Airbus A310 Seats

Airbus A310 has a maximum seat capacity of 200 seats. SEATMAESTRO has actually in data base seat maps for 3 aircrafts and for 5 among which Adria Airways. Choosing the best seat on Airbus A310 will also depend on the airlines configuration of seats and different the class offered onboard. We recommend once using our general information for best aircraft seats on Airbus A310 that you also consider taking notice of the seat maps of the airline by aircraft.

Class	Pitch	Seats	Recline
Business Class	n/a	19	n/a
Economy Class	n/a	200	n/a
Economy Class	n/a	176	n/a

Seats
2-5 A,K : This seat has all the pros and perks of a standard Business class seat as well as good views (weather and flight time depending).
2-5 A,K : This seat has all the pros and perks of a standard Business class seat and it is easy to get out of if you are in a rush to get off the plane or to go to the loo.
7,8 A,K : Good views (weather and flight time depending). No one will be climbing past you to get in and out of their seat.
7,8 B,D,G, : Easy to get out of if you are in a rush to get off the plane or to go to the loo!
7,8 E,F : No view but then no bumps from trolleys.
6 A,K : Good views (weather and flight time depending). No one will be climbing past you to get in and out of their seat. You will get extra legroom.
6 B,D,G,H : Easy to get out of if you are in a rush to get off the plane or to go to the loo! You will get extra legroom.
6 E,F : No view but then no bumps from trolleys. You will get extra legroom.

BAe 146-300 / AVRO RJ100

BAe 146-300 / AVRO RJ100

Regional Airliner

The British Aerospace BAe 146-300 / AVRO RJ100 is a four-engined regional airliner with a capacity of maximum 128 passengers produced by the British manufacturer British Aerospace (today BAE Systems). It is part of the BAe 146 / AVRO RJ family of regional airliner.

Crew	2
Passengers	100-116, max. 128
Propulsion	4 Turbofan Engines
Engine Model	Lycoming / Honeywell ALF 502R-5 (LF507-1F)
Engine Power (each)	31 (31,1) kN	6970 (7000)lbf
Speed	780 km/h	421 kts 484 mph
Mmo (max. Mach)	Mach 0.73
Service Ceiling	9.449 (10.668) m	31.000 (35.000) ft
Range	2.815 (2.759) km	1.520 (1.490) NM 1.749 (1.715) mi.
Empty Weight	24.880 (25.600) kg	54.850 (56.440) lbs
max. Takeoff Weight	45.132 (46.040) kg	99.500 (101.500) lbs
max. Landing Weight	39.236 (40.143) kg	86.500 (88.500) lbs
Wing Span	26,34 m	86,4 ft
Wing Area	77,3 m²	832 ft²
Length	30,99 m	101,7 ft
Height	8,59 m	28,2 ft
First Flight	01.05.1987 (13.05.1992)
Production Status	out of production
Production Range	1987-2003
Total Production	71 (71), Total 142
Developed from	BAe 146-100
ICAO Code	B463, RJ1H
FAA TCDS	A49EU
EASA TCDS	A.182
other TCDS	CAA UK BA16
Data for (Version)	BAe 146-300 (RJ100)
Variants	BAe 146-300, AVRO RJ100, BAe 146-300QC, BAe 146-300QT

Remarks
The BAe 146 was developed by Hawker Siddeley as the HS.146. The BAe 146-300 is a stretched variant of the BAe 146-100 (+4,81m / 15ft 8in). The AVRO RJ100 is a modernized variant which was introduced in 1992.

BAe 146-200 / AVRO RJ85

BAe 146-200 / AVRO RJ85
Regional Airliner
The British Aerospace BAe 146-200 / AVRO RJ85 is a four-engined regional airliner with a capacity of maximum 112 passengers produced by the British manufacturer British Aerospace (today BAE Systems). It is part of the BAe 146 / AVRO RJ family of regional airliner.

Crew	2
Passengers	85-112
Propulsion	4 Turbofan Engines
Engine Model	Lycoming / Honeywell ALF 502R-5 (LF507-1F)
Engine Power (each)	31 (31,1)kN	6970 (7000)lbf
Speed	780 km/h	421 kts 484 mph
Mmo (max. Mach)	Mach 0.73
Service Ceiling	9.449 (10.668) m	31.000 (35.000)ft
Range	2.908 (2.963) km	1.570 (1.600) NM 1.807 (1.841) mi.
Empty Weight	23.882 (24.603) kg	52.650 (54.240) lbs
max. Takeoff Weight	42.184 (43.998) kg	93.000 (97.000) lbs
max. Landing Weight	36.741 (38.555) kg	81.000 (85.000) lbs
Wing Span	26,34 m	86,4 ft
Wing Area	77,3 m²	832 ft²
Length	28,55 m	93,7 ft
Height	8,61 m	28,2 ft
First Flight	01.08.1982 (23.03.1992)
Production Status	out of production
Production Range	1983-2003
Total Production	116 (87), Total 203
Developed from	BAe 146-100
ICAO Code	B462, RJ85
FAA TCDS	A49EU
EASA TCDS	A.182
other TCDS	CAA UK BA16
Data for (Version)	BAe 146-200 (RJ85)
Variants	BAe 146-200, AVRO RJ85, BAe 146-200QC, BAe 146-200QT

RemarksThe BAe 146 was developed by Hawker Siddeley as the HS.146. The BAe 146-200 is a stretched variant of the BAe 146-100 (+2,36m / 7ft 9in).The AVRO RJ85 is a modernized variant which was introduced in 1992.

