JEROEN VOGELAAR: Aviation Photographs

Civilian aviation

Boeing 787 Dreamliner

Boeing 787-8 PH-TFL ArkeFly

The Boeing 787 Dreamliner is a long-range, mid-size wide-body, twin-engine jet airliner developed by Boeing Commercial Airplanes.

 

  • Role: Wide-body jet airliner
  • National origin: United States
  • Manufacturer: Boeing Commercial Airplanes
  • First flight: December 15, 2009
  • Introduction: October 26, 2011, with All Nippon Airways
  • Status: In service
  • Produced: 2007–present
  • Number built: 269 as of April 2015

Specifications

General characteristics

Boeing 787-8

First Flight: December 15, 2009

  • Cockpit crew: 2
  • Seating capacity: 381 (maximum)
  • Overall length: 186 ft 1 in (56.7 m)
  • Wingspan: 197 ft 3 in (60.1 m)
  • Overall height: 55 ft 6 in (16.9 m)
  • Fuselage width: 18 ft 11 in (5.77 m
  • Fuselage Height: 19 ft 7 in (5.97 m)
  • Operating empty weight: 259,500 lb (118,000 kg)
  • Maximum landing weight: 380,000 lb (172,000 kg)
  • Maximum take-off weight: 502,500 lb (228,000 kg)
  • Service ceiling: 43,000 ft (13,100 m)
  • Cruising speed: Mach 0.85 (567 mph, 490 knots, 913 km/h at 35,000 ft/10,700 m)
  • Maximum speed: Mach 0.90 (593 mph, 515 knots, 954 km/h at 35,000 ft/10,700 m)
  • Range fully loaded: 7,850 nmi (14,500 km; 9,030 mi)
  • Engine (× 2): General Electric GEnx-1B or Rolls-Royce Trent 1000 thrust: 64,000 lbf (280 kN)

Boeing 787-9

Boeing 787-9 Dreamliner PH-BHD KLM

Boeing 787-9 Dreamliner PH-BHD KLM

First Flight: September 17, 2013

  • Cockpit crew: 2
  • Seating capacity: 420 (maximum certificated)
  • Overall length: 206 ft 1 in (62.8 m)
  • Wingspan: 197 ft 3 in (60.1 m)
  • Overall height: 55 ft 10 in (17.0 m)
  • Fuselage width: 18 ft 11 in (5.77 m
  • Fuselage Height: 19 ft 7 in (5.97 m)
  • Operating empty weight: 304,000 lb (138,000 kg)
  • Maximum landing weight: 425,000 lb (193,000 kg)
  • Maximum take-off weight: 557,000 lb (253,000 kg)
  • Service ceiling: 43,000 ft (13,100 m)
  • Cruising speed: Mach 0.85 (567 mph, 490 knots, 913 km/h at 35,000 ft/10,700 m)
  • Maximum speed: Mach 0.90 (593 mph, 515 knots, 954 km/h at 35,000 ft/10,700 m)
  • Range fully loaded: 8,300 nmi (15,400 km; 9,550 mi)
  • Engine (× 2): General Electric GEnx-1B or Rolls-Royce Trent 1000 thrust: 71,000 lbf (320 kN)

Boeing 787-10

First Flight:

  • Cockpit crew: 2
  • Seating capacity: 323 (3-class) (maximum certificated)
  • Overall length: 224 ft 1 in (68.3 m)
  • Wingspan: 197 ft 3 in (60.1 m)
  • Overall height: 55 ft 10 in (17.0 m)
  • Fuselage width: 18 ft 11 in (5.77 m
  • Fuselage Height: 19 ft 7 in (5.97 m)
  • Operating empty weight: 304,000 lb (138,000 kg)
  • Maximum landing weight: 445,000 lb (202,000 kg)
  • Maximum take-off weight: 557,000 lb (253,000 kg)
  • Service ceiling: 43,000 ft (13,100 m)
  • Cruising speed: Mach 0.85 (567 mph, 490 knots, 913 km/h at 35,000 ft/10,700 m)
  • Maximum speed: Mach 0.90 (593 mph, 515 knots, 954 km/h at 35,000 ft/10,700 m)
  • Range fully loaded: 7,020 nmi (13,000 km; 8,080 mi)
  • Engine (× 2): General Electric GEnx-1B or Rolls-Royce Trent 1000 thrust: 76,000 lbf (340 kN)

Antonov An-12

Antonov An-12AP UR-CCP Cavok Air

The Antonov An-12 is a four-engined turboprop transport aircraft designed in the Soviet Union.

