JEROEN VOGELAAR: Aviation Photographs

Business jet

Gulfstream G200

Gulfstream Aerospace G200 UR-PRM IBE

The Gulfstream G200, formerly known as the  Israel Aircraft Industries Galaxy Astra is a twin-engine business jet.

  • Role: Mid-sized business jet
  • National origin: Israel
  • Manufacturer: Israel Aircraft Industries/Gulfstream Aerospace
  • Production line: Israel
  • First flight: December 25, 1997
  • Introduction: 1999
  • Status: In service
  • Produced: 1997–2011
  • Number built: 350

Specifications Gulfstream G200

General characteristics

  • Crew: 2
  • Capacity: Typical Seating of 8-10, 18 Max
  • Payload: 4,050 lb (1,840 kg)
  • Length: 62 ft 3 in (18.97 m)
  • Wingspan: 58 ft 1 in (17.70 m)
  • Height: 21 ft 5 in (6.53 m)
  • Wing area: 369 ft² (34.3 m²)
  • Empty weight: 19,200 lb (8,709 kg)
  • Max. takeoff weight: 35,450 lb (16,080 kg)
  • Powerplant: 2 × Pratt & Whitney Canada PW306A turbofans, 6,040 lbf (26.9 kN) each

Performance

  • Maximum speed: Mach 0.85 (487 knots, 560 mph, 900 km/h) at altitude
  • Cruise speed: Mach 0.80 (459 knots, 528 mph, 850 km/h) normal cruise at altitude
  • Range: 3,400 nmi (3,910 mi, 6,300 km) at Mach 0.75 with 4 passengers
  • Service ceiling: 45,000 ft (13,700 m)

 

Gulfstream G550

Gulfstream G550 N917GA

Gulfstream G550 is a business jet aircraft. The Gulfstream 550 has the longest flight range in its class.

 

  • Role: Business jet
  • National origin: United States of America
  • Manufacturer: Gulfstream Aerospace
  • Production line: Savannah, Georgia
  • First flight: July 18, 2002
  • Introduction: 2004
  • Status: In service
  • Produced: 2003–present
  • Number built: 300+

Specifications G550

General characteristics

  • Crew: 2 pilots, 0–2 attendants
  • Capacity: 14–19 passengers
  • Length: 96 ft 5 in (29.4 m)
  • Wingspan: 93 ft 6 in (28.5 m)
  • Height: 25 ft 10 in (7.9 m)
  • Empty weight: 48,300 lb (21,900 kg)
  • Loaded weight: 54,500 lb (24,700 kg)
  • Useful load: 6,200 lb (2,800 kg)
  • Max. takeoff weight: 91,000 lb (41,300 kg)
  • Powerplant: 2 × Rolls-Royce BR710 turbofan, 15,385 lbf (68.44 kN) each
  • Maximum Ramp Weight: 91,400 lb (41,500 kg)
  • Maximum landing weight: 75,300 lb (34,200 kg)
  • Maximum fuel weight: 41,300 lb (18,700 kg)
  • Cabin dimensions: volume: 1,669 ft³ (47.3 m³), height: 6 ft 2 in (1.88 m), width: 7 ft 4 in (2.24 m)
  • Baggage compartment volume: 226 ft³ (6.4 m³)

Performance

  • Maximum speed: 0.885 Mach (585 mph, 941 km/h)
  • Cruise speed: 488 knots (562 mph, 0.85 Mach, 904 km/h)
  • Range: 6,750 nmi (7,768 miles, 12,500 km)
  • Service ceiling: 51,000 ft (15,500 m)
  • Takeoff distance: 5,910 ft (1,800 m)
  • Landing distance: 2,770 ft (880 m)

 

Dassault Falcon 900

Dassault Falcon 900LX HB-JTA Air Sarina AG

The Dassault Falcon 900 is a French-built corporate jet aircraft made by Dassault Aviation

  • Role: Business jet
  • National origin: France
  • Manufacturer: Dassault Aviation
  • First flight: 21 September 1984
  • Status: In service
  • Produced: 1984-present
  • Number built: 260+
  • Developed from: Dassault Falcon 50
  • Variants: Dassault Falcon 2000, Dassault Falcon 7X

Specifications (Falcon 900B)

