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Universal Avionics Vision 1

Gulfstream Announces G450

Attention heavy-iron enthusiasts: The wait finally is over. Monday morning, Pres Henne, Gulfstream Aerospace's senior VP engineering, programs and test, officially announced development of the G450, the next-generation GIV featuring upgraded Rolls-Royce Tay 611-8C turbofans, Primus Epic PlaneView avionics, standard HUD with EVS and a 12-inch fuselage stretch.

The G-1159C family, including GIV, GIV-SP, G300 and G400, has been a best seller for Gulfstream, with more than 500 deliveries since its introduction 1987. In recent years, though, the world economic downturn, coupled with competition from Bombardier and Dassault, has softened demand for the G-1159C (indeed, Gulfstream recently dropped the price of a G400 from $32.5 million to $31 million).

In response, Gulfstream launched design studies for the G450, formerly known as GIV-X, immediately after the firm built its first G550 prototype in 2001. "This is the first time we've executed a parallel development program with two models," Henne said.

Serial Number 4001, the first of four G450 development aircraft, started flight tests on April 30, 2003. S/n 4002 flew on June 21, s/n 4003 soared on June 22 and s/n 4004, on static display at Orlando Executive, first flew on September 18. FAA certification is slated for third quarter 2004. EASA approval is scheduled for fourth quarter 2004 and the first customer deliveries should occur in mid-2005, according to the current plan.

Priced at $33 million, the newest Gulfstream will be able to fly eight passengers 4,350 nmi at Mach 0.80 and land with NBAA IFR reserves, taking square aim at Dassault's $34.35 million Falcon Jet 900EX. The G450 also will be able to fly eight passengers 3,300 nmi at Mach 0.85. "Everybody wants to go fast," Henne explained.

Notably, the G450 will weigh 800 to 900 pounds less than the G400 and with a 73,900 pound MTOW will have 200 pounds more tanks-full payload. Less weight will enable the G450 to climb directly to FL 410 in 23 minutes, plus it will offer improved hot-and-high airport performance. The G450, for example, will have a 7,890-ft TOFL when departing from B/CA's 5,000-ft elevation, ISA+20°C airport, Henne predicted. That's five percent less than a G400 departing under the same conditions. The newest Gulfstream, though, will have the same 5,450 ft TOFL at sea-level/ISA as a G400 due to more stringent FAR Part 25 certification requirements.

The 250 nmi range increase compared to the G400 primarily is the result of fitting the aircraft with 13,850 pounds thrust Tay 611-8C engines, featuring larger, more efficient fans borrowed from Tay 650, improved hot section parts and FADECs. The ­8C also has two percent better specific fuel consumption, in part due to a redesigned deep-fluted mixer nozzle. The engines are housed inside G550-style composite nacelles fitted with single-pivot thrust reversers. Numerous small drag reduction improvements also help boost maximum range. Operators can plan on 6,000-hour HSI intervals and 12,000-hour TBOs, a 50% increase over the original ­8 engines.

Up front, the G450 will sport the G550's entire nose section, including its PlaneView avionics suite. The cabin door is moved three feet aft to provide the crew with almost one-third more cockpit volume, for 12 in more legroom and storage space. This was immediately apparent when Show News toured the G450 on Sunday afternoon with Randy Gaston, Gulfstream's chief pilot.
PlaneView not only improves flight situational awareness, it also occupies two feet less cabin length. As a result, a more compact, left side equipment rack now is located forward of the door, eliminating the congestion in the entryway to the cabin.

The G450 actually shares more in common with the G550 than the G400. "We asked (G300/400) customers to tell us about their top ten reliability concerns. Changes on the G450 address nine of those ten issues," Henne said. Gone are the late model GIII/GIV wild-frequency AC generators and Bendix AC/DC power converters. The G450 will be fitted with more conventional and highly reliable integrated drive generators, plus the rest of the G550's electrical system, including its no-break power transfer feature. A new Honeywell 36-150GIV APU, fitted with a 40 Kva generator, will replace the 36-100G that has a 30 Kva generator. The -150GIV can be started and run up to FL 370 and it puts out 44% more bleed air for better engine starting and air conditioning. Noise sensitive airport neighbors will appreciate the -150GIV's greatly reduced EPNdB noise levels.

The G450 will be fitted with higher output G550 air-conditioning packs, dual digital pressurization system, three-zone cabin temperature control and a 6,000 foot maximum cabin altitude-500 feet lower than that of G400. The cabin altitude at FL 410 will be 5,000 feet. The new aircraft will be fitted with G550's heated cabin windows. New ABS wheels and brakes, including a digital anti-skid system will be fitted to G450. The newest Gulfstream also has G550's passive cabin door seal and most of its advanced Honeywell Primus Epic maintenance diagnostic functions. Pilots will appreciate the G450's greater aileron boost ratio that reduces roll control effort to G500/550 levels. As a result of all these changes, pilots will need GV/G550 type ratings to fly it, not the GIV endorsement on their certificates.

-Fred George

The G450's Primus Epic PlaneView avionics suite has four 14-inch LCDs with 35% more viewing area than the G400's six DU880 CRTs, plus full triplex synchronous FMSes, triple MCDUs in the console and ergonomically designed, left- and right-side armrests with integrated cursor control devices (CCDs) and push-to-talk switches. The large format LCDs feature wall-to-wall sky/earth attitude indicators, I-NAV plan view charts and fully integrated systems synoptic diagrams. The CCDs aren't required for dispatch, but when convenient they can be used for graphical flight planning, radio tuning and I-NAV control.

Gulfstream's Visual Guidance System, with its standard infrared Enhanced Vision System sensor, enables pilots to see images of terrain and runway lights well beyond natural vision range in conditions of fog or darkness. The FAA recently issued a Notice of Proposed Rule Making with the intention of affording operational credit for use of EVS in low visibility conditions.

Honeywell LASEREF V IRS units, Modular Radio Units, and Modular Avionics Units reduce by 16 the number of remote boxes. The PlaneView should provide 32% better reliability than SPZ8000 series avionics, while reducing weight, volume and power consumption.

 



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