft carriers, the Seasprite was developed into the twin-engined SH-2 anti-submarine helicopter for service on board smaller warships. The USA no longer uses the H-2, but limited numbers of SH-2G Super Seasprites serve with the navies of Egypt, New Zealand and Poland.

 

 
SH-2G
fuselage length 12.30 m
  (40 ft 4 in)
rotor diam 13.41 m (45 ft 0 in)
engine 2 × General Electric T700, 2 × 1723 hp
max take-off weight 6120 kg (13 500 lb)
max speed 256 km/h (159 mph)
capacity 8 persons
 
  KAMOV – Russia
Russian engineer Nikolai Kamov built his first autogyro in 1929, and in 1947 his first helicopter, the one-man Ka-8, took to the air. Its two co-axial main rotors, eliminating the need for a tail rotor, have been a feature of virtually all Kamov desgins until the appearance of the Ka-60 in 1998.
 
Ka-25
FIRST FLIGHT 1960
Initially known as Ka-20, the Ka-25 shipboard helicopter was deployed by the Soviet Navy in three variants: the Ka-25BSh for anti-submarine warfare, the Ka-25K for guiding missiles launched by ships, and the Ka-25PS for rescue and transport. Named Hormone by NATO,
the Ka-25 was exported to Bulgaria, India, Syria, Vietnam and Yugoslavia, and about 460 examples were built.

 

 
Ka-25BSh
fuselage length 9.75 m
  (32 ft 0 in)
rotor diam 15.74 m (51 ft 8 in)
engine 2 × Glushenkov GTD-3, 2 × 900 hp
max take-off weight 7500 kg (16 535 lb)
max speed 209 km/h (130 mph)
capacity 14 persons
 
Ka-27
FIRST FLIGHT 1974
Heavier than the Ka-25, the Ka-27 Helix fits in the same space with is rotors folded, and is thus able to operate from the same ships as its predecessor. The Ka-27PL is for anti-submarine use; the Ka -27PS for rescue work; the Ka-28 an export variant, sold to several nations, the Ka-29 a military transport; and the Ka-31 is a warning radar helicopter for Russian and Indian aircraft carriers. The Ka-32 civil model can be seen over forests in many countries, used for both logging and firefighting work.

 

 
Ka-32A
fuselage length 11.30 m
  (37 ft 1 in)
rotor diam 15.90 m (52 ft 2 in)
engine 2 × Klimov TV3, 2 × 2225 hp
max take-off weight 12 600 kg (27 775 lb)
max speed 250 km/h (155 mph)
capacity 16 passengers
 
  KLEMM – Germany
Hans Klemm's aircraft company in Böblingen, near Stuttgart, was known for its two-seat sports monoplanes. After World War II the refounded Klemm company was taken over by Bölkow.
 
Kl 35
FIRST FLIGHT 1935
Designed by Friedrich Fecher, the Kl 35 was a mixed- construction monoplane with open cockpits and a low- set inverted gull wing. The German Luftwaffe adopted it as an elementary trainer, and it was built at Fieseler and Zlin as well as by Klemm. The Swedish Air Force also used it, and surviving examples are of Swedish origin.

 

 
Kl 35D
length 7.50 m (24 ft 7 in)
span 10.40 m (34 ft 2 in)
engine 1 × Hirth HM 60, 80 hp
max take-off weight 750 kg (1654 lb)
max speed 212 km/h (132 mph)
capacity 2 persons
 
Kl 107
FIRST FLIGHT 1940
The Kl 107 first flew in 1940 and despite the fact that this light two-seater was of no value to the German war effort a small batch of Kl 107As were produced. In the 1950s Klemm built 26 updated Kl 207B aircraft before selling his business to Bölkow. Bölkow produced 30 Kl 107Cs and used the Kl 107 as the basis for its own Bo 207.

 

 
Kl 107A
length 8.16 m (26 ft 9 in)
span 10.87 m (35 ft 8 in)
engine 1 × Hirth HM 60, 82 hp
max take-off weight 625 kg (1378 lb)
max speed 190 km/h (118 mph)
capacity 2 persons
 
  LOCKHEED / LOCKHEED MARTIN – United States
In 1926, Allan and Malcolm Loughead, whose name was frequently being mispronounced, changed the name of their aircraft company to Lockheed. In the 1930s, the firm was succesful with its L-10 Electra airliner, and with Clarence 'Kelly' Johnson as it chief engineer, evolved into
a major company, with three assembly plants at Burbank and Palmdale, California, and Marietta
in Georgia. In 1995, Lockheed merged with Martin to form the Lockheed Martin Corporation.
 
P-2 Neptune
FIRST FLIGHT 1945
Though too late for World War II, the P2V maritime patrol bomber (later redesignated P-2) proved its abilities with an 18 000 km (11 000 miles) non-stop flight in 1946. During the Neptune's long life, cannon and bombs were replaced by sensors and depth charges, and the final models introduced two auxiliary jet engines to allow for higher take-off weights. The P-2J, with T64 turboprops replacing the piston engines, was produced in Japan.

 

 
P-2H
length 27.94 m (91 ft 8 in)
span 31.65 m (103 ft 10 in)
engine 2 × Wright R-3350 Cyclone, 2 × 3500 hp
  2 × Westinghouse J34, 2 x 1540 kg (3400 lb) thrust
max take-off weight 36 240 kg (79 895 lb)
max speed 648 km/h (403 mph)
capacity 7 persons
 
T-33
FIRST FLIGHT 1948
Originally designated TF-80C, the T-33 is an advanced trainer developed from the F-80 Shooting Star, an early jet fighter. Over 6500 'T-Birds' were built, the Canadair- built T-33A-Ns having Rolls-Royce Nene engines. The RT-33A is a single-seat photo reconnaissance aircraft.

 

 
T-33A
length 11.48 m (37 ft 9 in)
span 11.85 m (38 ft 10 in)
engine 1 × Allison J33, 1 × 2360 kg (5200 lb) thrust
max take-off weight 6551 kg (14 442 lb)
max speed 960 km/h (600 mph)
capacity 2 persons
 
F-104 Starfighter
FIRST FLIGHT 1954
In response to the increasing complexity of jet fighters, Kelly Johnson designed a light aircraft with a big engine and a tiny wing, sacrificing manoeuvrability and load- carrying ability for blistering climb speed and Mach 2.2 performance. It was a dismal failure in US service, but Lockheed still managed to sell improved fighter-bomber versions to America's allies: 2575 Starfighters, including two-seat trainers, were produced. The final variant, the Italian F-104S, was not retired from service until 2004.

 

 
F-104G
length 16.89 m (54 ft 9 in)
span 6.68 m (21 ft 11 in)
engine 1 × General Electric J79, 1 × 7166 kg (15 800 lb) thrust
max take-off weight 13 054 kg (28 779 lb)
max speed Mach 2.2 (2350 km/h / 1460 mph)
capacity 1 person
 
L-1011 TriStar
FIRST FLIGHT 1970
Lockheed's last airliner, the three-engined, widebodied
L-1011 was pitted against the DC-10, but was seriously hindered by difficulties at Rolls-Royce, the sole engine supplier, delaying the appearance of growth variants, the L-1011-200 and the shortened, long-range L-1011-500. Lockheed sold only 250 aircraft, half the number needed
to make a profit. Britain's Royal Air Force operates nine L-1011-500s as aerial refuelling tankers and transports.

 

 
L-1011-500
length 50.04 m (164 ft 2 in)
span 50.09 m (164 ft 4 in)
engine 3 × Rolls-Royce RB.211, 3 × 22 680 kg (50 000 lb) thrust
max take-off weight 224 980 kg (496 000 lb)
max cruising speed 960 km/h (597 mph)
capacity 234-330 passengers
 
  MACCHI – Italy
The Nieuport-Macchi company was founded by Giulio Macchi in 1913 to produce the Nieuport 11 fighter in Varese. Aeronautica Macchi subsequently concentrated on racing seaplanes, including the world's fastest aircraft, the MC.72, and fighter aircraft. It was renamed Aermacchi in 1962.
 