  • Role: Civil and Military transport aircraft
  • National origin: Soviet Union
  • Manufacturer: Antonov
  • First flight: 16 December 1957
  • Introduction: 1959
  • Status: Active service with various airlines (especially cargo) and Air Forces
  • Produced: 1957–1973
  • Number built: 1,248

Specifications (An-12)

General characteristics

  • Crew: 5: 2 pilots, flight engineer, navigator, radio operator
  • Payload: 20,000 kg (44,000 lb)
  • Length: 33.10 m (108 ft 7 in)
  • Wingspan: 38.00 m (124 ft 8 in)
  • Height: 10.53 m (34 ft 7 in)
  • Wing area: 121.7 m² (1,310 ft²)
  • Empty weight: 28,000 kg (62,000 lb)
  • Useful load: 60 paratroopers (two BMD-1 armoured vehicles)
  • Max. takeoff weight: 61,000 kg (130,000 lb)
  • Powerplant: 4 × Ivchenko AI-20L or AI-20M turboprops, 4,000 ehp (3,000 kW) each

Performance

  • Maximum speed: 777 km/h (419 knots, 482 mph)
  • Cruise speed: 670 km/h (361 knots, 415 mph)
  • Range:
    • With maximum fuel: 5,700 km (3,075 nm, 3,540 mi)
    • With maximum load: 3,600 km (1,945 nm, 2,235 mi))
  • Service ceiling: 10,200 m (33,500 ft)
  • Rate of climb: 10m/s (1960ft/min)

Armament

  • Guns: 2× 23 mm (0.906 in) Nudelman-Rikhter NR-23 cannons in a tail turret (some aircraft)

Embraer ERJ-145

Embraer ERJ-145MP PH-DND Denim Air

The Embraer ERJ 145 family is a series of twin-engine regional jets produced by Embraer, a Brazilian aerospace company. Family members include the ERJ 135 (37 passengers), ERJ 140 (44 passengers), and ERJ 145 (50 passengers), as well as the Legacy business jet and the R-99 family of military aircraft.

  • Role: Twin-engine Regional airliner
  • National origin: Brazil
  • Manufacturer: Embraer
  • Production line: São José dos Campos, São Paulo State.
  • First flight: August 11, 1995
  • Introduction: December 1996
  • Status: In service
  • Produced: 1995 – present
  • Number built: 890 as of January 2012
  • Variants: Embraer ERJ-135, ERJ-140, Embraer Legacy business jet

Specifications

General characteristics

  • Crew: 3 (2 pilots + flight attendant)
  • Capacity: 50
  • Length: 29.87 m (98 ft 0 in)
  • Wingspan: 20.04 m (65 ft 9 in)
  • Height: 6.76 m (22 ft 2 in)
  • Empty weight: 18,500 kg (40,785 lb)
  • Max Payload weight: 5,909 kg (13,027 lb)
  • Max take-off weight: 24,100 kg (53,131 lb)
  • Powerplant: 2x Rolls-Royce AE 3007-A1E (8700 lb thrust)

Performance

  • Maximum speed: Mach 0.80, 470 kts, 530 mph, 851 km/h
  • Range: 3,704 km (2,000 nmi)
  • Service ceiling:  11,278 m (37,000 ft)

Bombardier Dash 8/Q Series

Bombardier DHC-8-402/Q400 G-JECK Flybe - British European

The Bombardier Dash 8 or Q-Series, previously known as the de Havilland Canada Dash 8 or DHC-8, is a series of twin-engined, medium range, turboprop airliners.