BAe 146-100 / AVRO RJ70

BAe 146-100 / AVRO RJ70

Regional Airliner

The British Aerospace BAe 146-100 / AVRO RJ70 is a four-engined regional airliner with a capacity of maximum 94 passengers produced by the British manufacturer British Aerospace (today BAE Systems). It is part of the BAe 146 / AVRO RJ family of regional airliner.

Crew	2
Passengers	70-94
Propulsion	4 Turbofan Engines
Engine Model	Lycoming / Honeywell ALF 502R-5 (LF507-1F)
Engine Power (each)	31 (31,1)kN	6970 (7000)lbf
Speed	780 km/h	421 kts 484 mph
Mmo (max. Mach)	Mach 0.73
Service Ceiling	9.449 (10.668) m	31.000 (35.000) ft
Range	3.000 (3.074) km	1.620 (1.660) NM 1.864 (1.910) mi.
Empty Weight	23.288 (23.900) kg	51.341 (52.690)lbs
max. Takeoff Weight	38.102 (43.091) kg	84.000 (95.000)lbs
max. Landing Weight	35.153 (37.875) kg	77.500 (83.500) lbs
Wing Span	26,34 m	86,4 ft
Wing Area	77,3 m²	832 ft²
Length	26,16 m	85,8 ft
Height	8,61 m	28,2 ft
First Flight	03.09.1981 (23.06.1992)
Production Status	out of production
Production Range	1983-2003
Total Production	35 (12), Total 47
ICAO Code	B461, RJ70
FAA TCDS	A49EU
EASA TCDS	A.182
other TCDS	CAA UK BA16
Data for (Version)	BAe 146-100A (RJ70)
Variants	BAe 146-100, AVRO RJ70, BAe 146-100QC, BAe 146-100QT, BAe 146 Statesman

Remarks
The BAe 146 was developed by Hawker Siddeley as the HS.146. The AVRO RJ70 is a modernized variant which was introduced in 1992.

BAe 125-1000 / Hawker 1000

 

The BAe 125-1000 / Hawker 1000 is a twin-engined long-range corporate travel jet aircraft for max. 15 passengers produced by the British manufacturer BAe, British Aerospace and later by the US-American manufacturer Raytheon, today Hawker Beechcraft.

Crew	2
Passengers	15
Propulsion	2 Turbofan Engines
Engine Model	Pratt & Whitney Canada PW305
Engine Power (each)	23,2kN	5222lbf
Speed	867 km/h	468kts 539 mph
Service Ceiling	13.106 m	43.000ft
Range	6.375 km	3.442 NM 3.961 mi.
Empty Weight	7.629 kg	16.819lbs
max. Takeoff Weight	14.061 kg	31.000lbs
Wing Span	15,66 m	51,4ft
Wing Area	34,8 m²	375ft²
Length	16,42 m	53,9ft
Height	5,21 m	17,1ft
First Flight	16.06.1990
Production Status	out of production
Total Production	52
EASA TCDS	A.085
Data for (Version)	BAe 125-1000

Remarks
The BAe 125-1000 is a stretched long-range development of the BAe 125-800.

BAe 125-800 / Hawker 800

The BAe 125-800 / Hawker 800 is a series of twin-engined corporate jet aircraft for max. 15 passengers produced by the British manufacturer BAe, British Aerospace and later by the US-American manufacturer Raytheon, today Hawker Beechcraft. The BAe 125-800 series include the BAe 125-800 / Hawker 800 (BAe.125 Series 800A & Series 800B), the Hawker Beechcraft Hawker 800XP, Hawker 850XP, Hawker 900XP and the Hawker 750. The Hawker U-125A is a search and rescue (SAR) variant for the Japan Air Self Defense Force.

Crew	2
Passengers	8-14
Propulsion	2 Turbofan Engines
Engine Model	AlliedSignal TFE-731-5BR1H
Engine Power (each)	20,7kN	4654lbf
Speed	845 km/h	456kts 525 mph
Mmo (max.Mach)	Mach 0.80
Service Ceiling	12.497 m	41.000ft
Range	4.430 km	2.392 NM 2.753mi.
Empty Weight	7.075 kg	15.598lbs
max. Takeoff Weight	12.700 kg	28.000lbs
Wing Span	15,66 m	51,4ft
Wing Area	34,8 m²	375ft²
Length	15,60 m	51,2ft
Height	5,36 m	17,6ft
First Flight	26.05.1983 (HS 125-800)
Production Status	in production
Developed from	Hawker-Siddeley / BAe HS-125, DeHavilland D.H.125
FAA TCDS	A3EU
EASA TCDS	A.085
Data for (Version)	Hawker 800XP
Variants	BAe.125 Series 800A, Series 800B, Hawker 800, Hawker 800XP, Hawker 850XP, Hawker 900XP, Hawker 750, U-125, U-125A

Remarks
The BAe 125-800 is a development of the earlier Hawker Siddeley HS.125 (British Aerospace BAe 125) and is the successor of the BAe 125-700. The BAe 125-800 / Hawker 800 differs from the BAe 125-700 in the following major respects: new Garrett/AlliedSignal TFE 731-5R engines, increased wing span, new avionics including EFIS (Electronic Flight Instrument System), higher certified weights and a higher speed. The Hawker 800XP is equipped with more powerful AlliedSignal TFE 731-5BR engines. The Hawker 850XP differs from the Hawker 800XP by addition of winglets on the outboard wings. The Hawker 900XP is equipped with Honeywell TFE731-50R engines and new avionics equipment and offers a longer range. The Hawker 750 differs from the Hawker 800XP by having an external baggage unit in place of the aft ventral fuel tank. The range and MTOW is less than that of the Hawker 800XP as a result of the decrease in available fuel. Current (2010) production models are the Hawker 750 and the Hawker 900XP.