MB.308
FIRST FLIGHT 1947
Based on a prewar design by Ermanno Bazzocchi, the wooden MB.308 light touring aircraft was built in 1946 and ordered in quantity by the Italian Air Force, despite being of little military use, and most 'Macchinos' were made available to Italy's aeroclubs. The MB.308G model featured a third seat in the back, and was also produced in Argentina, by sailplane manufacturer German Bianco.

 

 
MB.308
length 6.52 m (21 ft 5 in)
span 10.00 m (32 ft 10 in)
engine 1 × Continental C85, 85 hp
max take-off weight 642 kg (1412 lb)
max speed 197 km/h (122 mph)
capacity 2 persons
 
  MANSYU – Japan
In 1938, the Japanese government established the Manchurian Aircraft Manufacturing Company in Manchuko, Japan's puppet state in China. It was a major production plant, but did not create significant designs of its own. Its facilities in Harbin were important to the Chinese after 1945.
 
Ki-79
FIRST FLIGHT 1942
The Ki-79 was a trainer derived from the Nakajima Ki-27 fighter, which was built at Mansyu. 1329 Ki-79's were produced, in four versions - the Ki-79a single-seat trainer, the Ki-79b two-seater, and the Ki-79c and Ki-79d in which scarce metal was replaced by wood. Several Ki-79s were left behind in Indonesia in 1945, and used against the returning Dutch troops by the Indonesians.

 

 
Ki-79a
length 7.85 m (25 ft 9 in)
span 11.50 m (37 ft 9 in)
engine 1 × Hitachi Ha-13, 510 hp
max take-off weight unknown
max speed 340 km/h (211 mph)
capacity 1 person
 
  MAX HOLSTE – France
Max Holste, who built his first aircraft in 1931, began his own aircraft company in Reims in 1946. It is now Reims Aviation. Holste went on to assist in the design of Brazil's Embraer Bandeirante.
 
MH.1521 Broussard
FIRST FLIGHT 1952
Broussard is 'bushman' in French, and this six-seat aircraft was designed to cope with short, rough airstrips. Of nearly 400 Broussards produced, most went to the French armed forces, some getting transferred to France's African colonies upon independence. Today a number of Broussards are still flying as private aircraft.

 

 
MH.1521M
length 8.65 m (28 ft 5 in)
span 13.75 m (45 ft 1 in)
engine 1 × Pratt & Whitney R-985, 450 hp
max take-off weight 2500 kg (5512 lb)
max speed 270 km/h (168 mph)
capacity 6 persons
 
  MBB – Germany
MBB was formed in 1969 by merging Messerschmitt, Bölkow and Hamburger Flugzeugbau (Blohm + Voss). VFW was purchased in 1981. The leading German aerospace company, MBB was a major participant in numerous international aircraft ventures. MBB became DASA in 1989. DASA is now the German division of EADS, the parent company of Airbus and Eurocopter.
 
Bo 105
FIRST FLIGHT 1967
Bölkow's Bo 105 was an advanced small helicopter at the time of its apperance, featuring two turbine engines and a hingeless rotor with four fiberglass blades, giving high manoeuvrability. As an ambulance helicopter it can carry two stretchers in its relatively roomy cabin. Some 1500 Bo 105s were produced, including over 300 for the German Army in observation, liaison and anti-tank roles.

 

 
Bo 105CB
fuselage length 8.56 m
  (28 ft 1 in)
rotor diam 9.84 m (32 ft 4 in)
engine 2 × Allison 250, 2 × 420 hp
max take-off weight 2500 kg (5510 lb)
max speed 242 km/h (150 mph)
capacity 5 persons
 
  MBB / Kawasaki – Germany / Japan  
BK 117
FIRST FLIGHT 1979
In 1977 MBB and Kawasaki Heavy Industries agreed to combine their Bo 107 and KH-7 designs, the German side developing the rotor and tail unit and the Japanese side a spacious fuselage as well as the gearbox. Of 370 BK 117s built, many serve as ambulance helicopters. A new, stretched derivative incorporating features of the Eurocopter EC.135 is known as the Eurocopter EC.145.

 

 
BK 117B-2
fuselage length 9.88 m
  (32 ft 5 in)
rotor diam 11.00 m (36 ft 1 in)
engine 2 × Lycoming LTS101, 2 × 700 hp
max take-off weight 3350 kg (7385 lb)
max speed 270 km/h (168 mph)
capacity 7-11 persons
 
  MIKOYAN-GUREVICH – Russia
Constructors Artem Mikoyan and Mikhail Gurevich were given their own design bureau in 1939
to develop the MiG-1 interceptor fighter. Practically all of their aircraft have been fighters. Based
in Moscow, their design bureau is now the MiG division of OAK, the United Aircraft Corporation.
 
MiG-9
FIRST FLIGHT 1946
Powered by captured BMW turbojets, the I-300 prototype became the first Russian jet to fly on 24 April 1946, just before the Yak-15 as the Mikoyan team had won a toss. Though limited as a fighter, the MiG-19, named Fargo
by NATO, was quite a good aircraft and 600 were built. Variants not built in quantity included two-seat trainers and the I-307 which was fitted with afterburning engines.

 

 
MiG-9
length 9.83 m (32 ft 3 in)
span 10.00 m (32 ft 10 in)
engine 2 × Kolesov RD-20, 2 × 800 kg (1764 lb) thrust
max take-off weight 4860 kg (10 714 lb)
max speed 910 km/h (565 mph)
capacity 1 person
 
MiG-15
FIRST FLIGHT 1947
In 1946 the Soviet Union was allowed to buy the power- ful Rolls-Royce Nene engine, and Mikoyan lost no time building around it a small swept-winged fighter that was arguably the best of its day, as the West found out in the Korean War. Some 6000 MiG-15 and improved -15bis fighters were built, not couting Czech-made S-102/-103s and Polish Lim-1/-2s. NATO called the type Fagot, the reporting name Falcon having been found 'too laudatory'.

,

 
MiG-15bis
length 10.11 m (33 ft 2 in)
span 10.08 m (33 ft 1 in)
engine 1 × Klimov VK-1, 2700 kg (5950 lb) thrust
max take-off weight 6106 kg (13 461 lb)
max speed 1107 km/h (688 mph)
capacity 1 person
 
  NHI – Netherlands
NHI (Nederlandse Helikopter Industrie) was a joint venture by aircraft manufacturer Aviolanda and engine maker Kromhout. Its purpose was to undertake production of the Kolibrie helicopter.
 
H-3 Kolibrie
FIRST FLIGHT 1956
Developed from the SOBEH H-2 of 1955 , the Kolibrie (Hummingbird) was an innovative two-seat helicopter powered by two rotor tip-mounted ramjets. Its main use was as a cropduster, fitted with spray booms and with up to three of the four fuel tanks devoted to chemicals. Its high fuel consumption made the type uneconomical, though, and only about a dozen aircraft were completed.

 

 
H-3
fuselage length 4.22 m
  (13 ft 10 in)
rotor diam 10.00 m (33 ft 10 in)
engine 2 × Kromhout TJ-5, 2 × 20 kg (44 lb) thrust
max take-off weight 650 kg (1433 lb)
max speed 113 km/h (70 mph)
capacity 2 persons
 
  NH INDUSTRIES - France / Germany / Italy / Netherlands
NH Industries is the consortium building the NH90 helicopter. After a round of mergers in Europe's aviation industry, Eurocopter holds a 63 per cent share in the project; Agusta, the Italian branch of Agusta Westland, holds 32 per cent; and Stork, the leftovers of Fokker, 5 per cent.
 
NH90 NFH
FIRST FLIGHT 1999
The NH90 is an all-new military helicopter built in two variants designated NFH (Nato Frigate Helicopter) and TTH (Tactical Transport Helicopter), the latter being able to carry 20 troops or over 2.5 tons of cargo. Engines are either RTM322s or General Electric T700s. After serious delays, deliveries to the German Army started in 2006 and orders from 15 nations have now been received.