General characteristics

  • Crew: Two
  • Capacity: 19 passengers
  • Length: 20.21 m (66 ft 4 in)
  • Wingspan: 19.33 m (63 ft 5 in)
  • Height: 7.55 m (24 ft 9.5 in)
  • Wing area: 49 m² (527 ft²)
  • Empty weight: 10,255 kg (22,608 lb)
  • Max. takeoff weight: 20,640kg (45,503 lb)
  • Powerplant: 3 × Honeywell TFE731-5BR-1C turbofan, 21.13 kN (4,750 lbf) each

Performance

  • Maximum speed: Mach 0.84-0.87
  • Cruise speed: 950 km/h (513 knots, 590 mph) at 36,000ft (10,970 m) (Mach 0.85)
  • Stall speed: 158 km/h (85 knots, 98 mph) (wheels and flaps down)
  • Range: 7,400 km (3,995 nm, 4,598 mi) (7 passengers)
  • Service ceiling: 15,500 m (51,000 ft)
  • Wing loading: 435kg/m² (91lb/ft²)

 

Eclipse 500

Eclipse Aviation Eclipse EA-500 N514EA  Private

The Eclipse 500 is a small six-seat business jet aircraft manufactured by Eclipse Aviation. Eclipse 500 became the first of a new class of Very Light Jet.

  • Role: very light jet (VLJ) class business jet
  • National origin: United States of America
  • Manufacturer: Eclipse Aviation
  • First flight: August 26, 2002
  • Introduction: December 31, 2006
  • Status: Production Halted, In service
  • Produced: January 2001- November 2008
  • Number built: 260

Specifications

General characteristics

  • Crew: one or two pilots
  • Capacity: 4 to 5 passengers
  • Length: 33 ft 1 in (10.1 m)
  • Wingspan: 37 ft 3 in (11.4 m)
  • Height: 11 ft 0 in (3.4 m)
  • Empty weight: 3,550 lb (1,610 kg)
  • Loaded weight: 5,520 lb (2,504 kg)
  • Useful load: 2,400 lb (1,089 kg)
  • Max. takeoff weight: 5,950 lb (2,699 kg)
  • Powerplant: 2 × Pratt & Whitney Canada PW610F turbofan engines, 900 lbf (4 kN flat-rated to > ISA+10C) each

Performance

  • Maximum speed: 370 knots (425 mph, 685 km/h)
  • Stall speed: 69 knots (79 mph, 128 km/h) in landing configuration
  • Range: 1,125 nmi (IFR with 45 min NBAA reserve) (1,295 mi, 2,084 km)
  • Service ceiling: 41,000 ft (12,500 m)
  • Rate of climb: 3,424 ft / min (1,044 m / min)
  • Takeoff distance: 2,345 ft (715 m)
  • Landing distance: 2,250 ft (686 m)

Avionics

  • Avio Next Generation (aka Avio NG)
  • Displays: Two 768 x 1024 resolution PFDs and one 1440 x 900 resolution MFD

Cessna 510 Citation Mustang

Cessna 510 Citation Mustang HB-VPM MyJet

 

  • Role: very light jet (VLJ) class business jet
  • National origin: United States of America
  • Manufacturer: Cessna Aircraft Company
  • Production line: Kansas
  • First flight: 23 April 2005
  • Introduction: 2006
  • Status: In service
  • Produced: 2005–present
  • Number built: 425

Specifications

General characteristics

  • Crew: one or two pilots
  • Capacity: 4 to 5 passengers
  • Length: 40 feet 7 inches (12.37 m)
  • Wingspan: 43 feet 2 inches (13.16 m)
  • Height: 13 feet 5 inches (4.09 m)
  • Empty weight: 5560 lb (2522 kg)
  • Loaded weight: 8730 lb (3960 kg)
  • Useful load: 3170 lb (1442 kg)
  • Max. takeoff weight: 8645 lb (3930 kg)
  • Powerplant: 2 × Pratt & Whitney Canada PW615F turbofans, 1460 lb thrust (6.49 kN) each

Performance

  • Maximum speed: Mach 0.63 (483 mph, 777 km/h)
  • Cruise speed: 340 ktas (390 mph, 630 km/h)
  • Range: 1167 nmi (at max. takeoff weight) (1,343 mi, 2,161 km)
  • Service ceiling: 41000 ft (12500 m)
  • Rate of climb: 3010 fpm (917 mpm)
  • Thrust/weight: 0.337 (at max. takeoff weight)
  • Takeoff distance: 3,110 ft (948 m)
  • Landing distance: 2,380 ft (729 m)

Avionics

  • Garmin G1000

 

Bombardier Global Express 5000/6000

Bombardier Global Express 6000 CS-GLC NetJets Europe

The Bombardier Global Express 5000/6000 is a large cabin, ultra long range business jet manufactured by Bombardier Aerospace in Toronto, Ontario, Canada.

