JEROEN VOGELAAR: Aviation Photographs

Passenger aircraft

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

 

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

Airbus A380

Airbus A380-861 A6-EDJ Emirates

The Airbus A380 is a double-deck, wide-body, four-engine jet airliner manufactured by Airbus. It is the world’s largest passenger airliner.

  • Role: Wide-body, double-deck jet airliner
  • National origin: European Multi-national
  • Manufacturer: EADS/Airbus
  • Production line: Toulouse, France
  • First flight: 27 April 2005 F-WWOW
  • Introduction: 25 October 2007 with Singapore Airlines
  • Status: In service
  • Produced: 2005–present
  • Number built: 154 as of 28 February 2015

Operators

  • Singapore Airlines
  • Emirates
  • Qantas
  • Air France
  • Lufthansa
  • Korean Air
  • China Southern Airlines
  • Malaysia Airlines
  • Thai Airways International
  • British Airways
  • Asiana Airlines
  • Qatar Airways
  • Etihad Airways

Airbus A380 A6-EDJ Emirates

Specifications

General characteristics

  • Cockpit crew: two
  • Seating capacity: 644 (2-class) 853 (1-class)
  • Length overall: 72.73 m (238 ft 7 in)
  • Wingspan: 79.75 m (261 ft 8 in)
  • Height: 24.45 m (80 ft 3 in)
  • Wheelbase: 31.88 m (104 ft 7 in)
  • Wheel track: 12.46 m (40 ft 11 in) 14.34 m (47 ft 1 in) total width
  • Outside fuselage width: 7.14 m (23 ft 5 in)
  • Exterior fuselage height: 8.41 m (27 ft 7 in)
  • Maximum cabin width: 6.54 m (21 ft 5 in) main deck, 5.80 m (19 ft 0 in) upper deck
  • Cabin length: 49.9 m (163 ft 9 in) main deck, 44.93 m (147 ft 5 in) upper deck
  • Wing area: 845 m2 (9,100 sq ft)
  • Aspect ratio: 7.5
  • Wing sweep: 33.5°
  • Maximum taxi/ramp weight: 577,000 kg (1,272,000 lb)
  • Maximum take-off weight: 575,000 kg (1,268,000 lb)
  • Maximum landing weight: 394,000 kg (869,000 lb)
  • Maximum zero fuel weight: 369,000 kg (814,000 lb)
  • Typical operating empty weight: 276,800 kg (610,200 lb)
  • Maximum structural payload: 89,200 kg (196,700 lb)
  • Maximum cargo volume: 184 m3 (6,500 cu ft)
  • Maximum fuel capacity: 323,546 l (85,472 US gal)
  • Engines (4 ×): GP7270 (A380-861), Trent 970/B (A380-841), Trent 972/B (A380-842)

Performance

  • Maximum operating speed: Mach 0.89 (945 km/h, 587 mph, 510 knots)
  • Maximum design speed: Mach 0.96 (at cruise altitude: 1020 km/h, 634 mph, 551 knots)
  • Cruise speed: Mach 0.85
  • Take off run at MTOW/SL ISA: 2,950 m (9,680 ft)
  • Landing speed: 130-135 kn (240–250 km/h)
  • Range at design load: 15,700 km (8,500 nmi, 9,755 mi)
  • Service ceiling: 13,136 m (43,097 ft)

Embraer 190/195

Embraer E-190 PH-EZZ KLM Cityhopper

The Embraer 190/195 member of the E-Jet family a series of narrow-body medium-range twin-engine jet airliners produced by Brazilian aerospace conglomerate Embraer.

The Embraer 190/195 models are a larger stretch of the Embraer 170/175 models fitted with a new, larger wing, larger horizontal stabilizer and a new engine, the GE CF34-10E, rated at 18,500 lb (82.30 kN).

