JEROEN VOGELAAR: Aviation Photographs

Narrow-body

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

Fokker 70

Fokker 70 PH-KZM KLM Cityhopper

The Fokker 70 is a narrow-body, twin-engined, medium-range, turbofan airliner produced by Fokker as a smaller version of the Fokker 100 jetliner.

  • Role: Narrow-body Regional jet airliner
  • National origin: Netherlands
  • Manufacturer: Fokker
  • First flight: 4 April 1993
  • Introduction: October 1994 with Ford Motor Company
  • Status: Out of production, in service
  • Produced: 1992-1997
  • Number built: 47 (+1 prototype)
  • Developed from: Fokker F28 Fellowship
  • Variants: Fokker 100

Specifications

General characteristics

  • Crew: two
  • Capacity:
    85 (1-class, maximum at 76 cm (30 in) seat pitch)
    79 (1-class, typical at 81 cm (32 in) seat pitch)
    72 (2-class, typical at 91 cm (36 in) and 81 cm (32 in) seat pitches)
  • Length: 30.91 m (101 ft 5 in)
  • Wingspan: 28.08 m (92 ft 2 in)
  • Width: 3.30 m (10 ft 10 in)
  • Height: 8.5 m (27.89 ft 11 in)
  • Empty weight: 22.673 kg (49.985 lb)
  • Powerplant: 2 × Rolls-Royce Tay 620, 61.6 kN (13.850 lbf) thrust each

Performance

  • Cruising speed: 845 km/h (525 mph)
  • Range: 3.410 km (2.119 miles)
  • Service ceiling: 11.000 m (36.089 ft)

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)