  • Role: Turboprop airliner
  • National origin: Canada
  • Manufacturer: de Havilland Canada/Bombardier Aerospace
  • First flight: June 20, 1983
  • Introduction: 1984 with NorOntair
  • Status: In production, in service
  • Produced: 1983–present
  • Number built: 1150 (as of 31 December 2014)

Variants

  • DHC-8-100 series
  • CC-142
  • CT-142
  • E-9A Widget
  • DHC-8-200 series
  • DHC-8-300 series
  • DHC-8-300 MSA
  • DHC-8-400 series
  • Q400
  • Q400NextGen
  • Q400-MR
  • DHC-8 MPA-D8
  • DHC-8-402PF

Specifications

DHC-8-100 series

General characteristics

  • Cockpit crew: 2
  • Seating capacity, typical: 37–39
  • Overall length: 73 ft (22.25 m)
  • Wingspan: 84 ft 11 in (25.89 m)
  • Overall height: 24 ft 7 in (7.49 m)
  • Fuselage width: 28 ft 10 in (2.69 m)
  • Operating empty weight: 32,400 lb (14,700 kg)
  • Maximum landing weight: 34,500 lb (15,650 kg)
  • Maximum take-off weight: 36,300 lb (16,470 kg)
  • Engine (× 2): PW120A/PW121

Performance

  • Service ceiling: 25,000 ft (7,620 m)
  • Cruising speed: 310 mph (500 km/h) 269 knots
  • Range fully loaded: 1,174 miles (1,889 km)

DHC-8-200 series

General characteristics

  • Cockpit crew: 2
  • Seating capacity, typical: 37–39
  • Overall length: 73 ft (22.25 m)
  • Wingspan: 84 ft 11 in (25.89 m)
  • Overall height: 24 ft 7 in (7.49 m)
  • Fuselage width: 28 ft 10 in (2.69 m)
  • Operating empty weight: 32,400 lb (14,700 kg)
  • Maximum landing weight: 34,500 lb (15,650 kg)
  • Maximum take-off weight: 36,300 lb (16,470 kg)
  • Engine (× 2): PW123C/D

Performance

  • Service ceiling: 25,000 ft (7,620 m)
  • Cruising speed: 334 mph (537 km/h) 290 knots
  • Range fully loaded: 1,065 miles (1,713 km)

DHC-8-300 series

General characteristics

  • Cockpit crew: 2
  • Seating capacity, typical: 50–56
  • Overall length: 84 ft 3 in (25.68 m)
  • Wingspan: 90 ft (27.43 m)
  • Overall height: 24 ft 7 in (7.49 m)
  • Fuselage width: 28 ft 10 in (2.69 m)
  • Operating empty weight: 25,995 lb (11,791 kg)
  • Maximum landing weight: 42,000 lb (19,050 kg)
  • Maximum take-off weight: 43,000 lb (19,500 kg)
  • Engine (× 2): PW123B

Performance

  • Service ceiling: 25,000 ft (7,620 m)
  • Cruising speed: 328 mph (528 km/h) 285 knots
  • Range fully loaded: 968 miles (1,558 km)

Q400 series

Bombardier DHC-8-402/Q400 YL-BAY Air Baltic

General characteristics

  • Cockpit crew: 2
  • Seating capacity, typical: 68–86
  • Overall length: 107 ft 8 in (32.81 m)
  • Wingspan: 93 ft 2 in (28.4 m)
  • Overall height: 27 ft 3 in (8.3 m)
  • Fuselage width: 28 ft 10 in (2.69 m)
  • Operating empty weight: 37,886 lb (17,185 kg)
  • Maximum landing weight: 61,750 lb (28,010 kg)
  • Maximum take-off weight: 64,500 lb (29,260 kg)
  • Engine (× 2): PW150A

Performance

  • Service ceiling: 27,000 ft (8,230 m)
  • Cruising speed: 414 mph (667 km/h) 360 knots
  • Range fully loaded: 1,567 miles (2,522 km)

Bombardier Q400 D-ABQG Air Berlin

Fokker F27 Friendship

Fokker F.27-100 Friendship PH-NIV Fokker Aircraft

The Fokker F27 Friendship is a turboprop airliner designed and built by the defunct Dutch aircraft manufacturer Fokker.