  • Role: Medium range airliner
  • National origin: Brazil
  • Manufacturer: Embraer
  • Production line: São José dos Campos, São Paulo State.
  • First flight: E190 March 12, 2004, PP-XMA, E-195 PP-XMJ on December 7, 2004
  • Status: In service
  • Produced: 2004 – present
  • Number built: E-190 515, E-195 138 April 2015
  • Variants: Embraer 170, Embraer 175, Embraer Lineage 1000
  • Developed into: Embraer E-Jet E2 family

Specifications

Embraer 190 (ERJ190-100)

General characteristics

  • Crew: Two
  • Capacity: 114 (1-class, 29 in/30 in pitch)
  • Length: 36.24 m (118 ft 11 in)
  • Wingspan: 28.72 m (94 ft 3 in)
  • Height: 10.28 m (34 ft 7 in)
  • Empty weight: 28,080 kg (61,910 lb)
  • Max Payload weight: 13,080 kg (28,840 lb)
  • Max take-off weight: 51,800 kg (114,200 lb) (AR)
  • Powerplant:  2× GE CF34-10E 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 E-190 G-LCYM BA CityFlyer

Embraer 195 (ERJ190-200)

General characteristics

  • Crew: Two
  • Capacity: 122 (1-class, 30 in/31 in pitch)
  • Length: 38.65 m  (126 ft 10 in)
  • Wingspan: 28.72 m (94 ft 3 in)
  • Height: 10.28 m (34 ft 7 in)
  • Empty weight: 28,970 kg (63,870 lb)
  • Max Payload weight: 13,080 kg (28,840 lb)
  • Max take-off weight: 13,650 kg (30,090 lb)
  • Powerplant:  2× GE CF34-10E turbofans

Performance

  • Maximum speed: 890 km/h (481 kn, Mach 0.82)
  • Range: AR: 4,077 km (2,201 nmi)
  • Service ceiling:  12,500 m (41,000 ft)

Boeing 747

Boeing 747-406(M) PH-BFE KLM

The Boeing 747 is a wide-body commercial jet airliner and cargo aircraft.

  • Role: Wide-body, long-range jet airliner
  • National origin: United States
  • Manufacturer: Boeing Commercial Airplanes
  • First flight: February 9, 1969
  • Introduction: January 22, 1970
  • Status: In service
  • Produced: 1968–present
  • Number built: 1,502 as of January 31, 2015

Variants

Boeing 747-100

First flight: February 9, 1969

The first 747-100s were built with six upper deck windows (three per side) to accommodate upstairs lounge areas. Later, as airlines began to use the upper deck for premium passenger seating instead of lounge space, Boeing offered a ten-window upper deck as an option.

General characteristics

  • Cockpit crew: 3
  • Seating capacity: 480; optional 550 (1-class, maximum)
  • Overall length: 231 ft 10 in (70.6 m)
  • Wingspan: 195 ft 8 in (59.6 m)
  • Overall height: 63 ft 5 in (19.3 m)
  • Operating empty weight: 358,000 lb (162,400 kg)
  • Maximum take-off weight: 735,000 lb (333,390 kg)
  • Cruising speed: Mach 0.84 (555 mph, 893 km/h, 481 knots )
  • Maximum speed: Mach 0.89 (594 mph, 955 km/h, 516 kn)
  • Range fully loaded: 5,300 nmi, 6,100 mi; 9,800 km
  • Engine (× 4): PW JT9D-7A/-7F/-7J RR RB211-524B2 GE CF6-45A2 (747SR)

Boeing 747-200

First flight: October 11, 1970

747-200 – The demand for longer range aircraft with increased payload quickly led to the improved −200, which featured more powerful engines, increased MTOW, and greater range than the −100.

General characteristics

  • Cockpit crew: 3
  • Seating capacity: 480; optional 550 (1-class, maximum)
  • Overall length: 231 ft 10 in (70.6 m)
  • Wingspan: 195 ft 8 in (59.6 m)
  • Overall height: 63 ft 5 in (19.3 m)
  • Operating empty weight: 383,000 lb (174,000 kg)
  • Maximum take-off weight: 833,000 lb (377,842 kg)
  • Cruising speed: Mach 0.84 (555 mph, 893 km/h, 481 knots )
  • Maximum speed: Mach 0.89 (594 mph, 955 km/h, 516 kn)
  • Range fully loaded: 6,850 nmi 7,880 mi; 12,690 km
  • Engine (× 4): PW JT9D-7R4G2 GE CF6-50E2 RR RB211-524D4

Boeing 747-300

First flight: October 5, 1982

The 747-300 features a 23-foot-4-inch-longer (7.11 m) upper deck than the −200.

