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The G450 is a designation for the model GIV-X, approved by the FAA on August 12, 2004, as is the G350, which has a reduced fuel capacity. Compared to the Gulfstream IV , its fuselage is 12 inches longer and the main entry door relocated aft.
The two larger models were unveiled on October 14, 2014 and the smaller G400 was unveiled on October 4, 2021. The G500 was first delivered on September 27, 2018, and the longer G600 was first delivered August 8, 2019. The G500 will replace the G450 while the larger G600 will succeed the G550. The smaller G400 meanwhile has not yet been ...
The Gulfstream G650 is a large business jet produced by Gulfstream Aerospace. [3] The model is designated Gulfstream GVI in its type certificate. [4] The aircraft can be configured to carry from 11 to 18 passengers over a range of 7,000 nautical miles [nmi] (13,000 km; 8,100 mi) at a top speed of Mach 0.925 (530.6 kn; 982.7 km/h; 610.6 mph).
G550 cabin. The first production G550 (GV-SP) flew on 18 July 2002 and the aircraft received its FAA type certificate on August 14, 2003. [3] [4] In 2014, Gulfstream looked at a re-engine with the Rolls-Royce Pearl BR700 development announced in May 2018 for the new Global Express 5500 and 6500 variants but preferred the BR725-powered, 7,500 nmi G650. [5]
Gulfstream IV/G400/G450 The Gulfstream III , a business jet produced by Gulfstream Aerospace , is an improved variant of the Grumman Gulfstream II . The U.S. military uses versions of the Gulfstream III as the C-20A/B/C/D/E aircraft, though later C-20 F/G/H/J are Gulfstream IV.
A major inspection every 180 months cost $800,000-1.2 million. Two 8,000h engine overhauls can cost $4 million. The cheaper and more efficient Gulfstream G450 or Falcon 900LX are slower, have less range and smaller cabins. [39]
Gulfstream G400/G450; Gulfstream G500/G550 This page was last edited on 24 July 2022, at 15:26 (UTC). Text is available under the Creative Commons Attribution ...
Operating ceiling is increased from 45,000 to 51,000 ft (14,000 to 16,000 m). It has thrust reversers and composite flight control surfaces. The horizontal tail area is 30% larger, wingspan is increased from 74.6 to 93.5 ft (22.7 to 28.5 m), the fuselage is lengthened by 5 ft (1.5 m) forward of the main entry door, and by 2 ft (0.6 m) aft of ...