JEROEN VOGELAAR: Aviation Photographs

Passenger aircraft

Saab 2000

Saab 2000 G-CDEB British Airways

The Saab 2000 is a twin-engined high-speed turboprop airliner built by Saab.

  • Role: Regional airliner
  • National origin: Sweden
  • Manufacturer: Saab Aircraft
  • Production line: Linköping
  • First flight: 26 March 1992
  • Introduction: 30 August 1994
  • Status: In service
  • Produced: 1992–1999
  • Number built: 63
  • Developed from: Saab 340

Saab 2000 G-CDEB British Airways

Specifications Saab 2000

General characteristics

  • Crew: two
  • Capacity: 50–58 passengers
  • Payload: 5,900 kg (13,010 lb)
  • Length: 27.28 m (89 ft 6 in)
  • Wingspan: 24.76 m (81 ft 3 in)
  • Height: 7.73 m (25 ft 4 in)
  • Wing area: 55.7 m² (600 sq ft)
  • Airfoil: NASA MS(1)013
  • Aspect ratio: 11:0
  • Empty weight: 13,800 kg (30,424 lb)
  • Max. takeoff weight: 22,800 kg (50,265 lb)
  • Powerplant: 2 × Allison AE 2100A turboprop, 3,096 kW (4,152 shp) each
  • Propellers: six blade constant speed Dowty propellers, 1 per engine

Performance

  • Cruise speed: 665 km/h (370 knots, 424 mph)
  • Service ceiling: 9,450 m (31,000 ft)
  • Rate of climb: 11.4 m/s (2,250 ft/min)

Avionics

  • Rockwell Collins Pro Line 4 avionics suite with integrated avionics processor (IAP)

Airbus A340

Airbus A340-311 PZ-TCP Surinam Airways

The Airbus A340 is a long-range, four-engine, wide-body commercial passenger jet airliner developed and produced by Airbus. Airbus manufactured the A340 in four fuselage lengths.

  • Role: Wide-body, jet airliner
  • National origin: European Multi-national
  • Manufacturer: EADS/Airbus
  • Production line: Toulouse, France
  • First flight: 25 October 1991
  • Introduction: 15 March 1993 with Lufthansa
  • Status: In service
  • Produced: 1991–2011
  • Number built: 377

Airbus A340-200

  • First Flight: 1 April 1992 c/n 004
  • First Delivery: 29 January 1993 to Lufthansa

Specifications A340-200

General characteristics

  • Minimum cockpit crew: Two
  • Capacity maximum: 375/420
  • Length: 60.30 metres (197 ft 10 in)
  • Wingspan: 60.3 m (197 ft 10 in)
  • Tail height: 16.70 metres (54 ft 9 in)
  • Cabin width: 5.28 metres (17 ft 4 in)
  • Fuselage width: 5.64 metres (18 ft 6 in)
  • Cargo volume: 162.8 cubic metres (5,750 cu ft)
  • Maximum Takeoff Weight: 275,000 kilograms (606,000 lb)
  • Operating empty weight (typical): 129,000 kilograms (284,000 lb)
  • Engines (×4): General Electric CFM56-5C, thrust 139–151 kilonewtons (31,000–34,000 lbf)

Performance

  • Service ceiling: 12,500 metres (41,000 ft)
  • Cruising speed: Mach 0.82 (871 km/h/537 mph at 11,000 m/36,000 ft)
  • Maximum speed: Mach 0.86 (913 km/h/563 mph at 11,000 m/36,000 ft)
  • Range fully loaded: 8,000 nautical miles (15,000 km; 9,200 mi)

Airbus A340-300

Airbus A340-313 B-18807 China Airlines

  • First Flight: 25 October 1991 F-WWAI c/n 001
  • First Delivery: March 1993 to Lufthansa and Air France

