JEROEN VOGELAAR: Aviation Photographs

airliner

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)

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)

 

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

 

Fokker 100

Fokker 100 PH-MJP Greenland Express

  • Role: Narrow-body Regional jet airliner
  • National origin: Netherlands
  • Manufacturer: Fokker
  • First flight: 30 November 1986
  • Introduction: April 5, 1988 with Swissair
  • Status: Out of production, in service
  • Produced: 1986-1997
  • Number built: 283
  • Developed from: Fokker F28 Fellowship
  • Variants: Fokker 70

Specifications

General characteristics

  • Cockpit crew: Two
  • Seating capacity: 122 (1-class, maximum)
  • Overall length: 35.53 metres (116 ft 7 in)
  • Wingspan: 28.08 metres (92 ft 2 in)
  • Wing area: 93.5 square metres (1,006 sq ft)
  • Overall height: 8.50 metres (27 ft 11 in)
  • Fuselage width: 3.30 m (10 ft 10 in)

Fokker 100 with Rolls-Royce Tay Mk 620-15

  • Operating empty weight: 24,375 kilograms (53,738 lb)
  • Maximum payload weight: 11,242 kilograms (24,784 lb)
  • Maximum take-off weight: 43,090 kilograms (95,000 lb)
  • Engine (× 2): Rolls-Royce Tay Mk 620-15, thrust 13,850 lbf (61.6 kN)

Performance

  • Service ceiling: 35,000 ft (11,000 m)
  • Cruising speed: 845 km/h (525 mph, 456 kn), Mach 0.77
  • Range fully loaded: 1,323 nautical miles (2,450 km; 1,522 mi)

Fokker 100 with Rolls-Royce Tay Mk 650-15

  • Operating empty weight: 24,541 kilograms (54,104 lb)
  • Maximum payload weight: 11,993 kilograms (26,440 lb)
  • Maximum take-off weight: 45,810 kilograms (100,990 lb)
  • Engine (× 2): Rolls-Royce Tay Mk 650-15 thrust 15,100 lbf (67.2 kN)

Performance

  • Service ceiling: 35,000 ft (11,000 m)
  • Cruising speed: 845 km/h (525 mph, 456 kn), Mach 0.77
  • Range fully loaded: 1,710 nautical miles (3,170 km; 1,970 mi)