BAe ATP

The BAe ATP is a twin-engined turboprop regional airliner with a capacity of maximum 72 passengers produced by the British manufacturer BAe, British Aerospace (today BAE Systems).

Crew	2
Passengers	max. 72
Propulsion	2 Turboprop Engines
Engine Model	Pratt & Whitney Canada PW126A
Engine Power (each)	1978 kW	2653 shp
Speed	493 km/h	266kts 306mph
Service Ceiling	7.620 m	25.000ft
Range	1.824 km	985 NM 1.134mi.
Empty Weight	14.193 kg	31.290lbs
max. Takeoff Weight	22.930 kg	50.552lbs
Wing Span	30,63 m	100,5 ft
Wing Area	78,3 m²	843 ft²
Length	26,00 m	85,3 ft
Height	7,14 m	23,4 ft
First Flight	01.04.1984
Production Status	out of production
Total Production	64
Developed from	Hawker Siddeley HS 748
Data for (Version)	BAe ATP

Remarks
The ATP -(A)dvanced (T)urbo (P)rop- is a development of the Hawker Siddeley HS 748.

BAe Jetstream 41

The BAe Jetstream 41 is a twin-engined turboprop regional airliner with a capacity of maximum 29 passengers produced by the British manufacturer BAe, British Aerospace (BAE Systems).

Crew	2
Passengers	max. 29
Propulsion	2 Turboprop Engines
Engine Model	Garrett TPE331-14GR/HR
Engine Power (each)	1100 kW	1475shp
Speed	480 km/h	259kts 298mph
Service Ceiling	7.925 m	26.000ft
Range	1.433 km	774 NM 891 mi.
Empty Weight	6.416 kg	14.145lbs
max. Takeoff Weight	10.886 kg	24.000lbs
Wing Span	19,25 m	63,2ft
Wing Area	32,4 m²	349ft²
Length	18,85 m	61,8ft
Height	5,74 m	18,8ft
First Flight	25.09.1991
Production Status	out of production
Total Production	103
Developed from	BAe Jetstream 31
Data for (Version)	BAe Jetstream 41

Remarks
The Jetstream 41 is a stretched development of the BAe Jetstream 31.

Handley Page Jetstream / BAe Jetstream 31

The Handley Page Jetstream / BAe Jetstream 31 is a twin-engined turboprop regional airliner and corporate aircraft with a capacity of maximum 19 passengers produced by the British manufacturer Handley Page, later Scottish Aviation and finally BAe, British Aerospace (today BAE Systems).

Crew	2
Passengers	max. 19
Propulsion	2 Turboprop Engines
Engine Model	Garrett TPE331-10
Engine Power (each)	671 kW	900shp
Speed	487 km/h	263kts 303mph
Service Ceiling	9.632 m	31.600ft
Range	780 km	421 NM 484 mi.
Empty Weight	3.450 kg	7.606lbs
max. Takeoff Weight	6.600 kg	14.551lbs
Wing Span	15,85 m	52,0ft
Wing Area	25,1 m²	270ft²
Length	14,36 m	47,1ft
Height	5,32 m	17,5ft
First Flight	28.03.1980
Production Status	out of production
Total Production	386

BAC 167 Strikemaster

The BAC 167 Strikemaster is a single-engine two-seat ground-attack and trainer jet aircraft produced by the British manufacturer BAC, British Aircraft Corporation.

Crew	2
Propulsion	1 Turbojet Engine
Engine Model	Rolls-Royce Viper Mk 535
Engine Power	15,2kN	3417lbf
max. Speed (vne)	833 km/h	450kts 518 mph
Service Ceiling	12.192 m	40.000ft
Range	1.450 km	783 NM 901 mi.
Empty Weight	2.810 kg	6.195lbs
max. Takeoff Weight	5.216 kg	11.500lbs
Wing Span	11,23 m	36,8ft
Wing Area	19,9 m²	214 ft²
Length	10,27 m	33,7ft
Height	3,34 m	11,0ft
First Flight	26.10.1967
Production Status	out of production
Total Production	146
Developed from	Hunting / BAC Jet Provost
Data for (Version)	BAC 167 Strikemaster

Remarks
The 167 Strikemaster is a direkt development of the Hunting-Percival / BAC Jet Provost.

BAC One-Eleven (1-11)

The BAC One-Eleven (1-11) is a twin-engined regional airliner with a capacity of maximum 119 passengers produced by the British manufacturer BAC, British Aircraft Corporation.

Crew	2
Passengers	max. 119
Propulsion	2 Turbofan Engines
Engine Model	Rolls-Royce Spey-2506 (Spey-25512)
Engine Power (each)	46,3 (58,8) kN	10409 (12544) lbf
Speed	885 (891) km/h	478 (481)kts 550 (554) mph
Service Ceiling	10.668 m	35.000ft
Rate of climb	762 m/min	2500 ft/min
Range	2.321 (2.745) km	1.253 (1.482) NM 1.442 (1.705)mi.
Empty Weight	20.473 (24.900) kg	45.135 (54.895)lbs
max. Takeoff Weight	33.793 (47.200) kg	74.501 (104.058) lbs
Wing Span	27,00 (28,50) m	88,6 (93,5)ft
Wing Area	93,2 (95,8) m²	1003 (1031)ft²
Length	28,20 (32,61) m	92,5 (107,0)ft
Height	7,20 (7,42) m	23,6 (24,3)ft
First Flight	20.08.1963
Production Status	out of production
Production Range	1963-1989
Total Production	244
EASA TCDS	A.188
Data for (Version)	BAC 1-11 Series 200 (Series 500)
Variants	One-Eleven Series 200 / 300 / 400 / 475 / 500 / Rombac One-Eleven Series 560

Remarks
The 1-11 was also produced by in small numbers (nine) in Romania as Rombac One-Eleven.

