JEROEN VOGELAAR: Aviation Photographs

Civilian aviation

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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)

Airbus A320

Airbus A320-216 EC-LVQ Iberia Express

Airbus A320 is the basis for a whole family of airliners, now including the A318, A319 and A321.The A320 was the first narrow body airliner from Airbus.

  • Role: Narrow-body jet airliner
  • National origin: European Multi-national
  • Manufacturer: EADS/Airbus
  • Production line: Toulouse – Blagnac, France
  • First flight: 22 February 1987 F-WWAI
  • Introduction: 18 April 1988 with Air France
  • Status: In service
  • Produced: 1986–present
  • Number built: 3,867 February 2015

Airbus A320-214 TC-FBO Freebird Airlines

Variants A320 family

Specifications

General characteristics

  • Cockpit crew: 2
  • Seating capacity: – 156 one class
  • 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):
  • – 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: 3,600 nmi (6,700 km; 4,100 mi), 3,700 nmi (6,900 km; 4,300 mi) with sharklets

 

Boeing 737

Boeing 737-800 OM-CEX Air Explore

Boeing 737 Next Generation (737NG) series includes four variants and can seat between 110 to 210 passengers.

  • Role: Narrow-body jet airliner
  • National origin: United States
  • Manufacturer: Boeing Commercial Airplanes
  • First flight: February 9, 1997
  • Introduction: 1998 with Southwest Airlines
  • Status: In service
  • Produced: 1996–present
  • Number built: 5,000 as of July 16, 2014

Specifications

Boeing 737-600

  • Cockpit crew: 2
  • Seating capacity: 149 (1-class, maximum)
  • Overall length: 102 ft 6 in  (31.2 m)
  • Wingspan: 117 ft 5 in  (35.7 m)
  • Overall height: 41 ft 3 in  (12.6 m)
  • Fuselage width: 12 ft 4 in (3.76 m)
  • Fuselage Height: 13 ft 2 in (4.01 m)
  • Operating empty weight: 80,031 lb  (36,378 kg)
  • Maximum landing weight: 120,500 lb  (54,658 kg)
  • Maximum take-off weight: 145,500 lb  (66,000 kg)
  • Service ceiling: 41,000 ft  (12,500 m)
  • Cruising speed: Mach 0.785 (447 kn, 514 mph, 828 km/h)
  • Maximum speed: Mach 0.82 (475 kn, 544 mph, 876 km/h)
  • Range fully loaded: 3,050 nmi (5,648 km)
  • Engine (× 2): CFM 56-7B20

Boeing 737-700

Boeing 737-7K2 KLM

  • Cockpit crew: 2
  • Seating capacity: 149 (1-class, dense)
  • Overall length: 110 ft 4 in  (33.6 m)
  • Wingspan: 117 ft 5 in  (35.7 m)
  • Overall height: 41 ft 3 in  (12.6 m)
  • Fuselage width: 12 ft 4 in (3.76 m)
  • Fuselage Height: 13 ft 2 in (4.01 m)
  • Operating empty weight: 84,100 lb  (38,147 kg)
  • Maximum landing weight: 134,000 lb  (60,781 kg)
  • Maximum take-off weight: 154,500 lb  (70,080 kg)
  • Service ceiling: 41,000 ft  (12,500 m)
  • Cruising speed: Mach 0.785 (447 kn, 514 mph, 828 km/h)
  • Maximum speed: Mach 0.82 (475 kn, 544 mph, 876 km/h)
  • Range fully loaded: 3,365 nmi (6,230 km)
  • Engine (× 2): CFM 56-7B26

Boeing 737-800

Boeing 737-8EH PR-GUB Gol Transportes Aereos

  • Cockpit crew: 2
  • Seating capacity: 189 (1-class, dense)
  • Overall length: 129 ft 6 in  (39.5 m)
  • Wingspan: 117 ft 5 in  (35.7 m)
  • Overall height: 41 ft 3 in  (12.6 m)
  • Fuselage width: 12 ft 4 in (3.76 m)
  • Fuselage Height: 13 ft 2 in (4.01 m)
  • Operating empty weight: 91,108 lb  (41,413 kg)
  • Maximum landing weight: 146,300 lb  (66,361 kg)
  • Maximum take-off weight: 174,200 lb  (79,010 kg)
  • Service ceiling: 41,000 ft  (12,500 m)
  • Cruising speed: Mach 0.785 (447 kn, 514 mph, 828 km/h)
  • Maximum speed: Mach 0.82 (475 kn, 544 mph, 876 km/h)
  • Range fully loaded: 3,060 nmi (5,665 km)
  • Engine (× 2): CFM 56-7B27

