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 Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-05.06.24

Airborne-NextGen-05.07.24

Airborne-Unlimited-05.08.24 Airborne-FlightTraining-05.09.24

Airborne-Unlimited-05.10.24

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

Airborne-Flight Training 05.09.24: ERAU at AIAA, LIFT Diamond Buy, Epic A&P

Also: Vertical Flight Society, NBAA Maintenance Conference, GA Honored, AMT Scholarship For the first time, students from Embry-Riddle’s Daytona Beach, Florida, campus took t>[...]

ANN's Daily Aero-Term (05.07.24): Hazardous Weather Information

Hazardous Weather Information Summary of significant meteorological information (SIGMET/WS), convective significant meteorological information (convective SIGMET/WST), urgent pilot>[...]

Aero-News: Quote of the Day (05.07.24)

"The need for innovation at speed and scale is greater than ever. The X-62A VISTA is a crucial platform in our efforts to develop, test and integrate AI, as well as to establish AI>[...]

NTSB Final Report: Cessna 150

(FAA) Inspector Observed That Both Fuel Tanks Were Intact And That Only A Minimal Amount Of Fuel Remained In Each Analysis: According to the pilot, approximately 8 miles from the d>[...]

Aero-News: Quote of the Day (05.08.24)

“Pyka’s Pelican Cargo is unlike any other UAS solution on the market for contested logistics. We assessed a number of leading capabilities and concluded that the Pelica>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2024 Web Development & Design by Pauli Systems, LC