Snow / Ayres S-2

 

The Snow / Ayres S-2 is a single-engine single-seat agricultural aircraft developed by Leland Snow. Production was run by several US-American manufacturers. First Production as S-2 by Snow Aeronautical, later by Rockwell Aero Commander Division as S-2D Ag Commander. Then produced by Rockwell as Thrush Commander 600 & 800. Between 1977 and 2003 production by Ayres as S-2R / S-2R-T. Today in production by Thrush Aircraft as Thrush.

Crew	1
Propulsion	1 Radial Engine (Turboprop)
Engine Model	Pratt & Whitney (Pratt & Whitney Canada) R-1340-AN1 Wasp (PT6A-34AG)
Engine Power	447 (559) kW	600(750)hp
Speed	256 (306) km/h	138(165)kts 159(190)mph
Service Ceiling	4.572 (3.658) m	15.000(12.000)ft
Range	648 km	350 NM 403 mi.
Empty Weight	1.678 (1.633) kg	3.700(3.600lbs
max. Takeoff Weight	2.722 (4.309) kg	6.000(9.500lbs
Wing Span	13,51 (13,54) m	44,3 (44,4)ft
Wing Area	30,3 m²	326 ft²
Length	8,95 (10,06) m	29,4 (33,0)ft
Height	2,79 m	9,2ft
First Flight	1956
Production Status	in production
Total Production	ca. 1700
EASA TCDS	A.040
Data for (Version)	Rockwell S-2D Thrush Commander 600 (S2R-T 660)

Remarks
Until 2007 approx. total production of 1700 S-2.

Avro Canada CF-100 Canuck

The Avro Canada CF-100 Canuck is a twin-engined two-seat all-weather interceptor jet fighter aircraft produced by the Canadian manufacturer Avro Aircraft Limited (Canada).

Crew	2
Propulsion	2 Turbojet Engines
Engine Model	Avro Canada Orenda 11
Engine Power (each)	32,5 kN	7306lbf
Speed	1046 km/h	565kts 650 mph
Service Ceiling	16.459 m	54.000ft
Range	2.093 km	1.130 NM 1.300 mi.
Empty Weight	10.478 kg	23.100lbs
max. Takeoff Weight	16.783 kg	37.000lbs
Wing Span	17,68 m	58,0ft
Wing Area	54,9 m²	591ft²
Length	16,48 m	54,1ft
Height	4,74 m	15,6ft
First Flight	19.01.1950
Production Status	out of production
Total Production	692
Data for (Version)	Avro Canada CF-100 Mk 5 Canuck

Remarks
The Avro Canada Canuck was the sole canadian mass production fighter aircraft. The Canuck was in service with the Canadian Forces and the Belgian Air Force.

AVRO 698 Vulcan

 

The AVRO 698 Vulcan is a four-engine delta-wing subsonic long-range strategic bomber aircraft produced by the British manufacturer AVRO, A.V. Roe and Company. The Vulcan was one of the three V-Bombers (Vulcan, Valiant und Victor) of the Royal Air Force.

Crew	5
Propulsion	4 Turbojet Engines
Engine Model	Rolls-Royce Olympus 301
Engine Power (each)	89 kN	20000lbf
Speed	1037 km/h	560kts 644 mph
Service Ceiling	19.812 m	65.000ft
Range	7.408 km	4.000 NM 4.603 mi.
Empty Weight	37.908 kg	83.573lbs
max. Takeoff Weight	113.398 kg	250.000lbs
Wing Span	33,83 m	111,0ft
Wing Area	368,3 m²	3964 ft²
Length	30,45 m	99,9 ft
Height	8,28 m	27,2 ft
First Flight	30.08.1952
Production Status	out of production
Production Range	1956-1965
Total Production	136
Data for (Version)	Avro 698 Vulcan B Mk.2

Remarks
The AVRO Vulcan was the world's first operational delta-wing bomber aircraft. After their service as a bomber six Vulcan have been converted to Vulcan K. Mk 2 tanker aircraft.

AVRO 696 Shackleton

The AVRO 696 Shackleton is a four-engine long-range maritime patrol aircraft produced by the British manufacturer AVRO, A.V. Roe and Company. The Shackleton was also used as an Airborne Early Warning (AEW) aircraft.

Crew	10
Propulsion	4 Piston Engines
Engine Model	Rolls-Royce Griffon 57A
Engine Power (each)	1831 kW	2455hp
Speed	485 km/h	262kts 302 mph
Service Ceiling	5.669 m	18.600ft
Range	4.260 km	2.300 NM 2.647 mi.
Empty Weight	26.218 kg	57.800lbs
max. Takeoff Weight	44.452 kg	98.000lbs
Wing Span	36,52 m	119,8ft
Wing Area	132,0 m²	1421ft²
Length	28,19 m	92,5ft
Height	7,11 m	23,3ft
First Flight	09.03.1949
Production Status	out of production
Production Range	1951-1958
Total Production	185
Data for (Version)	Avro 696 Shackleton MR.3

</DIV>

Remarks
The AVRO Shackleton was developed on base of the AVRO 694 Lincoln. The sole export customer was South Africa. Series 3 (MR.3 phase 2) Shackleton were equipped with 2 additional Rolls-Royce Viper 203 Turbojet Engines.