 

 
NH90 TTH
fuselage length 16.13 m
  (52 ft 11 in)
rotor diam 16.30 m (53 ft 6 in)
engine 2 × Rolls-Royce / Turboméca RTM322, 2 × 2230 hp
max take-off weight 10 600 kg (23 370 lb)
max speed 305 km/h (189 mph)
capacity 20 passengers
 
  NORTH AMERICAN – United States
Originally a holding company of aviaton-related interests, North American Aviation started aircraft production at Inglewood, near Los Angeles, in 1935 under the leadership of James Kindelberger (1895-1962), and soon NAA was creating some of America's principal military aircraft. Setbacks in the company's aircraft, missile and space projects caused it to merge with Rockwell in 1967.
 
T-6 Texan / Harvard
FIRST FLIGHT 1937
The AT-6 advanced trainer, original US Army designation BC-1, was developed from the fixed landing gear BT-9. The type was designated SNJ by the US Navy, and named Harvard by the British. Over 15 000 examples were built, including Candian-manufactured Noorduyn AT-16s. They served in many countries after 1945, both
as trainers and as a light attack aircraft in colonial wars.
 
 
T-6G
length 8.99 m (29 ft 6 in)
span 12.80 m (42 ft 0 in)
engine 1 × Pratt & Whitney R-1340 Wasp, 550 hp
max take-off weight 2548 kg (5617 lb)
max speed 341 km/h (212 mph)
capacity 2 persons
 
B-25 Mitchell
FIRST FLIGHT 1940
A larger derivative of the earlier NA-40, the NA-62 design was ordered 'off the drawing board' by the US Army. A good, well-armed aircraft, the B-25 became the principal US medium bomber of World War II; 10 000 were built for the Allied air arms. Although not designed for carrier use, B-25s took off from the Hornet and bombed Tokyo in the Doolittle Raid of 1942. B-25s also served as anti- shipping aircraft, sometimes toting a 75-mm field gun.

 

 
B-25J
length 16.13 m (52 ft 11 in)
span 20.60 m (67 ft 7 in)
engine 2 × Wright R-2600 Double Cyclone, 2 × 1700 hp
max take-off weight 15 876 kg (35 000 lb)
max speed 438 km/h (272 mph)
capacity 6 persons
 
  PILATUS – Switzerland
A small aircraft manufacturer based in Stans, near Lucene, Pilatus manages to find worldwide markets for its single-engined turboprop aircraft, both military trainers and light transport types.
 
P-2
FIRST FLIGHT 1945
Conceived during World War II, the P-2 basic trainer was a compromised design utilizing Messerschmitt Bf 109 parts, including the landing gear, though it now extended outward to increase the aircraft's stability on the ground. The Swiss Army received 54 P-2s, half of them unarmed P-2.05 aircraft and the other half P-2.06 armed trainers.

 

 
P-2
length 9.07 m (29 ft 9 in)
span 11.00 m (36 ft 1 in)
engine 1 × Argus As 410, 465 hp
max take-off weight 1970 kg (4343 lb)
max speed 340 km/h (211 mph)
capacity 2 persons
 
P-3
FIRST FLIGHT 1953
The P-3 was designed as a basic trainer for the Swiss Air Force, which bought 72. The aircraft was not an international success, the only other sale being an order for six for the Brazilian Navy. From it was developed, however, the succesful PC-7. In the 1990s, 65 P-3s still in Swiss military service were sold to private owners.

 

 
P-3
length 8.75 m (28 ft 8 in)
span 10.40 m (34 ft 1 in)
engine 1 × Lycoming O-435, 260 hp
max take-off weight 1500 kg (3307 lb)
max speed 310 km/h (193 mph)
capacity 2 persons
 
PC-6 Porter
FIRST FLIGHT 1959
Now in production for half a century, the Porter looked like a light transport aircraft of thirty years earlier even when it was new, but it had exceptional short take-off and landing (STOL) capacities that were the key to its success. The original Porter, fitted with a piston engine, was replaced in production by the turpoprop-powered Turbo Porter in the early 1960s. Over 500 PC-6 aircraft have been built, including 92 by Fairchild in the USA.

 

 
PC-6/B2-H4 Turbo Porter
length 11.00 m (36 ft 1 in)
span 15.87 m (52 ft 1 in)
engine 1 × Pratt & Whitney Canada PT6, 680 hp
max take-off weight 2800 kg 6173 lb)
max cruising speed 259 km/h (161 mph)
capacity 10 persons
 
PC-7
FIRST FLIGHT 1966
In the 1960s almost all military flying training was on jet aircraft, and initially the PC-7, a P-3 derivative with much enhanced performance thanks to its turboprop engine, evoked little interest. After the 1973 oil crisis, though, the fuel-efficient PC-7 Turbo Trainer began gathering orders from some 15 nations. 455 PC-7s were sold, production terminating in 2000. The PC-7 Mk.II is a different aircraft.

 

 
PC-7
length 9.75 m (32 ft 0 in)
span 10.40 m (34 ft 1 in)
engine 1 × Pratt & Whitney Canada PT6, 550 hp
max take-off weight 2700 kg (5952 lb)
max speed 411 km/h (255 mph)
capacity 2 persons
 
PC-7 Mk.II
FIRST FLIGHT 1992
Despite its designation, the PC-7 Mk.II is based on the PC-9 but fitted with a less powerful version of the PT6 engine, for customers who don't require the PC-9's performance. The PC-7 Mk.II was built initially for the South African Air Force, which has named it Astra.

 

 
PC-7 Mk.II
length 10.13 m (33 ft 3 in)
span 10.19 m (33 ft 5 in)
engine 1 × Pratt & Whitney Canada PT6, 700 hp
max take-off weight 2850 kg (6283 lb)
max speed 555 km/h (345 mph)
capacity 2 persons
 
PC-9
FIRST FLIGHT 1984
Looking similar to the PC-7 but with a raised rear seat, the PC-9 trainer is in fact an almost entirely new design, with a more powerful version of the PT6 turboprop giving it the speed of a Spitfire. The US Air Force's Raytheon
T-6 Texan II was developed from the PC-9. Illustrated is the first prototype PC-9, now preserved in a museum.

 

 
PC-9M
length 10.18 m (33 ft 4 in)
span 10.19 m (33 ft 5 in)
engine 1 × Pratt & Whitney Canada PT6, 1150 hp
max take-off weight 3200 kg (7055 lb)
max speed 667 km/h (414 mph)
capacity 2 persons
 
PC-12
FIRST FLIGHT 1991
Another Pilatus design powered by a single PT6 engine, the PC-12, with its single engine, is similar in capacity and perfromance to the twin-engined Beech King Air, making for an efficient aircraft. The PC-12 is used mainly as a business aircraft, but thanks to the reliability of its engine it has been cleared for use as a single-engined regional airliner. A few PC-12s have entered service with the US Air Force, these carrying the designation U-27A.

 

 
PC-12
length 14.40 m (47 ft 3 in)
span 16.23 m (53 ft 3 in)
engine 1 × Pratt & Whitney Canada PT6, 1200 hp
max take-off weight 4740 kg (10 450 lb)
max cruising speed 500 km/h (313 mph)
capacity 8-11 persons
 
PC-21
FIRST FLIGHT 2002
The latest Pilatus trainer, the newly designed PC-21 has a shorter-span wing and an advanced cockpit, in order to approximate to the characteristics of modern fast jet aircraft as much as possible. The first customer is the Singapore Air Force, which bought 19 for its flying school at Perth, Australia. The Swiss Air Force has ordered six.

 

 
PC-21
length 11.23 m (36 ft 11 in)
span 9.11 m (29 ft 11 in)
engine 1 × Pratt & Whitney Canada PT6, 1600 hp
max take-off weight 4250 kg (9370 lb)
max speed 685 km/h (428 mph)
capacity 2 persons
 
  PIPER – United States
In 1937, Taylor Aircraft was renamed Piper Aircraft by businessman William Piper, following a clash with designer Clarence Taylor, who had left to start another company, Tailorcraft. Piper is a major manufacturer of light aircraft: by 2009 it had built 144 000 aircraft, of which some 85 000 were still active. Product liability problems completely stopped production in the mid-1980s. The resurgent company was known as New Piper for a while. Piper is based in Vero Beach, Florida.
 
