Fourth G650 Now In Flight Test Program | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

** AIRBORNE 05.21.13 Aero-TV-- CLICK HERE! ** HD iPad-Friendly Version -- AIRBORNE 05.21.13 **

** AIRBORNE 05.17.13 Aero-TV-- CLICK HERE! ** HD iPad-Friendly Version -- AIRBORNE 05.17.13 **

** AIRBORNE 04.01.13 SPECIAL EDITION of Aero-TV-- CLICK HERE! ** HD iPad-Friendly Version -- AIRBORNE 04.01.13 SPECIAL EDITION **

Tue, Jun 22, 2010

Fourth G650 Now In Flight Test Program

First Production Aircraft To Begin Testing

A fourth aircraft is now part of the Gulfstream G650 flight-test program, Gulfstream Aerospace announced Monday. The newest test aircraft flew for the first time June 6 and has spent more than five hours in the air.

Unlike its three predecessors, the fourth G650 (S/N 6004) is a production aircraft. S/N 6004 will be the first G650 outfitted and tested with a full interior, which will be installed later this summer. The aircraft, which will be used to evaluate the aircraft's cabin systems, is expected to resume flight testing following the installation.


File Photo

The G650 flight-test program involves an estimated 1,800 hours of flight and a specific purpose for each of five aircraft. S/N 6001 is focused on envelope expansion, air data calibration, flutter, in-flight performance and flight controls. S/N 6002 is used to evaluate the aircraft's systems, while S/N 6003 tests the avionics, in-flight load measurement and ice protection system. S/N 6005, which has been turned over to the Flight Test department for outfitting, will participate in the reduced vertical separation minimum testing.

The G650 flight-test program officially began on Nov. 25, 2009. Through June 20, the four aircraft currently in the program have completed more than 85 flights and 240 flight-test hours.

Ultimate load testing of the aircraft's primary structural components has also begun. In April, the aircraft completed the structural limit load testing required by the FAA and the EASA. The limit load represents the maximum load the aircraft should experience during its life cycle. Ultimate load is 50 percent more than limit load. Ultimate load testing will be performed on the fuselage, wing, vertical and horizontal stabilizers, nose landing gear and all control surfaces.


File Photo

The G650 has also flown at its maximum takeoff weight of 99,600 pounds and recently reached its maximum operational Mach number of Mach 0.925 at 42,500 feet.

The aircraft is expected to receive certification from the FAA and EASA in 2011. It is on schedule to enter service in 2012.

FMI: www.gulfstream.com

Advertisement

More News

Four Companies Recognized With 2013 EBAA Safety Of Flight Awards

Cited For Focus On Maintaining And Improving Best Practices Four European companies have been recognized for their commitment to safe operations as recipients of the 2013 European >[...]

Classic Aero-TV: Viking Engines--Building A Rep For Alternative SportAv Engines

Rotax Is NOT The Only Player In Sport Aviation Propulsion Ya gotta hand to Viking... in an industry so VERY well dominated by Rotax, it takes some serious talent and extraordinary >[...]

ANN's Daily Aero-Linx (05.22.13)

The European Cockpit Association The European Cockpit Association (ECA) was created in 1991 and is the representative body of European pilots at European Union (EU) level. It repre>[...]

ANN's Daily Aero-Term (05.22.13): Known Traffic

With respect to ATC clearances, means aircraft whose altitude, position, and intentions are known to ATC.>[...]

Aero-News: Quote Of The Day (05.22.13)

"(T)he PC-24 is a completely new development – not a 'me too product'." Source: Oscar J. Schwenk, Chairman of the Board of Directors of Pilatus, introducing the company's new>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2013 Web Development & Design by Pauli Systems, LC