Boeing 737-900

Boeing 737-958ER 4X-EHD El Al Israel Airlines

  • Cockpit crew: 2
  • Seating capacity: 220 (1-class high density, maximum certificated)
  • Overall length: 138 ft 2 in  (42.1 m)
  • Wingspan: 117 ft 5 in  (35.7 m)
  • Overall height: 41 ft 3 in  (12.6 m)
  • Fuselage width: 12 ft 4 in (3.76 m)
  • Fuselage Height: 13 ft 2 in (4.01 m)
  • Operating empty weight: 98,495 lb  (44,676 kg)
  • Maximum landing weight: 157,300 lb   (71,350 kg)
  • Maximum take-off weight: 187,700 lb  (85,130 kg)
  • Service ceiling: 41,000 ft  (12,500 m)
  • Cruising speed: Mach 0.785 (447 kn, 514 mph, 828 km/h)
  • Maximum speed: Mach 0.82 (475 kn, 544 mph, 876 km/h)
  • Range fully loaded: ,265 NM (6,045 km) in 2 class layout
  • Engine (× 2): CFM 56-7B27

Boeing 737-8K2 PH-HZG Transavia

 

 

AgustaWestland AW109

AgustaWestland AW109SP HB-ZRT REGA

  • Role: SAR/utility helicopter
  • Manufacturer: Anglo-Italian manufacturer AgustaWestland
  • First flight: 4 August 1971
  • Introduction: 1976
  • Status: Active service In production
  • Produced: 1971-present

Specifications (AW109 Power with PW206C)

General characteristics

  • Crew: 1 or 2
  • Capacity: 6 or 7 passengers
  • Length: 11.448 m (37 ft 7 in) fuselage
  • Width: 2.88 m (9 ft 5 in)
  • Height: 3.50 m (11 ft 6 in)
  • Empty weight: 1,590 kg (3,505 lb)
  • Max takeoff weight: 2,850 kg (6,283 lb)
  • Powerplant: 2 × Pratt & Whitney Canada PW206C Turboshaft engine, 418 kW (561 hp) each
  • Main rotor diameter: 11.00 m (36 ft 1 in)

Performance

  • Maximum speed: 285 km/h (177 mph; 154 kn)
  • Ferry range: 932 km (579 mi; 503 nmi)
  • Rate of climb: 9.8 m/s (1,930 ft/min)

Pilatus PC-12

Pilatus PC-12.47E HB-FVY Pilatus Aircraft Factory

  • Role: Passenger and cargo aircraft
  • National origin: Switzerland
  • Manufacturer: Pilatus Aircraft
  • First flight: 31 May 1991
  • Introduction: 1994
  • Status: Active service, in production

Pilatus PC-12 HB-FVJ Privat

Specifications

General characteristics

  • Crew: one or two pilots
  • Capacity: 9 passengers standard, 6-8 executive
  • Payload: 1,500 kg (3,502 lb)
  • Length: 14.40 m (47 ft 3 in)
  • Wingspan: 16.23 m (53 ft 3 in)
  • Height: 4.26 m (14 ft 0 in)
  • Wing area: 25.81 m² (277.8 ft²)
  • Empty weight: 2,761 kg (5,867 lb)
  • Loaded weight: 4,700 kg (10,450 lb)
  • Max. takeoff weight: 4,740 kg (10,450 lb)
  • Powerplant: 1 × Pratt & Whitney Canada PT6A-67B or -67P turboprop, 895 kW (1,200 shp)
  • Maximum landing: 4,500 kg (9,921 lb)
  • Maximum payload full fuel: 539 kg (1,189 lb)
  • Tail wingspan: 5.20 m (17 ft 1 in)
  • Propeller: Hartzell HC – E4A – 3D/E10477K – 4 blade aluminum
  • Propeller diameter: 2.67 m (8 ft 9 in)
  • Propeller RPM: 1,700 rpm

Performance

  • Cruise speed: 500 km/h (312.5 mph/270 KTAS/280 KTAS @ 20000 ft (PC-12NG))
  • Stall speed: 120 km/h (74.8 mph/ 65 KCAS/66 KCAS (PC-12NG))
  • Service ceiling: 9,150 m (30,000 ft)
  • Rate of climb: 512 m/min at sea level (1,680 ft/min)
  • Wing loading: 174.3 kg/m² (35.7 lb/ft²)
  • Power/mass: 3.7 kg/shp (8.2 lb/shp)
  • Range 0 passenger: 3,389 km (1,830 nm)
  • Range 9 passenger: 2,804 km (1,753 mi) (1,513 nm)
  • Takeoff distance over 15 m (50 ft) obstacle: 701 m (2,300 ft)
  • Takeoff distance ground roll: 450 m (1,475 ft)
  • Landing distance over 15 m (50 ft) obstacle: 558 m (1,830 ft)
  • Landing distance ground roll: 228 m (945 ft)
  • Climb to 30,000 ft: 26.5 minutes
  • Fuel consumption: 360 pounds per hour (54 gph)

Avionics
Honeywell Primus Apex (PC-12NG)

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