J-2 Cub
FIRST FLIGHT 1938
First flown in 1930, Taylor's E-2 Cub, built with different engines as the F-2 through H-2, was refined into the J-2 and J-3 models by young engineer Walter Jamouneau, to Taylor's outrage. After 1200 J-2s, World War II caused the production of 20 000 J-3 Cubs, painted yellow for the screening of new military pilots by civilian flying schools, or olive green as frontline light observation and liaision aircraft, designated L-4 (initially O-59) by the US Army.

 

 
J-3C-65
length 6.79 m (22 ft 3 in)
span 10.75 m (35 ft 3 in)
engine 1 × Continental O-170, 65 hp
max take-off weight 499 kg (1100 lb)
max speed 148 km/h (92 mph)
capacity 2 persons
 
PA-18 Super Cub
FIRST FLIGHT 1949
An improved Cub, the PA-18 featured wing flaps and a more powerful engine, ranging from 90 to 180 hp. Like the Cub, the Super Cub enjoys popularity as a sporting aircraft, but was also produced as a military observation, liaison and training aircraft, known to the military as L-18 and L-21. PA-18 production did not finally end until 1994, and over 10 000 civil and military examples were built.

 

 
PA-18-150
length 6.88 m (22 ft 7 in)
span 10.73 m (35 ft 2 in)
engine 1 × Continental O-320, 150 hp
max take-off weight 794 kg (1750 lb)
max speed 208 km/h (130 mph)
capacity 2 persons
 
  REPUBLIC – United States
The Seversky Aircraf Corporation, renamed Republic Aviation in 1939, was established in 1931 at Farmingdale on Long Island, New York, by Russian-born Alexander de Seversky. Also from Russia, his chief engineer, Alexander Kartveli, created Republic's important lineage of 'Thunder' combat aircraft - the P-47, F-84 family, and F-105. Republic was acquired by Fairchild in 1965.
 
P-47 Thunderbolt
FIRST FLIGHT 1941
The heaviest single-engined fighter to see World War II action, the P-47 was built around a huge 18-cylinder engine and supercharger. It was fast, very fast in a dive, tough and heavily armed, but not overly manoeuvrable and expensive; yet it was the most numerous US fighter. Of 15 683 built, the major part served with the US Army
as escort fighters, interceptors and fighter-bombers.

 

 
P-47D
length 11.02 m (36 ft 2 in)
span 12.43 m (40 ft 9 in)
engine 1 × Pratt & Whitney R-2800 Double Wasp, 2535 hp
max take-off weight 7938 kg (17 500 lb)
max speed 686 km/h (426 mph)
capacity 1 person
 
F-84 Thunderjet
FIRST FLIGHT 1946
Despite its elegant appearance, the Thunderjet was a heavyweight among the early jets. Badly underpowered, the straight-winged fighter was mauled by the MiG-15 in the Korean War, and switched from the escort figher to the fighter-bomber role. In the latter capacity the F-84, especially the F-84G, was built in large numbers for the US and allied air forces. The F-84F is a different aircraft.

 

 
F-84G
length 11.61 m (38 ft 1 in)
span 11.09 m (36 ft 5 in)
engine 1 × Allison J35, 1 × 2540 kg (5600 lb) thrust
max take-off weight 10 670 kg (23 525 lb)
max speed 1000 km/h (622 mph)
capacity 1 person
 
F-84F Thunderstreak
FIRST FLIGHT 1950
A swept-wing Thunderjet derivative, the Thunderstreak retained little commonality when the fuselage was redesigned to accomodate a bigger engine. Despite this, its F-96 designation was changed to F-84F to ease funding. Like its predecesso, it wasn't much of a fighter and better suited as a fighter-bomber. Out of 2714 built, nearly half were supplied to European NATO nations.

 

 
RF-84F
length 13.22 m (43 ft 5 in)
span 10.24 m (33 ft 7 in)
engine 1 × Wright J65, 1 × 3275 kg (7220 lb) thrust
max take-off weight 12 701 kg (28 000 lb)
max speed 1118 km/h (695 mph)
capacity 1 person
 
RF-84F Thunderstreak
FIRST FLIGHT 1952
One Thunderstreak prototype was experimentally fitted with side air intakes, giving a slight decrease in thrust and speed, but freeing up space in the nose that was used for a battery of six cameras in the Thunderflash photo reconaissance derivative. 716 RF-84Fs were built. Under the FICON project, a converted RF-84F could be launched and picked up again later by a B-36 bomber.

 

 
RF-84F
length 14.51 m (47 ft 8 in)
span 10.24 m (33 ft 7 in)
engine 1 × Wright J65, 1 × 3538 kg (7800 lb) thrust
max take-off weight 12 156 kg (26 800 lb)
max speed 1093 km/h (679 mph)
capacity 1 person
 
F-105 Thunderchief
FIRST FLIGHT 1955
Enormous for a single-seat, single-engined aircraft, and very complex and expensive, the 'Thud' fighter-bomber was also nicknamed the 'One-Man Air Force'. Designed for nuclear strike missions, it spearheaded the US air fleet in the Vietnam War, and half of the 833 F-105s built were lost. F-105F two-seat trainers were converted to fly 'Wild Weasel' missions against surface-to-air missile sites. The last F-105 was retired from service in 1984.

 

 
F-105D
length 19.63 m (64 ft 5 in)
span 10.65 m (34 ft 11 in)
engine 1 × Pratt & Whitney J75, 1 × 12 020 kg (26 500 lb) thrust
max take-off weight 23 834 kg (52 546 lb)
max speed Mach 2.1 (2237 km/h / 1390 mph)
capacity 1 person
 
  ROBIN – France
In 1957, Pierre Robin and Jean Délémontez founded the Centre Est Aéronautique at Dijon-Darois to produce and further develop the Jodel light aircraft. CEA was renamed Avions Robin in 1969.
 
DR300 / DR400
FIRST FLIGHT 1968
Through the DR253, the Jodel DR200 was developed into the Robin DR300. The DR400 differs in having a forward-sliding cockpit canopy. Various models of these aircraft have been built, with names such as Petit Prince, Dauphin, Regent and Remorqueur. The DR400 remains in production, still utilizing the Jodel cranked wing and wooden construction. The DR500 has a wider fuselage.

 

 
DR400/180 Regent
length 6.96 m (22 ft 10 in)
span 8.72 m (28 ft 7 in)
engine 1 × Lycoming O-360, 180 hp
max take-off weight 1100 kg (2425 lb)
max speed 278 km/h (173 mph)
capacity 4 persons
 
  ROBINSON – United States
Based in Torrance, California, the Robinson Helicopter Company was founded in 1973 by former Bell and Hughes employee Frank Robinson. Building light, cheap types with piston engines, the firm can now claim to be the world's largest manufacturer of helicopters in terms of numbers.
 
R22
FIRST FLIGHT 1975
The small R22 isn't much more expensive to buy than a light aircraft, and is powered by a similar piston engine. Despite the loss of the prototype, hundreds were already on order when deliveries began in 1979, and over 4000 have now been built, models including the R22 Alpha and Beta. Its roles include helicopter pilot training and cattle herding at large ranches in the USA and Australia.

 

 
R22 Beta
fuselage length 6.30 m
  (20 ft 8 in)
rotor diam 7.67 m (25 ft 2 in)
engine 1 × Lycoming O-320, 131 hp
max take-off weight 620 kg (1370 lb)
max speed 180 km/h (111 mph)
capacity 2 persons
 
R44
FIRST FLIGHT 1990
Larger and faster than the R22, the R44 was designed to have a performance close to that of turbine-engined helicopter types against dramatically lower acquisition and maintenance costs. The original R44 Astro has now been replaced in production by the more refined Raven version. The Clipper model has fixed or inflatable floats.