General characteristics

  • Cockpit crew: 3
  • Seating capacity: 565; optional 660 (1-class)
  • Overall length: 231 ft 10 in (70.6 m)
  • Wingspan: 195 ft 8 in (59.6 m)
  • Overall height: 63 ft 5 in (19.3 m)
  • Operating empty weight: 392,800 lb (178,100 kg)
  • Maximum take-off weight: 833,000 lb (377,842 kg)
  • Cruising speed: Mach 0.84 (555 mph, 893 km/h, 481 knots )
  • Maximum speed: Mach 0.89 (594 mph, 955 km/h, 516 kn)
  • Range fully loaded: 6,700 nmi 7,700 mi; 12,400 km
  • Engine (× 4): PW JT9D-7R4G2 GE CF6-80C2B1 RR RB211-524D4

Boeing 747-400ER

First flight: April 29, 1988

The 747-400 introduced a new glass cockpit designed for a flight crew of two instead of three, with a reduction in the number of dials, gauges and knobs from 971 to 365 through the use of electronics. The type also features tail fuel tanks, revised engines, and a new interior.

General characteristics

  • Cockpit crew: 2
  • Seating capacity: 565; optional 660 (1-class)
  • Overall length: 231 ft 10 in (70.6 m)
  • Wingspan: 211 ft 5 in (64.4 m)
  • Overall height: 63 ft 6 in (19.4 m)
  • Operating empty weight: 406,900 lb (184,600 kg)
  • Maximum take-off weight: 910,000 lb (412,775 kg)
  • Cruising speed: Mach 0.855 (570 mph, 918 km/h, 495 kn)
  • Maximum speed: Mach 0.92 (614 mph, 988 km/h, 533 kn)
  • Range fully loaded: 7,670 nmi 8,830 mi; 14,200 km
  • Engine (× 4): PW 4062 GE CF6-80C2B5F RR RB211-524G/H ER: GE CF6-80C2B5F

Boeing 747-8I

First flight: March 20, 2011

The 747-800 uses the same engine and cockpit technology as the 787, hence the use of the “8”. The variant is designed to be quieter, more economical, and more environmentally friendly. The 747-8’s fuselage is lengthened from 232 to 251 feet (70.8 to 76.4 m), marking the first stretch variant of the aircraft. Power is supplied by General Electric GEnx-2B67 engines.

General characteristics

  • Cockpit crew: 2
  • Seating capacity: 605 (maximum)
  • Overall length: 250 ft 2 in (76.25 m)
  • Wingspan: 224 ft 7 in (68.5 m)
  • Overall height: 63 ft 6 in (19.4 m)
  • Operating empty weight: 472,900 lb (214,503 kg)
  • Maximum take-off weight: 987,000 lb (447,696 kg)
  • Cruising speed: Mach 0.855 (570 mph, 918 km/h, 495 kn)
  • Maximum speed: Mach 0.92 (614 mph, 988 km/h, 533 kn)
  • Range fully loaded: 8,000 nmi 9,200 mi; 15,000 km
  • Engine (× 4): GEnx-2B67

Boeing 767

Boeing 767-300ER N647UA United Airlines

The Boeing 767 is a mid- to large-size, long-range, wide-body twin-engine jet airliner built by Boeing Commercial Airplanes. It was the manufacturer’s first wide-body twinjet and its first airliner with a two-crew glass cockpit.