  • Role: airliner
  • National origin: Netherlands
  • Manufacturer: Fokker
  • First flight: 24 November 1955
  • Introduction: 19 November 1958
  • Status: Out of production, in service
  • Produced: 1986-1997
  • Number built: 586
  • Developed from: Fokker F28 Fellowship
  • Variants: Fairchild F-27/FH-227
  • Developed into: Fokker 50, Fokker 60

Variants

  • F27-100 – was the first production model; 44 passengers
  • F27-200 – uses the Dart Mk 532 engine
  • F27-300 Combiplane – Civil passenger/cargo aircraft
  • F27-400 – “Combi” passenger/cargo aircraft, with two Rolls-Royce Dart 7 turboprop engines and large cargo door
  • F27-500 – The -500, had a 1.5 m (4 ft 11 in) longer fuselage, a return to the Dart Mk 528 engine, and accommodation for up to 52 passengers. It first flew in November 1967
  • F27-500F – A version of the -500 for Australia with smaller front and rear doors
  • F27-600 – Quick change cargo/passenger version of -200 with large cargo door
  • F27-700 – A F27-100 with a large cargo door
  • F-27 – license-built version manufactured by Fairchild Hiller in the United States
  • FH-227 – stretched version of the F-27, independently developed and manufactured by Fairchild Hiller in the United States

Military variants

Specifications (F.27)

General characteristics

  • Crew: 2 or 3
  • Capacity: 48-56 passengers
  • Length: 25.06 m (82 ft 3 in)
  • Wingspan: 29 m (95 ft 2 in)
  • Height: 8.72 m (28 ft 7 in)
  • Wing area: 70 m2 (750 sq ft)
  • Empty weight: 11,204 kg (24,701 lb)
  • Max takeoff weight: 19,773 kg (43,592 lb)
  • Powerplant: 2 × Rolls-Royce Dart Mk.532-7 two-stage centrifugal compressor turboprop, 1,678 kW (2,250 hp) each

Performance

  • Cruising speed: 460 km/h (286 mph; 248 kn)
  • Range: 2,600 km (1,616 mi; 1,404 nmi)
  • Rate of climb: 7.37 m/s (1,451 ft/min)

Boeing 777

Boeing 777-306ER PH-BVI KLM

The Boeing 777 is a family of long-range wide-body twin-engine jet airliners developed and manufactured by Boeing Commercial Airplanes. It is the world’s largest twinjet and has a typical seating capacity for 314 to 451 passengers.

  • Role: long-range wide-body twin-engine jet airliner
  • National origin: United States
  • Manufacturer: Boeing Commercial Airplanes
  • First flight: June 12, 1994
  • Introduction: June 7, 1995, with United Airlines
  • Status: In service
  • Produced: 1993–present
  • Number built: 1,274 through February 2015
  • Variant: Boeing 777 Freighter
  • Developed into: Boeing 777X

Specifications

Boeing 777-200LR

General characteristics

  • Cockpit crew: 2
  • Seating capacity, typical: 440 (maximum)
  • Overall length: 209 ft 1 in (63.7 m)
  • Wingspan: 212 ft 7 in (64.8 m)
  • Overall height: 61 ft 1 in (18.6 m)
  • Fuselage width: 20 ft 4 in (6.20 m)
  • Operating empty weight: 320,000 lb (145,150 kg)
  • Maximum landing weight: 492,000 lb (223,168 kg)
  • Maximum take-off weight: 766,000 lb (347,500 kg)
  • Engine (× 2): General Electric GE90-110B1 thrust 110,100 lbf (490 kN)
  •                              General Electric GE90-115B1 thrust 115,300 lbf (512 kN)

Performance

  • Service ceiling: 43,100 ft (13,140 m)
  • Cruising speed: Mach 0.84 (560 mph, 905 km/h, 490 knots) at a cruise altitude of 35,000 ft (11,000 m)
  • Maximum speed: Mach 0.87 (~200) (590 mph, 950 km/h, 512 knots) at a cruise altitude of 35,000 ft (11,000 m)
  • Range fully loaded: 9,395 nmi (17,395 km, 10,811 mi)