AVRO 694 Lincoln

The AVRO 694 Lincoln is a four-engine heavy bomber aircraft produced by the British manufacturer AVRO, A.V. Roe and Company.

Crew	7
Propulsion	4 Piston Engines
Engine Model	Rolls-Royce Merlin 85
Engine Power (each)	1305 kW	1750hp
Speed	474 km/h	256kts 295 mph
Service Ceiling	9.296 m	30.500ft
Range	2.371 km	1.280 NM 1.473 mi.
Empty Weight	19.686 kg	43.400lbs
max. Takeoff Weight	34.019 kg	75.000lbs
Wing Span	36,58 m	120,0ft
Wing Area	132,0 m²	1421ft²
Length	23,86 m	78,3ft
Height	5,27 m	17,3ft
First Flight	09.06.1944
Production Status	out of production
Production Range	1945-1951
Total Production	583
Developed from	AVRO 683 Lancaster
Data for (Version)	AVRO 694 Lincoln I
Variants	Lincoln I, II, III, IV, Mk 15, Mk 30, Mk 30A, Mk 31

Remarks
The AVRO Lincoln is a development of the AVRO 683 Lancaster, the first variants were initially designated Lancaster IV and V. The Lincoln was the last piston-engined bomber aircraft in service with the Royal Air Force.

AVRO 685 York

The AVRO 685 York is a four-engine airliner and transport aircraft produced by the British manufacturer AVRO, A.V. Roe and Company. The York was used by both civil and military operators.

Crew	5
Passengers	56
Propulsion	4 Piston Engines
Engine Model	Rolls-Royce Merlin 24
Engine Power (each)	954 kW	1280hp
Speed	480 km/h	259kts 298mph
Service Ceiling	7.010 m	23.000ft
Range	4.345 km	2.346NM 2.700 mi.
Empty Weight	16.069 kg	42.040lbs
max. Takeoff Weight	31.115 kg	68.597lbs
Wing Span	31,09 m	102,0ft
Wing Area	120,5 m²	1297ft²
Length	23,93 m	78,5ft
Height	5,44 m	17,8ft
First Flight	05.07.1942
Production Status	out of production
Production Range	1943-1946
Total Production	258
Developed from	AVRO 683 Lancaster
Data for (Version)	Avro 685 York

Remarks
The AVRO York was developed on base of the AVRO 683 Lancaster.

AVRO 683 Lancaster

The AVRO 683 Lancaster is a four-engine heavy bomber aircraft during WWII produced by the British manufacturer AVRO, A.V. Roe and Company.

Crew	7
Propulsion	4 Piston Engines
Engine Model	Rolls-Royce Merlin 24
Engine Power (each)	1223 kW	1640hp
Speed	463 km/h	250kts 288 mph
Service Ceiling	7.468 m	24.500ft
Range	4.074 km	2.200 NM 2.532 mi.
Empty Weight	16.738 kg	36.900lbs
max. Takeoff Weight	31.751 kg	70.000lbs
Wing Span	31,09 m	102,0ft
Wing Area	120,5 m²	1297ft²
Length	21,18 m	69,5ft
Height	5,97 m	19,6ft
First Flight	09.01.1941
Production Status	out of production
Total Production	7377
Developed from	AVRO 679 Manchester
Data for (Version)	Avro Lancaster B.I

Remarks
The Lancaster is a development of the AVRO 679 Manchester.

AVRO 652A Anson

The AVRO 652A Anson is a twin-engined trainer aircraft produced by the British manufacturer AVRO, A.V. Roe and Company. The Anson was used as a liaison aircraft also.

Crew	3-4
Passengers	4
Propulsion	2 Radial Engines
Engine Model	Armstrong-Siddeley Cheetah IX
Engine Power (each)	261 kW	350hp
Speed	304 km/h	164kts 189 mph
Service Ceiling	5.791 m	19.000ft
Range	1.270 km	686 NM 789 mi.
Empty Weight	2.438 kg	5.375lbs
max. Takeoff Weight	3.629 kg	8.000lbs
Wing Span	17,20 m	56,4 ft
Wing Area	38,1 m²	410 ft²
Length	12,88 m	42,3 ft
Height	3,99 m	13,1 ft
First Flight	24.03.1935
Production Status	out of production
Production Range	1936-1952
Total Production	11020
Data for (Version)	Avro 652A Anson Mk I

Remarks
The AVRO Anson was originally designed for maritime reconnaissance operations. After WWII several AVRO Anson were operated as civil passenger aircraft. 8138 were produced by Avro and 2882 by Canadian Federal Aircraft.

AVRO 631 / 643 Cadet

The AVRO 631 / 643 Cadet is a single-engine two-seat trainer biplane aircraft produced by the British manufacturer AVRO, A.V. Roe and Company.

Crew	2
Propulsion	1 Radial Engine
Engine Model	Armstrong Siddeley Gent Major 1A
Engine Power	112 kW	150hp
max. Cruise Speed	161 km/h	87kts 100 mph
max. Speed (vne)	187 km/h	101kts 116 mph
Service Ceiling	3.658 m	12.000 ft
Range	522 km	282 NM 325 mi.
Empty Weight	583 kg	1.285lbs
max. Takeoff Weight	907 kg	2.000lbs
Wing Span	9,19 m	30,2ft
Wing Area	24,3 m²	262ft²
Length	7,54 m	24,7ft
Height	2,69 m	8,8ft
First Flight	10/1931
Production Status	out of production
Total Production	105
Developed from	AVRO 621 Tutor
Data for (Version)	AVRO 643 Cadet
Variants	AVRO 631 Cadet, 643 Cadet

Remarks
The AVRO 631 is a development of the AVRO 621 Tutor.

