13 Ekim 2012 Cumartesi

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.

3 Ekim 2012 Çarşamba

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.

2 Ekim 2012 Salı

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.

1 Ekim 2012 Pazartesi

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