 

 
R44 Raven II
fuselage length 6.76 m
  (21 ft 5 in)
rotor diam 10.06 m (33 ft 0 in)
engine 1 × Lycoming O-540, 245 hp
max take-off weight 1134 kg (2500 lb)
max speed 240 km/h (150 mph)
capacity 4 persons
 
  SAAB – Sweden
Based in Linköping, Saab (Svenska Aeroplan Aktiebolaget) was established in 1937 to produce aircraft for the Swedish Air Force. It later diversified into cars. With few export orders, Saab managed to create an impressive lineage of combat aircraft, from the Saab 17 in 1940 to today's Gripen. Training aircraft and three airliners, the Saab Scandia, 340 and 2000, were also built.
 
91 Safir
FIRST FLIGHT 1945
Designed by Anders Andersson, the Safir (Sapphire) followed the lines of his earlier Bücker Bestmann. 323 Safirs were produced as military or civil training aircraft, including 120 subcontracted to the Dutch De Schelde factory. The Saab 91A and B were three-seaters, while the 91C and more powerful D could carry four people.

 

 
91D
length 8.04 m (26 ft 4 in)
span 10.60 m (34 f 9 in)t
engine 1 × Lycoming O-360, 180 hp
max take-off weight 1205 kg (2657 lb)
max speed 265 km/h (165 mph)
capacity 4 persons
 
29 Tunnan
FIRST FLIGHT 1948
Sweden's first jet fighter was the converted Saab 21R, but Saab was quick to follow up with the advanced, swept-winged J29 that was among the world's fastest aircraft of its time, despite the tubby fuselage, housing a licence-built De Havilland Ghost centrifugal turbojet; it was nicknamed Flygande Tunnan (Flying Barrel). 661 J29 fighters and S29 reconnaissance aircraft were built, all for Swedish use, though 30 were later sold to Austria.

 

 
J29F
length 11.00 m (36 ft 1 in)
span 10.23 m (33 ft 7 in)
engine 1 × Volvo RM2, 1 × 2753 kg (6070 lb) thrust
max take-off weight 8375 kg (18 465 lb)
max speed 1060 km/h (660 mph)
capacity 1 person
 
32 Lansen
FIRST FLIGHT 1952
A fairly heavy aircraft designed for ground and maritime attack, powered by a single Volvo-built Rolls-Royce Avon engine, the Lansen (Lance) still had good performance, being able to exceed the speed of sound in a shallow dive. 84 A32 attack aircraft, 120 J32 night fighters, and 44 S32 photo recce aircraft were procured by Sweden.

 

 
J32E
length 14.65 m (48 ft 1 in)
span 13.00 m (42 ft 8 in)
engine 1 × Volvo RM6, 1 × 6500 kg (14 330 lb) thrust
max take-off weight 13 000 kg (28 660 lb)
max speed 1200 km/h (746 mph)
capacity 2 persons
 
35 Draken
FIRST FLIGHT 1955
Another tremendous achievement by Saab, the Draken (Dragon, or Dragon Kite), with its futuristic 'double delta' shape, was arguably superior to comparable fighters such as the F-104 Starfighter and Mirage III, but being from neutral Sweden it was exported only to Finland, Denmark and Austria. Over 600 Drakens were built, including a number of two-seat conversion trainers.

 

 
J35F
length 15.35 m (50 ft 4 in)
span 9.40 m (30 ft 10 in)
engine 1 × Volvo RM6, 1 × 8000 kg (17 650 lb) thrust
max take-off weight 12 270 kg (27 051 lb)
max speed Mach 2.0 (2125 km/h / 1320 mph)
capacity 1 person
 
105
FIRST FLIGHT 1963
Designated Sk60 by the Swedish military, the Saab 105
jet trainer is unusual in being able to carry four people, when not fitted with ejection seats, for use in a liaison role. Not surprisingly, it can also serve as a light attack aircraft. Sweden got 150, and Austria bought 40 105Ös fitted with more powerful General Electric J85 engines.

 

 
Sk60
length 10.50 m (34 ft 5 in)
span 9.50 m (31 ft 2 in)
engine 2 × Turboméca Aubisque, 2 × 743 kg (1640 lb) thrust
max take-off weight 4500 kg (9920 lb)
max speed 765 km/h (475 mph)
capacity 2-4 persons
 
37 Viggen
FIRST FLIGHT 1967
Saab's second Mach 2 fighter, the Viggen (Thunderbolt) featured another unusual layout, with foreplanes and a Pratt & Whitney JT8D airliner engine adapted by Volvo. Emphasis was laid on short take-off and landing (STOL) and fighter-bomber capability, though the AJ37 variants were followed by the JA37 interceptor. Including 18
Sk37 two-seat trainers, 329 Viggens were delivered
to the Swedish Air Force. After the end of the Cold War, defence cuts caused the Viggen's retirement by 2005.

 

 
AJ37
length 16.30 m (53 ft 6 in)
span 10.60 m (34 ft 9 in)
engine 1 × Volvo RM8, 1 × 11 800 kg (26 015 lb) thrust
max take-off weight 20 500 kg (45 194 lb)
max speed Mach 2.0 (2125 km/h / 1320 mph)
capacity 1 person
 
Safari / Supporter
FIRST FLIGHT 1969
Derived from the smaller MFI-9 Junior (licence-produced
by Bölkow as the Bo 208), the MFI-15 light aircraft was named Safari after the takeover of Malmö Flygindustri
by Saab. The MFI-17 military model, for training, liaison and even light attack, became the Supporter. The latter is designated T-17 by the Danish military, and entered
licence production in Pakistan as the MFI-17 Mushshak.
The MFI-395 Super Mushshak is an upgraded version.

 

 
Safari / Supporter
length 7.00 m (23 ft 0 in)
span 8.85 m (29 ft 0 in)
engine 1 × Lycoming O-360, 200 hp
max take-off weight 1200 kg (2646 lb)
max speed 236 km/h (147 mph)
capacity 2-3 persons
 
340
FIRST FLIGHT 1983
Originally designated SF340, the Saab 340 regional airliner was developed in conjunction with Fairchild, which produced the wing, tail and engine nacelles before pulling out in 1985. 159 Saab 340As and some 300 Saab 340Bs were built, the latter having slightly more powerful engines and larger tailplanes. Six Swedish Air Force aircraft carry a dorsal early warning radar. The Saab 2000 was developed from the 340.

 

 
340B
length 19.73 m (64 ft 9 in)
span 21.44 m (70 ft 4 in)
engine 2 × General Electric CT7, 2 × 1750 hp
max take-off weight 13 155 kg (29 000 lb)
max cruising speed 523 km/h (320 mph)
capacity 30-37 passengers
 
39 Gripen
FIRST FLIGHT 1988
Powered by a single, Volvo-built General Electric F404 engine, the JAS39 is a relatively light, compact Mach 2 fighter, ground attack and reconnaissance aircraft, and as such it has secured some export as well as Swedish orders, aided by the end of Sweden's neutral position, which also means, however, that the Gripen (Griffin) is likely the last Swedish fighter. A new version is offered as an alternative to the Lockheed Martin F-35, aka JSF.

 

 
JAS39C
length 14.10 m (46 ft 3 in)
span 8.40 m (27 ft 7 in)
engine 1 × Volvo RM12, 1 × 8170 kg (18 012 lb) thrust
max take-off weight 14 000 kg (30 865 lb)
max speed Mach 2.0 (2125 km/h / 1320 mph)
capacity 1 persoon
 
2000
FIRST FLIGHT 1992
A stretched Saab 340, the Saab 2000 has over twice the engine power installed and is the fastest propeller airliner in service, while still burning less fuel than jets. Propellers, however, are viewed as obsolete by the public, and airlines preferred to order the new regional jet aircraft, the Canadair CRJ and Embrear ERJ. 2000 production was halted in 1998, after only 64 aircraft.