AVRO 626

 

The AVRO 626 is a single-engine two-or three-seat trainer biplane aircraft produced by the British manufacturer AVRO, A.V. Roe and Company.

Crew	2 / 3
Propulsion	1 Radial Engine
Engine Model	Armstrong Siddeley Lynx IVC
Engine Power	179 kW	240hp
Speed	180 km/h	97kts 112 mph
Service Ceiling	4.511 m	14.800ft
Range	385 km	208 NM 239 mi.
Empty Weight	801 kg	1.766lbs
max. Takeoff Weight	1.247 kg	2.749lbs
Wing Span	10,36 m	34,0ft
Wing Area	27,9 m²	300 ft²
Length	8,08 m	26,5ft
Height	2,92 m	9,6ft
First Flight	1930
Production Status	out of production
Total Production	ca. 200
Developed from	AVRO 621 Tutor
Data for (Version)	AVRO 626
Variants	AVRO 637, Tatra T-126

Remarks
The AVRO 626 is a development of the AVRO 621 Tutor

AVRO 621 Tutor

The AVRO 621 Tutor is a single-engine two-seat trainer biplane aircraft produced by the British manufacturer AVRO, A.V. Roe and Company.

Crew	2
Propulsion	1 Radial Engine
Engine Model	Armstrong Siddeley Lynx IVc
Engine Power	179 kW	240hp
max. Cruise Speed	169 km/h	91kts 105 mph
Speed	196 km/h	106kts 122 mph
Service Ceiling	4.938 m	16.200 ft
Range	402 km	217 NM 250 mi.
Empty Weight	839 kg	1.850lbs
max. Takeoff Weight	1.115 kg	2.458lbs
Wing Span	10,36 m	34,0ft
Wing Area	28,0 m²	301ft²
Length	8,08 m	26,5ft
Height	2,92 m	9,6ft
First Flight	26.06.1926
Production Status	out of production
Total Production	795
ICAO Code	TUTR
Data for (Version)	AVRO 621 Tutor
Variants	AVRO Sea Tutor, 621 Tutor II, P.W.S.18

AVRO 594 / 616 Avian

The AVRO 594 / 616 Avian is a single-engine two-seat touring and trainer biplane aircraft produced by the British manufacturer AVRO, A.V. Roe and Company.

Crew	1
Passengers	1
Propulsion	1 Piston Engine
Engine Model	ADC Cirrus III
Engine Power	71 kW	95hp
max. Cruise Speed	141 km/h	76kts 87 mph
max. Speed (vne)	165 km/h	89kts 102 mph
Service Ceiling	5.486 m	18.000ft
Range	644 km	348 NM 400 mi.
Empty Weight	424 kg	935lbs
max. Takeoff Weight	651 kg	1.435lbs
Wing Span	8,53 m	28,0ft
Wing Area	22,8 m²	245 ft²
Length	7,39 m	24,2ft
Height	2,59 m	8,5ft
First Flight	1926
Production Status	out of production
Total Production	405
ICAO Code	AVIN
Data for (Version)	Avro 594 Avian Mk IIIA
Variants	581 (Prototype), 594, 605, 616, 625 Avian Monoplane

AVRO 504

 

The AVRO 504 is a single-engine two-seat trainer, fighter and light bomber biplane aircraft of WWI produced by the British Manufacturer AVRO, A.V. Roe and Company. Most AVRO 504 were used as trainers.

Crew	2
Propulsion	1 Rotary Engine
Engine Model	Le Rhône 9J
Engine Power	82 kW	110 hp
Speed	144 km/h	78 kts 90 mph
Service Ceiling	4.877 m	16.000 ft
Range	402 km	217 NM 250mi.
Empty Weight	558 kg	1.230lbs
max. Takeoff Weight	830 kg	1.830lbs
Wing Span	10,97 m	36,0 ft
Wing Area	30,7 m²	330 ft²
Length	8,97 m	29,4 ft
Height	3,17 m	10,4 ft
First Flight	07/1913
Production Status	out of production
Production Range	1913-1932
Total Production	ca. 8500
Developed from	AVRO 500
ICAO Code	A504
Data for (Version)	AVRO 504K
Variants	AVRO 504A ... S, Yokosuka K1Y, K2Y1, K2Y2, U-1 Avruska, MU-1

Remarks
The AVRO 504 was license-built by several other manufacturers. The AVRO 504 was produced with several different engine variants (inline piston, rotary, radial piston).

Aviation Traders ATL.98 Carvair

 

The Aviation Traders ATL.98 Carvair is a four-engine cargo freighter aircraft produced by the British manufacturer Aviation Traders Limited. The ATL.98 is a special freighter for the transportation of 5 cars and up to 25 passengers.