Specifications A340-300

General characteristics

  • Minimum cockpit crew: Two
  • Capacity maximum: 375/440
  • Length: 63.60 metres (208 ft 8 in)
  • Wingspan: 60.3 m (197 ft 10 in)
  • Tail height: 16.85 metres (55 ft 3 in)
  • Cabin width: 5.28 metres (17 ft 4 in)
  • Fuselage width: 5.64 metres (18 ft 6 in)
  • Cargo volume: 162.8 cubic metres (5,750 cu ft)
  • Maximum Takeoff Weight: 276,500 kilograms (609,600 lb)
  • Operating empty weight (typical): 130,200 kilograms (287,000 lb)
  • Engines (×4): General Electric CFM56-5C, thrust 139–151 kilonewtons (31,000–34,000 lbf)

Performance

  • Service ceiling: 12,500 metres (41,000 ft)
  • Cruising speed: Mach 0.82 (871 km/h/537 mph at 11,000 m/36,000 ft)
  • Maximum speed: Mach 0.86 (913 km/h/563 mph at 11,000 m/36,000 ft)
  • Range fully loaded: 7,400 nautical miles (13,700 km; 8,500 mi)

Airbus A340-500

  • First Flight: 11 February 2002 c/n 394
  • First Delivery: 23 October 2003 to Emirates

Specifications A340-500

General characteristics

  • Minimum cockpit crew: Two
  • Capacity maximum: 375 (1-class, maximum)
  • Length: 67.90 metres (222 ft 9 in)
  • Wingspan: 63.45 metres (208 ft 2 in)
  • Tail height: 17.10 metres (56 ft 1 in)
  • Cabin width: 5.28 metres (17 ft 4 in)
  • Fuselage width: 5.64 metres (18 ft 6 in)
  • Cargo volume: 153.9 cubic metres (5,430 cu ft)
  • Maximum Takeoff Weight: 380,000 kilograms (840,000 lb)
  • Operating empty weight (typical): 174,800 kilograms (385,400 lb)
  • Engines (×4): Rolls-Royce Trent 500, thrust 248–260 kilonewtons (56,000–58,000 lbf)

Performance

  • Service ceiling: 12,500 metres (41,000 ft)
  • Cruising speed: Mach 0.83 (881 km/h/543 mph at 11,000 m/36,000 ft)
  • Maximum speed: Mach 0.86 (913 km/h/563 mph at 11,000 m/36,000 ft)
  • Range fully loaded: 9,000 nautical miles (17,000 km; 10,000 mi)

Airbus A340-600

  • First Flight: 23 April 2001 F-WWTA c/n 360
  • First Delivery: August 2002 to Virgin Atlantic

Specifications A340-600

General characteristics

  • Minimum cockpit crew: Two
  • Capacity maximum: 440 (1-class, maximum)
  • Length: 75.30 metres (247 ft 1 in)
  • Wingspan: 63.45 metres (208 ft 2 in)
  • Tail height: 17.30 metres (56 ft 9 in)
  • Cabin width: 5.28 metres (17 ft 4 in)
  • Fuselage width: 5.64 metres (18 ft 6 in)
  • Cargo volume: 207.6 cubic metres (7,330 cu ft)
  • Maximum Takeoff Weight: 380,000 kilograms (840,000 lb)
  • Operating empty weight (typical): 174,800 kilograms (385,400 lb)
  • Engines (×4): Rolls-Royce Trent 500, thrust 260–275 kilonewtons (58,000–62,000 lbf)

Performance

  • Service ceiling: 12,500 metres (41,000 ft)
  • Cruising speed: Mach 0.83 (881 km/h/543 mph at 11,000 m/36,000 ft)
  • Maximum speed: Mach 0.86 (913 km/h/563 mph at 11,000 m/36,000 ft)
  • Range fully loaded: 7,900 nautical miles (14,600 km; 9,100 mi)

Beechcraft Super King Air

Beechcraft 350i King Air N350KA Beechcraft Corporation

The Beechcraft Super King Air family is part of a line of twin-turboprop aircraft produced by Beechcraft.