Specifications

Boeing 777-300ER

Boeing 777-35RER VT-JEW Jet Airways

Boeing 777-35RER VT-JEW Jet Airways

General characteristics

  • Cockpit crew: 2
  • Seating capacity, typical: 550 (maximum)
  • Overall length: 242 ft 4 in (73.9 m)
  • Wingspan: 212 ft 7 in (64.8 m)
  • Overall height: 60 ft 8 in (18.5 m)
  • Fuselage width: 20 ft 4 in (6.20 m)
  • Operating empty weight: 370,000 lb (167,800 kg)
  • Maximum landing weight: 554,000 lb (251,290 kg)
  • Maximum take-off weight: 775,000 lb (351,500 kg)
  • Engine (× 2): General Electric GE90-115B1 thrust 115,300 lbf (512 kN)

Performance

  • Service ceiling: 43,100 ft (13,140 m)
  • Cruising speed: Mach 0.84 (560 mph, 905 km/h, 490 knots) at a cruise altitude of 35,000 ft (11,000 m)
  • Maximum speed: Mach 0.87 (~200) (590 mph, 950 km/h, 512 knots) at a cruise altitude of 35,000 ft (11,000 m)
  • Range fully loaded: 7,825 nmi (14,490 km, 9,005 mi)

 

Embraer 170/175

Embraer 175LR G-FBJJ Flybe - British European

The Embraer 170/ Embraer 175 models in the 80-seat range are the smaller in the E-Jet family.

  • Role: Medium range airliner
  • National origin: Brazil
  • Manufacturer: Embraer
  • Production line: São José dos Campos, São Paulo State.
  • First flight: Embraer 170 19 February 2002 PP-JXE, Embraer 175 June 14 ,2003, PP-XJD
  • Introduced: Embraer 170 March 2004 to LOT Polish Airlines, Embraer 175 July 2005 to Air Canada
  • Status: In service
  • Produced: 2003 – present
  • Number built:  Embraer 170 188, Embraer 175 249 April 2015
  • Variants:  Embraer 190, Embraer 195, Embraer Lineage 1000
  • Developed into: Embraer E-Jet E2 family

Specifications

Embraer 170 (ERJ170-100)

General characteristics

  • Crew: Two
  • Capacity: 80 (1-class, 29 in/30 in pitch)
  • Length: 29.90 m (98 ft 1 in)
  • Wingspan: 26.00 m (85 ft 4 in)
  • Height: 9.67 m (32 ft 4 in)
  • Empty weight: 21,140 kg (46,610 lb)
  • Max Payload weight: 9,840 kg (21,690 lb) (AR)
  • Max take-off weight: 38,600 kg (85,100 lb) (AR)
  • Powerplant:  2× GE CF34-8E turbofans

Performance

  • Maximum speed: 890 km/h (481 kn, Mach 0.82)
  • Range: AR: 4,448 km (2,402 nmi)
  • Service ceiling:  12,500 m (41,000 ft)

Embraer 175 (ERJ170-200)

General characteristics

  • Crew: Two
  • Capacity: 88 (1-class, 30 in pitch)
  • Length: 31.68 m (103 ft 11 in)
  • Wingspan: 28.72 m (94 ft 3 in)
  • Height: 10.28 m (34 ft 7 in)
  • Empty weight: 21,810 kg (48,080 lb)
  • Max Payload weight: 10,360 kg (22,840 lb) (AR)
  • Max take-off weight: 40,370 kg (89,000 lb) (AR)
  • Powerplant:  2× GE CF34-10E turbofans

Performance

  • Maximum speed: 890 km/h (481 kn, Mach 0.82)
  • Range: AR: 3,706 km (2,001 nmi)
  • Service ceiling:  12,500 m (41,000 ft)

Airbus A330

Airbus A330-323 N815NW Delta Airlines

The Airbus A330 is a medium wide-body twin-engine jet airliner made by Airbus, a division of Airbus Group.