Crew	2
Propulsion	4 Radial Engines
Engine Model	Pratt & Whitney R-2000-7M2 Twin Wasp
Engine Power (each)	1081 kW	1450 hp
Speed	402 km/h	217 kts 250 mph
Service Ceiling	5.700 m	18.700 ft
Range	3.704 km	2.000 NM 2.302 mi.
Empty Weight	18.999 kg	41.885 lbs
max. Takeoff Weight	33.475 kg	73.800 lbs
Wing Span	35,81 m	117,5 ft
Wing Area	135,8 m²	1462 ft²
Length	31,27 m	102,6 ft
Height	9,09 m	29,8 ft
First Flight	21.06.1961
Production Status	out of production
Total Production	21
Developed from	Douglas DC-4
Data for (Version)	Aviation Traders ATL.98

Aviat A-1 Husky

The Aviat A-1 Husky is a single-engine two-seat light utility aircraft produced by the US-American manufacturer Aviat Aircraft Inc.

Crew	1
Passengers	1
Propulsion	1 Piston Engine
Engine Model	Lycoming O-360-A1P
Engine Power	134 kW	180 hp
Speed	233 km/h	126 kts 145 mph
Service Ceiling	6.096 m	20.000 ft
Range	1.019 km	550 NM 633 mi.
Empty Weight	540 kg	1.190 lbs
max. Takeoff Weight	857 kg	1.890 lbs
Wing Span	10,82 m	35,5 ft
Wing Area	17,0 m²	183 ft²
Length	6,88 m	22,6 ft
Height	2,01 m	6,6 ft
First Flight	1986
Production Status	in production
Data for (Version)	Aviat A-1A Husky

AOP

 

Light Observation Aircraft

Crew	3
Propulsion	1 Piston Engine
Engine Model	de Havilland Gipsy Major 1
Engine Power	97 kW	130 hp
Speed	209 km/h	113 kts 130 mph
Service Ceiling	4.572 m	15.000 ft
Range	463 km	250 NM 288 mi.
Empty Weight	499 kg	1.100 lbs
max. Takeoff Weight	771 kg	1.700 lbs
Wing Span	10,97 m	36,0 ft
Wing Area	15,5 m²	167 ft²
Length	7,03 m	23,1 ft
Height	2,44 m	8,0 ft
First Flight	1942
Production Status	out of production
Data for (Version)	Auster AOP Mk.III

Remarks
AOP = Air Observation Post

Auster J/5 Autocar

The Auster J/5 Autocar is a single-engine four-seat light touring aircraft produced by the British manufacturer Auster Aircraft Limited.

Crew	1
Passengers	3
Propulsion	1 Piston Engine
Engine Model	de Havilland Gipsy Major I
Engine Power	97 kW	130 hp
max. Cruise Speed	178 km/h	96 kts 110 mph
max. Speed (vne)	257 km/h	139 kts 160 mph
Service Ceiling	3.353 m	11.000 ft
Range	419 km	226 NM 260 mi.
Empty Weight	605 kg	1.334 lbs
max. Takeoff Weight	1.088 kg	2.399 lbs
Wing Span	10,97 m	36,0 ft
Wing Area	17,1 m²	184 ft²
Length	7,11 m	23,3 ft
Height	2,50 m	8,2 ft
First Flight	1949
Production Status	out of production
Total Production	ca. 180
ICAO Code	ACAR
other TCDS	LBA L-508
Data for (Version)	Auster J-5B Autocar
Variants	J-5B, J-5E, J-5G, J-5H, J-5P, J-5V

Auster J/1 Autocrat

The Auster J/1 Autocrat is a single-engine three-seat light touring aircraft produced by the British manufacturer Auster Aircraft Limited.

Crew	1-2
Passengers	1-2
Propulsion	1 Piston Engine
Engine Model	Blackburn Cirrus Minor II
Engine Power	75 kW	100 hp
max. Cruise Speed	159 km/h	86 kts 99 mph
max. Speed (vne)	194 km/h	105 kts 121 mph
Service Ceiling	4.267 m	14.000 ft
Range	515 km	278 NM 320 mi.
Empty Weight	478 kg	1.054 lbs
max. Takeoff Weight	841 kg	1.854 lbs
Wing Span	10,97 m	36,0 ft
Wing Area	17,2 m²	185 ft²
Length	7,70 m	25,3 ft
Height	1,98 m	6,5 ft
First Flight	1945
Production Status	out of production
Total Production	ca. 420
Developed from	Taylorcraft Auster AOP Mk.V
ICAO Code	J1
Data for (Version)	Auster J-1 Autocrat
Variants	J-1A,J-1B Aiglet, J-1N Alpha, J-1S Autocrat

Remarks
The J/1 Autocrat is a development of the (Taylorcraft) Auster Model J AOP Mk.V.

ATR 72

The ATR 72 is a twin-engine turboprop-powered regional airliner with a capacity of maximum 74 passengers produced by the French/Italian manufacturer ATR, Avions de Transport Regional, a joint-venture of EADS and Alenia Aeronautica.

Crew	2
Passengers	66 - 74
Propulsion	2 Turboprop Engines
Engine Model	Pratt & Whitney Canada PW124B
Engine Power (each)	1611 kW	2160 shp
Speed	509 km/h	275 kts 316 mph
Service Ceiling	7.620 m	25.000 ft
Range	1.400 km	756 NM 870 mi.
Empty Weight	12.700 kg	28.000 lbs
max. Takeoff Weight	21.500 kg	47.399 lbs
Wing Span	27,06 m	88,8 ft
Wing Area	61,0 m²	657 ft²
Length	24,16 m	79,3 ft
Height	7,65 m	25,1 ft
First Flight	12.10.1988
Production Status	in production
FAA TCDS	A53EU
EASA TCDS	A.084
Data for (Version)	ATR 72-200
Variants	72-200, 72-210, 72-500

Remarks
The ATR 72 is a streched development of the ATR 42. Current version is the ATR 72-500 with the ATR 72-600 under development.