  • Role: Wide-body jet airliner
  • National origin: United States
  • Manufacturer: Boeing Commercial Airplanes
  • First flight: 767-200ER September 26, 1981, 767-300ER December 9, 1986, 767-400ER October 9, 1999
  • Introduction: September 8, 1982 with United Airlines
  • Status: In service
  • Produced: 1981–present
  • Number built: 1,069 through January 2015

Military variants

  • 767 Airborne Surveillance Testbed – – the Airborne Optical Adjunct (AOA) was modified from the prototype 767-200 for a United States Army program
  • E-767 – the Airborne Early Warning and Control (AWACS) platform for the Japan Self-Defense Forces
  • KC-767 Advanced Tanker – the 767-200ER-based aerial tanker developed for the USAF KC-X tanker competition
  • KC-767 Tanker Transport – the 767-200ER-based aerial refueling platform operated by the Italian Air Force (Aeronautica Militare), and the Japan Self-Defense Forces
  • Tanker conversions – the 767 MMTT or Multi-Mission Tanker Transport is a 767-200ER-based aircraft operated by the Colombian Air Force

Specifications

General characteristics

Boeing 767-200ER

  • Cockpit crew: 2
  • Seating capacity: 255, optional 290 (1-class)
  • Overall length: 159 ft 2 in (48.5 m)
  • Wingspan: 156 ft 1 in (47.6 m)
  • Overall height: 15,85 m.
  • Fuselage width: 16 ft 6 in (5.03 m)
  • Fuselage Height: 17 ft 9 in (5.41 m)
  • Operating empty weight: 181,610 lb (82,380 kg)
  • Maximum take-off weight: 395,000 lb (179,170 kg)
  • Service ceiling: 11.887 m
  • Cruising speed: Mach 0.80 (470 knots, 530 mph, 851 km/h at 35,000 ft (11,000 m) cruise altitude)
  • Maximum speed: Mach 0.86 (493 knots, 567 mph, 913 km/h at 35,000 ft (11,000 m) cruise altitude)
  • Range fully loaded: 6,385 nmi (7,348 mi; 11,825 km)
  • Engine (× 2): P&W PW4052, or 4056, GE CF6-80C2, RR RB211-524G or H
  • Thrust: PW: 63,300 lb (282 kN), GE: 62,100 lbf (276 kN)

Boeing 767-300ER

  • Cockpit crew: 2
  • Seating capacity: 290; optional 350 (1-class)
  • Overall length: 180 ft 3 in (54.9 m)
  • Wingspan: 156 ft 1 in (47.6 m)
  • Overall height: 15,85 m.
  • Fuselage width: 16 ft 6 in (5.03 m)
  • Fuselage Height: 17 ft 9 in (5.41 m)
  • Operating empty weight: 198,440 lb (90,010 kg)
  • Maximum take-off weight: 412,000 lb (186,880 kg)
  • Service ceiling: 11.887 m
  • Cruising speed: Mach 0.80 (470 knots, 530 mph, 851 km/h at 35,000 ft (11,000 m) cruise altitude)
  • Maximum speed: Mach 0.86 (493 knots, 567 mph, 913 km/h at 35,000 ft (11,000 m) cruise altitude)
  • Range fully loaded: 6,310 nmi (7,260 mi; 11,690 km)
  • Engine (× 2): P&W PW4056, 4060, or 4062. GE CF6-80C2. RR RB211-524G, or H
  • Thrust: PW: 63,300 lbf (282 kN), GE: 62,100 lbf (276 kN), RR: 59,500 lbf (265 kN)

Boeing 767-400ER

  • Cockpit crew: 2
  • Seating capacity: 375 (1-class)
  • Overall length: 201 ft 4 in (61.4 m)
  • Wingspan: 170 ft 4 in (51.9 m)
  • Overall height: 15,85 m.
  • Fuselage width: 16 ft 6 in (5.03 m)
  • Fuselage Height: 17 ft 9 in (5.41 m)
  • Operating empty weight: 229,000 lb (103,870 kg)
  • Maximum take-off weight: 395,000 lb (179,170 kg)
  • Service ceiling: 11.887 m
  • Cruising speed: Mach 0.80 (470 knots, 530 mph, 851 km/h at 35,000 ft (11,000 m) cruise altitude)
  • Maximum speed: Mach 0.86 (493 knots, 567 mph, 913 km/h at 35,000 ft (11,000 m) cruise altitude)
  • Range fully loaded: 5,625 nmi (6,473 mi; 10,418 km)
  • Engine (× 2): P&W PW4062 GE CF6-80C2
  • Thrust: PW: 63,300 lbf (282 kN) GE: 63,500 lbf (282 kN)

Airbus A321

Airbus A321-231 P4-NAS Air Astana

The A321 is the largest member of the Airbus A320 Family. The basic A321-100 features a reduction in range compared to the A320, an extra fuel tank was not added to the initial design to compensate for the extra weight.