  • Role: Wide-body, jet airliner
  • National origin: European Multi-national
  • Manufacturer: EADS/Airbus
  • Production line: Toulouse, France
  • First flight: 2 November 1992
  • Introduction: 17 January 1994 with Air Inter
  • Status: In service
  • Produced: 1992–present
  • Number built: 1,174 as of March 2015
  • Variants: Airbus A330 Freighter

Airbus A330-242 A6-EYE Etihad

Specifications A330-200

General characteristics

  • Minimum cockpit crew: Two
  • Capacity, typical: 375: (optional) 406
  • Length: 58.82 m (193 ft 0 in)
  • Wingspan: 60.3 m (197 ft 10 in)
  • Tail height: 17.39 m (57 ft 1 in)
  • Cabin width: 5.28 m (17 ft 4 in)
  • Fuselage width: 5.64 m (18 ft 6 in)
  • Cargo volume: 136 m3 (4,800 cu ft)
  • Maximum Takeoff Weight: 242,000 kg (534,000 lb)
  • Maximum Landing Weight: 182,000 kg (401,000 lb)
  • Operating empty weight (typical): 119,600 kg (263,700 lb)
  • Engines (×2): General Electric CF6-80E1, Pratt & Whitney PW4000, Rolls-Royce Trent 700

Performance

  • Service ceiling: 12,527 m (41,100 ft)
  • Maximum service ceiling: 13,000 m (42,651 ft)
  • Cruising speed: Mach 0.82 (871 km/h or 470 kn or 541 mph at 11,000 m or 36,000 ft cruise altitude)
  • Maximum speed: Mach 0.86 (913 km/h or 493 kn or 567 mph at 11,000 m or 36,000 ft cruise altitude)
  • Range fully loaded: 13,400 km (7,200 nmi)

Airbus A330-343 HB-JHN Swiss International Airlines

Specifications A330-300

General characteristics

  • Minimum cockpit crew: Two
  • Capacity, typical: 375: (optional) 440
  • Length: 63.69 m (208 ft 11 in)
  • Wingspan: 60.3 m (197 ft 10 in)
  • Tail height: 16.83 m (55 ft 3 in)
  • Cabin width: 5.28 m (17 ft 4 in)
  • Fuselage width: 5.64 m (18 ft 6 in)
  • Cargo volume: 162.8 m3 (5,750 cu ft)
  • Maximum Takeoff Weight: 242,000 kg (534,000 lb)
  • Maximum Landing Weight: 187,000 kg (412,000 lb)
  • Operating empty weight (typical): 124,500 kg (274,500 lb)
  • Engines (×2): General Electric CF6-80E1, Pratt & Whitney PW4000, Rolls-Royce Trent 700

Performance

  • Service ceiling: 12,527 m (41,100 ft)
  • Maximum service ceiling: 13,000 m (42,651 ft)
  • Cruising speed: Mach 0.82 (871 km/h or 470 kn or 541 mph at 11,000 m or 36,000 ft cruise altitude)
  • Maximum speed: Mach 0.86 (913 km/h or 493 kn or 567 mph at 11,000 m or 36,000 ft cruise altitude)
  • Range fully loaded: 11,300 km (6,100 nmi)
Airbus A330-343 TC-LOE Turkish Airlines

Airbus A330-343 TC-LOE Turkish Airlines

 

Airbus A330 Freighter

Airbus A330-223F 9M-MUD MASkargo

The Airbus A330-200F is an all-cargo derivative of the A330-200. To overcome the standard A330’s nose-down body angle on the ground, the A330F uses a revised nose undercarriage layout to provide a level deck during cargo loading.

 

  • Role: Wide-body, cargo airliner
  • National origin: European Multi-national
  • Manufacturer: EADS/Airbus
  • Production line: Toulouse, France
  • First flight: 5 November 2009
  • Introduction: 2010
  • Status: In service
  • Produced: 2009–present
  • Number built: As of April 2015, Airbus had delivered 31 aircraft with 11 unfilled orders

Specifications

General characteristics

  • Minimum cockpit crew: Two
  • Capacity, typical: 12 (courier area)
  • Length: 58.82 m (193 ft 0 in)
  • Wingspan: 60.3 m (197 ft 10 in)
  • Tail height: 16.90 m (55 ft 5 in)
  • Cabin width: 5.28 m (17 ft 4 in)
  • Fuselage width: 5.64 m (18 ft 6 in)
  • Cargo volume: 475 m3 (16,800 cu ft) 70 t / up to 12 couriers
  • Maximum Takeoff Weight: 233,000 kg (514,000 lb)
  • Maximum Landing Weight: 187,000 kg (412,000 lb)
  • Operating empty weight (typical): 109,000 kg (240,000 lb)
  • Engines (×2): Pratt & Whitney PW4000, Rolls-Royce Trent 700