  • Role: large cabin, ultra long range business jet
  • National origin: Canada
  • Manufacturer: Bombardier Aerospace
  • First flight: 13 October 1996
  • Introduction: 1993
  • Status: In service
  • Produced:
  • Number built: 500 (as of 17 June 2013)

Specifications (Global 5000)

General characteristics

  • Crew: 2-3
  • Capacity: 8 passengers in a typical configuration, up to 19 in high density arrangement
  • Length: 96 ft 10 in (29.5 m)
  • Wingspan: 94 ft 0 in (28.65 m)
  • Height: 25 ft 6 in (7.7 m)
  • Wing area: 1,022 ft² (94.75 m²)
  • Useful load: 1,775 lb (w/full fuel) (805 kg)
  • Max. takeoff weight: 92,750 lb (42,071 kg)
  • Powerplant: 2 × Rolls-Royce Deutschland BR710A2-20 turbofans, 14,750 lbf (65.6 kN) each
  • Cabin length: 42.47 f (12.94 m)
  • Cabin width (centerline): 8.17 ft (2.49 m)
  • Cabin width (floorline): 6.92 ft (2.11 m)
  • Cabin height: 6.25 ft (1.91 m)
  • Cabin floor area: 317 ft² (29.4 m²)
  • Cabin Total Volume 1,884 ft³ (53.9 m³)

Performance

  • Maximum speed: Mach .89 (513 kt, 590 mph, 950 km/h)
  • Cruise speed: Mach .85 (488 kt, 562 mph, 904 km/h)
  • Range: 5,200 nmi (9,360 km)
  • Service ceiling: 51,000 ft (15,000 m)
  • Basic Operating Weight: 50,840 lb (23,061 kg)
  • Maximum Ramp Weight: 92,750 lb (42,071 kg)
  • Maximum Takeoff Weight: 92,500 lb (41,957 kg)
  • Maximum Zero Fuel Weight: 56,000 lb (25,401 kg)
  • Maximum Fuel Weight: 39,250 lb (17,804 kg)
  • Balanced field length (SL, ISA, MTOW): 5,540 ft (1,689 m)
  • Landing distance (SL, ISA, MLW): 2,670 ft (814 m)

Avionics

  • Rockwell Collins Pro Line Fusion avionics suite

Bombardier Global Express 6000

The Global 6000 is an improved version of the original aircraft, (announced on October 6, 2003 during the NBAA Convention at Orlando, Florida) offering higher cruise speed, increased range, improved cabin layout and lighting.

Dassault Falcon 7X

Dassault Falcon 7X N889AB Bank of Utah Trustee

The Dassault Falcon 7X is a large-cabin, long range business jet manufactured by Dassault Aviation, the flagship offering of their business jet line.

  • Role: Business jet
  • National origin: France
  • Manufacturer: Dassault Aviation
  • First flight: 5 May 2005
  • Status: In service
  • Produced: 2005-present
  • Number built: 200+
  • Developed from: Dassault Falcon 50
  • Variants: Dassault Falcon 900, Dassault Falcon 2000

Specifications

General characteristics

  • Crew: Up to three
  • Capacity: Up to 19 passengers (not including crew)
  • Length: 23.19 m (76 ft 1 in)
  • Wingspan: 26.21 m (86 ft)
  • Height: 7.863 m (25 ft 8 in)
  • Wing area: 70.7 m² (761 ft²)
  • Empty weight: 15,456 kg (34,072 lb)
  • Max. takeoff weight: 31,750 kg (70,000 lb)
  • Powerplant: 3 × Pratt & Whitney Canada PW307A turbofans, 28.46 kN (6,400 lbf) each

Performance

  • Maximum speed: 953 km/h (515 knots, 593 mph)
  • Cruise speed: 900 km/h (486 knots, 559 mph)
  • Range: 11,000 km (5,940 nm) 8 passengers
  • Service ceiling: 15 500 m (51,000 ft)
  • Wing loading: 435 kg/m² (91 lb/ft²)

Avionics

  • Falcon EASy and EASy 2