 

 
2000
length 27.28 m (89 ft 6 in)
span 24.76 m (81 ft 3 in)
engine 2× Allison AE2100 , 2 × 4152 hp
max take-off weight 23 000 kg (50 706 lb)
max cruising speed 682 km/h (424 mph)
capacity 50-58 passengers
 
  SIAI-MARCHETTI – Italy
SIAI-Marchetti is an old Italian aircraft manufacturer from Varese, known as Savoia-Marchetti during its heyday in the 1930s. The firm has now been absorbed into the Aermacchi company.
 
SF.260
FIRST FLIGHT 1964
Designed by Stelio Frati, the SF.260 is a fully aerobatic three-seater which, though also sold to private pilots, has been built mainly as the SF.260M military trainer. The SF.260W Warrior version can be armed, and the SF.260TP version is powered by a 350-hp Alllison 250
turboprop engine replacing the Lycoming piston engine.
 
 
SF.260M
length 7.10 m (23 ft 4 in)
span 8.35 m (27 ft 5 in)
engine 1 × Lycoming O-540, 260 hp
max take-off weight 1360 kg (3000 lb)
max speed 340 km/h (190 mph)
capacity 3 persons
 
S.205 / S.208
FIRST FLIGHT 1965
A design by Alessandro Brena, the S.205 is a four-seat touring aircraft with fixed (S.205/F models) or retractable (S.205/R) landing gear. The S.208 has retractable gear and a more powerful engine, and can carry five people.
A number of S.208Ms were sold to the Italian Air Force which utilizes them as liaison aircraft and glider tugs.
 
 
S.208M
length 8.00 m (26 ft 3 in)
span 10.86 m (35 ft 8 in)
engine 1 × Lycoming O-540, 260 hp
max take-off weight 1500 kg (3307 lb)
max speed 320 km/h (199 mph)
capacity 5 persons
 
  SIKORSKY – United States
Russian engineer Igor Skorsky (1889-1972) built the world's first multi-engined aircaft in 1913. After the Russian Revolution he emigrated to the USA, where his initial focus lay on flying boats. Long interested in helicopters, Sikorksy built the world's first functional helicopter, the VS-300,
in 1939. Based in Stratford, Connecticut, Sikorsky Aircraft now specializes in larger helicopters.
 
S-51
FIRST FLIGHT 1943
The first helicopter in US military service, the two-seat
R-4 was developed into the refined R-6 and the four- seater R-5, company designation S-51. The US Army designation R-5 was changed to H-5, while the US Navy called it HO3S; the British named it Dragonfly, Westland producing a re-engined variant as the WS-51. The S-51 was utilized mainly for rescue work and various trials.

 

 
S-51
fuselage length 12.45 m
  (40 ft 10 in)
rotor diam 14.94 m (49 ft 2 in)
engine 1 × Pratt & Whitney R-985 Wasp Junior, 450 hp
max take-off weight 2495 kg (4500 lb)
max speed 166 km/h (103 mph)
capacity 4 persons
 
S-55
FIRST FLIGHT 1949
The S-55 was innovative in having its engine mounted
in the nose, allowing for the payload to be carried in the helicopter's centre of gravity, though the useful load was limited as in any piston-engined helicopter. The type was designated H-19 Chickasaw by the US Air Force, HO4S with the Navy, and HRS by the Marine Corps; the name Whirlwind applied to Westland-built airframes. Civil users included the Belgian airline, Sabena. Some S-55s and Whirlwinds were fitted with turbine engines.

 

 
H-19B Chickasaw
fuselage length 12.88 m
  (42 ft 3 in)
rotor diam 16.15 m (53 ft 0 in)
engine 1 × Wright R-1300 Cyclone, 700 hp
max take-off weight 3583 kg (7900 lb)
max speed 180 km/h (112 mph)
capacity 10 passengers
 
  STAMPE & VERTONGEN – Belgium
Stampe & Vertongen was established in Antwerp in 1922, to build training and touring aircraft designed by Alfred Renard, who left to start his own firm in 1927. After 1945 Renard's Brussels plant was used to relaunch production of the prewar SV.4. Stampe & Renard existed till 1970.
 
SV.4
FIRST FLIGHT 1933
Initially only a handful of SV.4s were sold for civil use, but shortly before World War II the Belgian Air Force took 30 of an improved version as elementary trainers. A large French military order was reconfirmed after 1945, and over 1000 Stampes were produced post-war, including another 65 aircraft, these having enclosed cockpits, for the Belgian Air Force. Today the Stampe is a celebrated classic biplane, many of them still remaining airworthy.
 
 
SV.4b
length 6.80 m (22 ft 4 in)
span 8.39 m (27 ft 6 in)
engine 1 × De Havilland Gipsy Major, 145 hp
max take-off weight 770 kg (1697 lb)
max speed 188 km/h (117 mph)
capacity 2 persons
 
  SUD-OUEST – France
In 1936, France's aircraft companies were nationalized into regional groups, including SNCASO or Sud-Ouest (Southwest). Sud-Ouest merged with Sud-Est in 1957, to form Sud Aviation.
 
SO.4050 Vautour
FIRST FLIGHT 1952
Following on the unsuccesful SO.4000 bomber, the SO.4050 Vautour (Vulture) was planned in three models: the single-seat Vautour IIA attack aircraft, the two-seat IIN night fighter, and tthe two-seat IIB bomber with a bombardier in a glazed nose. Limited numbers of each were built for the French Air Force, and the IIAs were sold to Israel which used them in the 1967 Six-Day War.
 
 
Vautour IIA
length 15.57 m (51 ft 2 in)
span 15.10 m (49 ft 7 in)
engine 2 × Snecma Atar, 2 × 3500 kg (7716 lb) thrust
max take-off weight 21 000 kg (46 297 lb)
max speed 1100 km/h (687 mph)
capacity 1 person
 
  TACHIKAWA – Japan
In 1924, the Ishikawa shipyard established an aircraft manufacturing subsidiary of the same name in Tachikawa, near Tokyo. It was taken over by the Japanese Army in 1936, and renamed Tachikawa. The company was reconstituted after World War II, but turned away from aviation.
 
Ki-36 / Ki-55
FIRST FLIGHT 1938
The Ki-36 was an all-metal two-seat reconnaissance and light attack aircraft, used with some success by the Japanese Army in China, where there were few enemy fighters. Having good handling characteristics, the design was employed also, with minor changes, as an advanced trainer, the trainer version being designated
Ki-55. 1344 Ki-36s and 1389 Ki-55s were constructed.

 

 
Ki-36
length 8.00 m (25 ft 3 in)
span 11.80 m (38 ft 9 in)
engine 1 × Hitachi Ha-13, 510 hp
max take-off weight 1660 kg (3660 lb)
max speed 348 km/h (216 mph)
capacity 2 persons
 
  TRANSALL – France / Germany
The Transall C-160 transport aircraft was designed and built by Transall (Transporter Allianz), a consortiom of French and German companies: Nord Aviation, Hamburger Flugzeugbau and VFW.
 
C-160
FIRST FLIGHT 1963
Smaller than a Lockheed C-130 Hercules, the Transall military transport aircraft can carry freight or vehicles with a maximum weight of 16 000 kg (35 270 lb), 93 troops, or 62 stretcher cases and four attendants. Just over 200 were built, mostly for the German and French armed forces. The two French C-160H aircraft are equipped with long trailing antennae to maintain communications with France's nuclear ballistic missile submarines.

 

 
C-160
length 32.40 m (106 ft 4 in)
span 40.00 m (131 ft 3 in)
engine 2 × Rolls-Royce Tyne, 2 × 6100 hp
max take-off weight 51 000 kg (112 435 lb)
max speed 513 km/h (319 mph)
capacity 93 passengers
 
  TUPOLEV – Russia
Leading designer Andrei Tupolev (1888-1972) built the Sovet Union's first all-metal plane in 1924 and went on to construct a diversity of aicraft, including the giant ANT-20. A victim of Stalin's paranoia, he worked in imprisonment for several years. After World War II his Moscow-based design bureau, led by his son Alexei from 1963, concentrated on heavy bombers and airliners. The Tupolev company has become a division of OAK, the United Aircraft Corporation as of 2006.
 