Performance

  • Service ceiling: 12,527 m (41,100 ft)
  • Maximum service ceiling: 13,000 m (42,651 ft)
  • Cruising speed: Mach 0.82 (871 km/h or 470 kn or 541 mph at 11,000 m or 36,000 ft cruise altitude)
  • Maximum speed: Mach 0.86 (913 km/h or 493 kn or 567 mph at 11,000 m or 36,000 ft cruise altitude)
  • Range fully loaded: 7,400 km (4,000 nmi) (65t), 5,950 km (3,210 nmi) (70t)

 

Boeing 757

Boeing 757-208 TF-FIJ Icelandair

The Boeing 757 is a mid-size, narrow-body twin-engine jet airliner that was designed and built by Boeing Commercial Airplanes. It is the manufacturer’s largest single-aisle passenger aircraft.

  • Role: Narrow-body jet airliner
  • National origin: United States
  • Manufacturer: Boeing Commercial Airplanes
  • First flight: February 19, 1982
  • Introduction: January 1, 1983 with Eastern Air Lines
  • Status: In service
  • Produced: 1981–2004
  • Number built: 1,050
  • Variant: Boeing C-32, Boeing 757-200PF

Specifications

General characteristics

Boeing-757-256 TF-FIU Icelandair

Boeing 757-200

  • Cockpit crew: two
  • Seating capacity: 239 (one-class)
  • Overall length: 155 ft 3 in (47.32 m)
  • Wingspan: 124 ft 10 in (38.05 m)
  • Overall height: 44 ft 6 in (13.56 m)
  • Cabin width: 11.6 ft (3.54 m)
  • Cabin length: 118.4 ft (36.09 m)
  • Operating empty weight: 127,520 lb (57,840 kg)
  • Maximum Fuel: 11,489 US gal (43,490 L)
  • Maximum take-off weight: 255,000 lb (115,680 kg)
  • Engine (× 2): Rolls-Royce RB211, Pratt & Whitney PW2037, PW2040

Performance

  • Service ceiling: 42,000 ft (12,800 m)
  • Cruising speed: Mach 0.80 (530 mph, 458 knots, 850 km/h at cruise altitude of 35,000 ft or 10.66 km)
  • Maximum speed: Mach 0.86 (567 mph, 493 knots, 913 km/h at 35,000 ft (11,000 m) cruise altitude)
  • Range fully loaded: 3,900 nmi (7,222 km), 4,100 nmi (7,600 km) with winglets

Boeing 757-300

Boeing 757-3E7 4X-BAW Arkia Israeli Airlines

The 757-300, the stretched version of the aircraft, entered service with Condor in 1999. With an overall length of 178.7 feet (54.5 m), the type is the longest single-aisle twinjet ever built.

 

  • First flight: August 2, 1998, N757X
  • Introduction: March 10, 1999 to Condor

 

Specifications

General characteristics

Boeing 757-300

  • Cockpit crew: two
  • Seating capacity: 295 (one-class)
  • Overall length: 178 ft 8 in (54.47 m)
  • Wingspan: 124 ft 10 in (38.05 m)
  • Overall height: 44 ft 6 in (13.56 m)
  • Cabin width: 11.6 ft (3.54 m)
  • Cabin length: 141.8 ft (43.21 m)
  • Operating empty weight: 142,400 lb (64,590 kg)
  • Maximum Fuel: 11,466 US gal (43,400 L)
  • Maximum take-off weight: 272,500 lb (123,600 kg)
  • Engine (× 2): Rolls-Royce RB211, Pratt & Whitney PW2037, PW2040, PW2043

Performance

  • Service ceiling: 42,000 ft (12,800 m)
  • Cruising speed: Mach 0.80 (530 mph, 458 knots, 850 km/h at cruise altitude of 35,000 ft or 10.66 km)
  • Maximum speed: Mach 0.86 (567 mph, 493 knots, 913 km/h at 35,000 ft (11,000 m) cruise altitude)
  • Range fully loaded: 3,395 nmi (6,287 km), 3,595 nmi (6,658 km) with winglets