ATR 42

The ATR 42 is a twin-engined turboprop-powered regional airliner with a capacity of maximum 50 passengers produced by the French/Italian manufacturer ATR, Avions de Transport Regional, a joint-venture of EADS and Alenia Aeronautica.

Crew	2
Passengers	46 - 50
Propulsion	2 Turboprop Engines
Engine Model	Pratt & Whitney Canada PW120
Engine Power (each)	1529 kW	2050 shp
Speed	491 km/h	265 kts 305 mph
Service Ceiling	7.620 m	25.000 ft
Range	1.150 km	621 NM 715 mi.
Empty Weight	10.285 kg	22.675 lbs
max. Takeoff Weight	16.700 kg	36.817 lbs
Wing Span	24,57 m	80,6 ft
Wing Area	54,5 m²	587 ft²
Length	22,67 m	74,4 ft
Height	7,59 m	24,9 ft
First Flight	16.08.1984
Production Status	in production
FAA TCDS	A53EU
EASA TCDS	A.084
Data for (Version)	ATR 42-300
Variants	42-300, 42-320, 42-400, 42-500, 42-600

Remarks
Current version is the ATR 42-500.

Hawker SeaHawk

 

The Hawker SeaHawk is a single-engine single-seat naval jet fighter aircraft produced by the British manufacturer Hawker and its sister company Armstrong Whitworth.

Crew	1
Propulsion	1 Turbojet Engine
Engine Model	Rolls-Royce Nene Mk.103
Engine Power	24 kN	5395 lbf
Speed	965 km/h	521 kts 600 mph
Service Ceiling	13.564 m	44.500 ft.
Range	772 km	417 NM 480 mi.
Empty Weight	4.800 kg	10.582 lbs.
max. Takeoff Weight	7.500 kg	16.535 lbs.
Wing Span	11,90 m	39,0 ft.
Wing Area	25,8 m²	278 ft²
Length	12,30 m	40,4 ft.
Height	3,00 m	9,8 ft.
First Flight	02.09.1947
Production Status	out of production
Production Range	1951-1961
Total Production	547
Data for (Version)	SeaHawk Mk.101

Armstrong Whitworth AW.650/AW.660 Argosy

The Armstrong Whitworth AW.650/AW.660 Argosy is a four-engine turboprop-powered civil and military transport aircraft produced by the British manufacturer Armstrong Whitworth Aircraft. AW.650 is the civil desigation, AW.660 the military designation, both were called Argosy Crew 4 Propulsion 4 Turboprop Engines Engine Model Rolls-Royce Dart 526 Engine Power (each) 1506 kW 2020 shp Speed 452 km/h 244 kts 281 mph Service Ceiling 6.096 m 20.000 ft Range 3.219 km 1.738 NM 2.000 mi. Empty Weight 20.865 kg 46.000 lbs max. Takeoff Weight 39.916 kg 88.000 lbs Wing Span 35,05 m 115,0 ft Wing Area 135,5 m² 1459 ft² Length 26,44 m 86,7 ft Height 8,23 m 27,0 ft First Flight 08.01.1958 Production Status out of production Total Production 74  Data for (Version) Armstrong Whitworth AW.650 Argosy Development The Argosy came from the Air Ministry “Operation Requirement 323″ (OR323) which resulted in a specification issued in 1955 for a medium range freight aircraft capable of lifting 25,000 lb and that had a range of 2,000 nmi (3,700 km) with 10,000 lb (4,500 kg). This led AW to develop a twin engined design for the military, the AW.66. The potential for civil sales led to a civil design AW.65. The 1957 Defence White Paper would show the lack of funding available for military work but AW had revised the design for the civil market alone as a 4 engined aircraft. Operational history The Argosy was used by the Royal Air Force for its capability to accommodate 69 troops, or 48 stretcher cases or 29,000 lb (13 tonnes) of freight. This meant it could carry military equipment such as the Saracen or Ferret armoured cars, or artillery such as the 105 mm howitzer or Wombat. The earliest deployments were in 1962 to 105 Squadron in the Middle East and 114 and 267 Squadrons at RAF Benson. The following year 215 Squadron received its Argosies when based at RAF Changi, Singapore. The squadron was disbanded on New Years Eve 1967 and the aircraft went to 70 Squadron at RAF Akrotiri, Cyprus. This was the last squadron to operate the aircraft when it disposed of them in February 1975 in favour of Lockheed Hercules. The E.1 version of the Argosy was with 115 Squadron from 1968 to 1978, most of the time based at RAF Cottesmore. IN our account of the development by SirW.G.Armstrong Whitworth Aircraft Ltd of the AW.650 Argosy which appeared in the issue of October 17,1958, the point was made that this commercial freighter had its genesis in a military specification. Formulated in1955 , the Air Ministry's Operational Requirement 323 outlined the desired characteristics of a multi-purpose transport capable of replacing the Hastings and Valetta as standard equipment in RAF Transport Command. Although OR.323 eventually lapsed ,the need to find a replacement for these aircraft is more pressing than ever; and AWA's company-financed development of the civil AW.650 has allowed the Air Ministry to procure a new transport for a substantially reduced development cost. Discussions were held between the Air Ministry, Ministry of Aviation (then Supply) and manufacturer from 1958 onwards ,and by mid-1959 a specification had been written using the civil 650 as a starting point. It was at first considered that the task of converting the 650 to fulfil military requirements would be a minor one; but in the event—and as so often happens—the two aircraft differ more than might at first sight appear. s