  • Role: Narrow-body jet airliner
  • National origin: European Multi-national
  • Manufacturer: EADS/Airbus
  • Production line: Hamburg – Finkenwerder, Germany
  • First flight: March 11, 1993. F-WWIA
  • Introduction: January 27, 1994 to Lufthansa, D-AIRA
  • Status: In service
  • Produced: 1993–present
  • Number built: 1,036 February 2015

Variants A320 family

Specifications

General characteristics

  • Cockpit crew: 2
  • Seating capacity: – 199 one class
  • Overall length: 44.51 m (146 ft 0 in)
  • Wingspan: 34.10 m (111 ft 11 in) (35.8 m (117 ft 5 in) with sharklets)
  • Overall height: 11.76 m (38 ft 7 in)
  • Fuselage width: 3.95 m (13 ft 0 in)
  • Fuselage Height: 4.14 m (13 ft 7 in)
  • Operating empty weight: 48,500 kg (106,900 lb)
  • Maximum landing weight: 77.8 t (172,000 lb)
  • Maximum take-off weight: 93.5 t (206,000 lb)
  • Engine (× 2):
  • – CFM International CFM56-5A1 rated 111.2 kN.
  • – CFM International CFM56-5A3 rated 117.88 kN.
  • – CFM International CFM56-5B4 rated 117.9 kN.
  • – International Aero Engines V2500-A1 rated 111.2 kN.
  • – International Aero Engines V2527-A5 rated 117.9 kN.

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: 3,200 nmi (5,900 km; 3,700 mi) with sharklets

 

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)

Airbus A319

Airbus A319-111 G-EZET easyJet

Airbus A319 is a minimum change, shortened derivative of the highly successful A320.

  • Role: Medium range airliner
  • National origin: European Multi-national
  • Manufacturer: EADS/Airbus
  • Production line: Hamburg-Finkenwerder, Germany
  • First flight: August 25, 1995 F-WWDB
  • Introduction: April 1996. Swissair
  • Status: In service
  • Produced: 1995 – present
  • Number built: 1,433 February 2015

Variants A320 family

Specifications

General characteristics

  • Cockpit crew: 2
  • Seating capacity: 134
  • Overall length: 33.84 m (111 ft 0 in)
  • Wingspan: 34.10 m (111 ft 11 in) (35.8 m (117 ft 5 in) with sharklets)
  • Overall height: 11.76 m (38 ft 7 in)
  • Fuselage width: 3.95 m (13 ft 0 in)
  • Fuselage Height: 4.14 m (13 ft 7 in)
  • Operating empty weight: 40,800 kg (89,900 lb)
  • Maximum landing weight: 62.5 t (138,000 lb)
  • Maximum take-off weight: 75.5 t (166,000 lb)
  • Engine (× 2):
  • Two CFM International CFM56-5A4 rated 97.89 kN.
  • Two CFM International CFM56-5A5 rated 104.53 kN.
  • Two CFM International CFM56-5B5 rated 97.89 kN.
  • Two CFM International CFM56-5B6 rated 104.53 kN.
  • Two International Aero Engines V2522-A5 rated 102.66 kN.
  • Two International Aero Engines V2524-A5 rated 109.06 kN.

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: 3,600 nmi (6,700 km; 4,100 mi), 3,700 nmi (6,900 km; 4,300 mi) with sharklets

 

Airbus A319-112 OK-OER SkyTeam (CSA - Czech Airlines)

Airbus A319-112 OK-OER SkyTeam (CSA – Czech Airlines)