  • Role: Passenger and cargo aircraft
  • National origin: United States
  • Manufacturer: Beechcraft
  • First flight: September 3, 1983
  • Introduction: 1983
  • Status: Active service, in production
  • Produced: 1983–present
  • Built: 3,550+ all models King Air

Specifications (Beech 350i Super King Air)

General characteristics

  • Crew: 1–2
  • Capacity: 11 passengers
  • Length: 46 ft 8 in (14.22 m)
  • Wingspan: 57 ft 11 in (17.65 m)
  • Height: 14 ft 4 in (4.37 m)
  • Empty weight: 12,500 lb (5,670 kg)
  • Max. takeoff weight: 15,000 lb (6,804 kg)
  • Powerplant: 2 × Pratt & Whitney Canada PT6A-60A turboprops, 1,050 shp (783kW) each

Performance

  • Maximum speed: 313 knots, 580 km/h) at 25,000 ft (7,600m)
  • Range: 2,075 mi (1,796 nm, 3,338 km) with maximum fuel and 45 minutes reserve
  • Service ceiling: 35,000 ft (10,700 m)
  • Rate of climb: 2,450 ft/min (12.5 m/s)

Bombardier CRJ700

Bombardier CRJ700 F-GRZH HOP

The Bombardier CRJ700, are regional airliners based on the Bombardier CRJ200.

  • Role: Regional airliner
  • National origin: Canada
  • Manufacturer: Bombardier Aerospace
  • First flight: 27 May 1999
  • Introduction: 2001
  • Status: In production, in service
  • Produced: 1999–present
  • Number built: 334 as of March 2015

Specifications (CRJ700 ER)

General characteristics

  • Cockpit crew: 2
  • Seating capacity, typical: 78 (1-class, maximum)
  • Overall length: 32.51 m (106 ft 8 in)
  • Wingspan: 23.24 m (76 ft 3 in)
  • Overall height: 27.57 m (24 ft 10 in)
  • Fuselage width: 2.7 m (8 ft 10 in)
  • Operating empty weight: 19,731 kg (43,499 lb)
  • Maxium payload: 8,527 kg (18,800 lb)
  • Engine (× 2): GE CF34-8C5B1

Performance

  • Service ceiling: 12,497 m (41,000 ft)
  • Cruising speed: Mach 0.78 (829 km/h, 515 mph)
  • Range fully loaded: 1,504 nmi (2,785 km; 1,731 mi)

 

 

Airbus A318

Airbus A318-111 F-GUGH Air France

The Airbus A318 is the smallest member of the Airbus A320 family of short- to medium-range, narrow-body, commercial passenger twin-engine jet.

  • Role: Medium range airliner
  • National origin: European Multi-national
  • Manufacturer: EADS/Airbus
  • Production line: Hamburg-Finkenwerder, Germany
  • First flight: 15 January 2002, F-WWIA
  • Introduction: 2003 with Frontier Airlines
  • Status: In service
  • Produced: 2002–present
  • Number built: 80 May 2015

Variants A320 family

Specifications

General characteristics

  • Cockpit crew: 2
  • Seating capacity: 117 (1-class, typical)
  • Overall length: 31.44 m (103 ft 2 in)
  • Wingspan: 34.10 m (111 ft 11 in) (35.8 m (117 ft 5 in) with sharklets)
  • Overall height: 12.51 m (41 ft 1 in)
  • Fuselage width: 3.95 m (13 ft 0 in)
  • Fuselage Height: 4.14 m (13 ft 7 in)
  • Operating empty weight: 39,500 kg (87,100 lb)
  • Maximum landing weight: 62.5 t (138,000 lb)
  • Maximum take-off weight: 54,500 kg (120,200 lb)
  • Engine (× 2): Pratt & Whitney PW6000 series or CFM International CFM56-5 series
  • Thrust: 96–106 kN (22,000–24,000 lbf)

Performance

  • Service ceiling: 12,000 m (39,000 ft)
  • Cruising speed: Mach 0.78 (828 km/h/511 mph at 11,000 m/36,000 ft)
  • Maximum speed: Mach 0.82 (871 km/h/537 mph at 11,000 m/36,000 ft)
  • Range fully loaded: 3,100 nmi (5,700 km; 3,600 mi)

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)

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)