SB
FIRST FLIGHT 1934
SB stood for Fast Bomber in Russian, and this modern light bomber, also known as ANT-40 and developed from the ANT-29 heavy fighter, surprised the world with its speed when it turned up in the Spanish Civil War. When intercepted, though, it was vulnerable, and it was obsolete when Germany invaded the Soviet Union. No less than 7000 SBs were built, the final, 1941 version having the designation Ar-2 for Alexander Arkhangelsky, Tupolev's deputy and leader of the SB's design team.

 

 
SB 2M-103
length 12.57 m (41 ft 3 in)
span 20.33 m (66 ft 8 in)
engine 2 × Klimov VK-103, 2 × 960 hp
max take-off weight 7880 kg (17 370 lb)
max speed 450 km/h (280 mph)
capacity 3 persons
 
Tu-2
FIRST FLIGHT 1941
While imprisoned Andrei Tupolev was ordered to design a bomber better than the German Ju 88, and the result was an advanced aircraft that eventually entered service as the Tu-2 in 1942. 2500 Tu-2s were built, the majority after 1945. The type saw action in the Korean War, and remained in Chinese service for many years thereafter. A jet bomber of 1947, the Tu-12, was based on the Tu-2.

 

 
Tu-2S
length 13.80 m (45 ft 3 in)
span 18.86 m (61 ft 11 in)
engine 2 × Shvetsov ASh-82, 2 × 1850 hp
max take-off weight 11 450 kg (25 243 lb)
max speed 550 km/h (342 mph)
capacity 4 persons
 
  UTVA – Serbia
Utva is a small manufacturer of light aircraft . Its factory in Pančevo was damaged in the 1999 NATO air strikes. The Lasta trainer, first flown in 1985, remains in the development phase.
 
75
FIRST FLIGHT 1976
The Utva 75 is a two-seat elementary trainer for civil and military use. Almost 140 examples were built, and small numbers are in use with military air arms and aeroclubs in the former Yugoslavia. The four-seat Utva 75A and the agricultural 75Ag models were not built in any numbers.

 

 

 
75
length 7.11 m (23 ft 4 in)
span 9.73 m (31 ft 11 in)
engine 1 × Lycoming O-360, 180 hp
max take-off weight 960 kg (2116 lb)
max speed 215 km/h (133 mph)
capacity 2 persons
 
  VFW – Germany
Vereinigte Flugtechnische Werke (United Aerotechnical Works) in Bremen was created by the merger of Focke-Wulf and Weserflug in 1961. In 1969 VFW and Fokker formed Fokker-VFW, but the unsuccesful combination was dissolved in 1980 and VFW was then taken over by MBB.
 
614
FIRST FLIGHT 1971
The VFW 614 was a small short-range airliner powered by jet engines that were unusally placed above the wing. The especially developed M45H engine gave problems, and the aircraft proved too expensive to acquire for the small airlines it was intended for. Only 14 VFW 6154s were built, some ending up with the German Air Force.

 

 
614
length 20.60 m (67 ft 7 in)
span 21.50 m (70 ft 6 in)
engine 2 × Rolls-Royce / Snecma M45H,
  2 × 3311 kg (7300 lb) thrust
max take-off weight 19 958 kg (44 000 lb)
max cruising speed 705 km/h (438 mph)
capacity 40-44 passengers
 
  VOUGHT – United States
Birdseye Lewis and Chance Vought established the Lewis and Vought Corporation in Astoria, New York, in 1917. It moved to Long Island in 1919. After his partner retired in 1922, Vought died in 1930, but the company bearing his name has existed through several incarnations until today. Vought Aircraft Industries currently produces airframe components for other manufacturers.
 
O2U / O3U Corsair
FIRST FLIGHT 1926
The first of three Vought aircraft to be named Corsair was a US Navy scout and observation biplane built in landplane, floatplane and amphibious floatplane forms for aircraft carriers and shore stations. O2U versions were superseded by improved O3U models from 1930, these being designated SU by the US Marine Corps.
Export models carried the V-65 and V-93 designations.

 

 

 
SU-4
length 8.37 m (27 ft 6 in)
span 10.97 m (36 ft 0 in)
engine 1 × Pratt & Whitney R-1690 Hornet, 600 hp
max take-off weight 2161 kg (4765 lb)
max speed 269 km/h (167 mph)
capacity 2 persons
 
F4U Corsair
FIRST FLIGHT 1940
The best carrier-capable fighter and fighter-bomber of World War II, the remarkable, gull-winged F4U entered combat in 1943, but didn't start operating from aircraft carriers until 1944 because of worries about the pilot's limited view over the long nose. Production continued until 1952 and totalled over 12 500, including Goodyear- built aircraft designated FGs and Brewster-made F3As.

 

 

 
F4U-1D
length 10.16 m (33 ft 4 in)
span 12.47 m (40 ft 11 in)
engine 1 × Pratt & Whitney R-2800 Double Wasp, 2000 hp
max take-off weight 6350 kg (14 000 lb)
max speed 671 km/h (417 mph)
capacity 1 person
 
  VULTEE – United States
In 1932, automobile manufacturer Erett Cord set up an aircraft company in the Los Angeles area to manufacture the V-1, an all-metal singled-engined airliner designed by Gerard 'Jerry' Vultee.
Renamed Vultee Aircraft in 1939, the firm merged with Consolidated to form Convair in 1943.
 
BT-13 Valiant
FIRST FLIGHT 1939
Nicknamed 'Vibrator', because it would shake violently when flying at the minimum speed, the BT-13 was the US basic training aircraft during World War II. Students would fly an elementary trainer first, the BT-13 next and finally, the AT-6 Texan. The BT-13's US Navy designation was SNV. The BT-15 variant had a Wright R-975 engine.

 

 

 
BT-13
length 8.79 m (28 ft 10 in)
span 12.80 m (42 ft 0 in)
engine 1 × Pratt & Whitney R-985 Wasp Junior, 450 hp
max take-off weight 2039 kg (4496 lb)
max speed 290 km/h (180 mph)
capacity 2 persons
 
  WESTLAND – United Kingdom
Westland Aircraft Works in Yeovilton, in Somerset, was established in 1915. After World War II the company concentrated on helicopters, having reached a licensing agreement with Sikorsky.
In 2000 it merged with its Italian partner in the AW101 programme, to form Agusta Westland.
 
Scout
FIRST FLIGHT 1960
The Scout was developed from the Saunders-Roe P.531 prototype, which itself evolved from the piston-engined Skeeter. Some 150 Scouts were produced for the British Army as observation, liaison and light attack helicopters; machine guns and anti-tank missiles could be fitted. The type was used in conflict areas, including Northern Ireland and the Falklands. The Wasp is a naval version.

 

 
Wasp AH.1
fuselage length 9.24 m
  (30 ft 4 in)
rotor diam 9.83 m (32 ft 3 in)
engine 1× Rolls-Royce Nimbus, 685 hp
max take-off weight 2405 kg (5300 lb)
max speed 211 km/h (131 mph)
capacity 5 persons
 
Wasp
FIRST FLIGHT 1962
For operations from small frigate decks, the Royal Navy ordered a naval version of the Scout with a four-wheel undercarriage replacing its skids. It did not have sonar equipment of its own, but could carry two anti-submarine torpedoes, or alternatively, light anti-ship missiles, three personnel or one stretcher. 133 Wasps were produced, including small numbers for export to several nations.

 

 
Wasp HAS.1
fuselage length 9.24 m
  (30 ft 4 in)
rotor diam 9.83 m (32 ft 3 in)
engine 1× Rolls-Royce Nimbus, 710 hp
max take-off weight 2495 kg (5500 lb)
max speed 193 km/h (120 mph)
capacity 5 persons
 
Sea King
FIRST FLIGHT 1969
The British variant of the Sikorsky-conceived S-61/H-3,
the Westland Sea King has been buit in anti-submarine
and search and rescue models for the Royal Navy and military export customers. A transport model was named Commando by Westland, and Sea King HC.4 by the Royal Navy. The Sea King AEW.5 carrying early warning radar was developed hastily for the 1982 Falklands War.

 

 
Sea King HC.4
fuselage length 17.01 m
  (55 ft 10 in)
rotor diam 18.90 m (62 ft 0 in)
engine 2 × Rolls-Royce Gnome, 2 × 1590 hp
max take-off weight 9526 kg (21 000 lb)
max speed 225 km/h (140 mph)
capacity 28 passengers
 
Lynx
FIRST FLIGHT 1971
One of the helicopters developed under an Ango-French agreement, the fast, agile Lynx is used by many navies and the British Army, but the French Army cancelled it and it failed to sell on the civil market. The British Army received 114 Lynx AH.1s with skid landing gears for use in the light transport and anti-tank roles. They have been upgraded to AH.7 standard, receiving uprated engines and larger main and tail rotors. The few Lynx AH.9s are fitted with the wheeled undercarriage of the naval Lynx.
 
 
Lynx AH.1
fuselage length 12.06 m
  (39 ft 7 in)
rotor diam 12.80 m (42 ft 0 in)
engine 2 × Rolls-Royce Gem, 2 × 900 hp
max take-off weight 4535 kg (10 000 lb)
max cruising speed 269 km/h (167 mph)
capacity 11 persons
 
Lynx HAS.2
FIRST FLIGHT 1972
The naval variant of the Lynx, the initial version of which was the Lynx HAS.2 for the British and French navies, is fitted with a wheeled undercarriage to ease shipboard use. Various versions are now in use with 16 countries, mainly in an anti-submarine capacity or, like the British
Lynx HMA.8, in an anti-surface vessel role. Upgraded engines and rotors are often installed. The illustrated version is designated SH-14D by the Netherlands Navy.
 
 
Lynx HAS.2
fuselage length 11.92 m
  (39 ft 1 in)
rotor diam 12.80 m (42 ft 0 in)
engine 2 × Rolls-Royce Gem, 2 × 900 hp
max take-off weight 4765 kg (10 500 lb)
max cruising speed 230 km/h (145 mph)
capacity 11 persons
 
  XIAN – China
Established in 1958, the state aircraft factory in the city of Xian was tasked with copying the Tupolev Tu-16 bomber and the Antonov An-24 transport aircraft. Xian has developed its own versions of the Antonov, as well as an indigenous attack bomber, the JH-7 Flying Leopard.
 
Y-7 / MA60
FIRST FLIGHT 1970
The Antonov An-24 was copied without a licence at Xian as the Y-7, which entered service with China's state airline in the mid-1980s. A rear-loading cargo model similar to the An-26 is known as the Y-7H (initially Y-14). The MA60 (Modern Ark 60) stretched 60-passenger variant is fitted with Western engines and equipment.

 

 
MA60
length 24.31 m (81 ft 0 in)
span 29.20 m (95 ft 11 in)
engine 2 × Pratt & Whitney Canada PW127, 2 × 2880 hp
max take-off weight 21 800 kg (48 060 lb)
max speed 514 km/h (319 mph)
capacity 60 passengers
 
  YAKOVLEV – Russia
Alexander Yakovlev (1906-1989) was one of the Soviet Union's great aircraft designers, getting his own design bureau, located at State Aviation Factory 115 in Moscow, in 1934. As of 2006 the Yak Aircraft Corporation has become the Yak division of OAK, or United Aircraft Corporation.
 
Yak-3
FIRST FLIGHT 1943
One of the best fighters of World War II, the lightweight Yak-3, the second design to use this designation, was a refined variant of the Yak-1. Optimized for aerial combat at lower altitudes, the Yak-3 made a formidable foe for the German Luftwaffe over the Eastern Front battlefields. 5000 Yak-3s were built, followed in the 1990s by a small batch of new Yak-3UAs manufactured for enthousiasts.

 

 

 
Yak-3
length 8.49 m (27 ft 11 in)
span 9.20 m (30 ft 2 in)
engine 1 × Klimov VK-105, 1620 hp
max take-off weight 2550 kg (5622 lb)
max speed 655 km/h (407 mph)
capacity 1 person
 
Yak-11
FIRST FLIGHT 1946
In 1945 Yakovev built a radial-engined all-metal version of the Yak-3, the Yak-3U. A two-seat trainer version, the Yak-3UTI, was put into production in refined form as the Yak-11, which became the communist world's standard advanced trainer. 4500 examples were built, including 700 by Let in Czechoslovakia with the C-11 designation. The Yak-11U / C-11U version featured a nose landing gear. The Yak-11 was known as Moose to NATO pilots.

 

 

 
Yak-11
length 8.20 m (26 ft 11 in)
span 9.40 m (30 ft 10 in)
engine 1 × Shvetsov ASh-21, 700 hp
max take-off weight 2440 kg (5379 lb)
max speed 465 km/h (289 mph)
capacity 2 persons
 
Yak-40
FIRST FLIGHT 1966
Long before regional jet airliners became popular in the West, the Soviet Union built just over 1000 examples
of this three-engined, straight-winged aircraft, which can use unpaved runways of 700 m (2297 ft). The central engine was intended to boost take-off performance, but is used throughout the flight in practice, fuel efficiency
is poor. Many Yak-40s are now utilized as private jets.
 
 
Yak-40
length 20.36 m (66 ft 10 in)
span 25.00 m (82 ft 0 in)
engine 3 × Ivchenko AI-25, 3 × 1500 kg (3307 lb) thrust
max take-off weight 16 000 kg (35 273 lb)
max cruising speed 550 km/h (342 mph)
capacity 33 passengers
 
Yak-42
FIRST FLIGHT 1975
Of similar configuration to the Yak-40 , the Yak-42 is a much larger and faster airliner, powered by turbofan engines. The sweep angle of its wing was increased during its protracted development, the Yak-42 entering service with Aeroflot in late 1980. Due to the collapse
of the Soviet Union only some 180 aircraft were built.
 
 
Yak-42D
length 36.38 m (119 ft 4 in)
span 34.88 m (114 ft 5 in)
engine 3 × Lotarev D-36, 3 × 1500 kg (14 300) thrust
max take-off weight 57 000 kg (125 700 lb)
max cruising speed 810 km/h (503 mph)
capacity 104-120 passengers
 
  ZLÍN – Czech Republic
Zlín is the brand name of the Moravan company, which has manufactured over 5000 light aicraft since 1934. Based in the city of Otrokovice, Moravan is currently owned by Irish investors.
 
Z-326 Trenér Master
FIRST FLIGHT 1957
The Z-326 Trenér Master elementary trainer was derived from the earlier Z-26 Trenér, introducing an electrically retractable undercarriage. The Z-526 version is nearly identical, the Z-Z26F being powered by an M137 engine. The ultimate Z-726 is powered by a supercharged M337. Single-seat Akrobat versions have also been produced.

 

 
Z-326
length 7.83 m (25 ft 8 in)
span 10.58 m (34 ft 9 in)
engine 1 × Walter Minor, 160 hp
max take-off weight 900 kg (1984 lb)
max speed 245 km/h (152 mph)
capacity 2 persons
 
Z-37 Čmelák
FIRST FLIGHT 1963
Under the design leadership of Ladislav Smrčekinne, development of the Čmelák (Bumblebee) cropduster was undertaken jointly by Moravan and Let. Some 700 were built, this number including some thirty Z-37Ts powered by a Walter M601 turbine engine. A mechanic may ride as a passenger in a cabin behind the cockpit.

 

 
Z-37
length 8.55 m (28 ft 1 in)
span 12.22 m (40 ft 1 in)
engine 1 × Avia M462, 380 hp
max take-off weight 1850 kg (4078 lb)
max speed 216 km/h (134 mph)
capacity 2 persons