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NTSB, Aggressive Test Flight Schedule, Pilot Errors Led To Crash Of Gulfstream G650
By Jim Douglas

October 11, 2012 - The National Transportation Safety Board determined on Wednesday that the probable cause of the crash of an experimental Gulfstream G650, N652GD on April 2, 2011, in Roswell, N.M., was the result of an aerodynamic stall and uncommanded roll during a planned takeoff test flight conducted with only one of the airplane's two engines operating.

The Board found that the crash was the result of Gulfstream's failure to properly develop and validate takeoff speeds and recognize and correct errors in the takeoff safety speed that manifested during previous G650 flight tests.

The Board also found that the flight test team's persistent and aggressive attempts to achieve a takeoff speed that was erroneously low; and Gulfstream's inadequate investigation of uncommanded roll events that occurred during previous flight tests, which should have revealed incorrect assumptions about the airplane's stall angle of attack in ground effect.


Contributing to the accident, the NTSB found, was Gulfstream's pursuit of an aggressive flight test schedule without ensuring that the roles and responsibilities of team members were appropriately defined, sufficient technical planning and oversight was performed, and that hazards had been fully identified and addressed with appropriate, effective risk controls. 

"In this investigation we saw an aggressive test flight schedule and pressure to get the aircraft certified," said NTSB Chairman Deborah A.P. Hersman. "Deadlines are essential motivators, but safety must always trump schedule." 

At approximately 9:34 a.m. Mountain Time, during takeoff on the accident flight, the G-650 experienced a right wing stall, causing the airplane to roll to the right with the right wingtip contacting the runway. The airplane then departed the runway, impacting a concrete structure and an airport weather station, resulting in extensive structural damage and a post-crash fire. The two pilots and two flight engineers on board were killed and the airplane was substantially damaged. 



The airplane was operating under a Federal Aviation Administration (FAA) Experimental Certificate of Airworthiness and was performing a take off with a simulated engine failure to determine take-off distance requirements at minimum flap setting. Wingtip scrape marks beginning on the runway approximately 5,300 feet from the end of the runway lead toward the final resting spot about 3,800 feet from the first marks on the runway. Witnesses close to the scene saw the airplane sliding on the ground with sparks and smoke coming from the bottom of the wing, and described the airplane being fully involved in fire while still moving across the ground. The airplane struck several obstructions and came to rest upright about 200 feet from the base of the airport control tower. Several airport rescue and fire fighting (ARFF) units responded quickly and fought the fire. 

The NTSB made recommendations to the Flight Test Safety Committee and the Federal Aviation Administration to improve flight test operating policies and encourage manufacturers to follow best practices and to coordinate high-risk flight tests. And the Board recommended that Gulfstream Aerospace Corporation commission an independent safety audit to review the company's progress in implementing a flight test safety management system and provide information about the lessons learned from its implementation to interested manufacturers, flight test safety groups and other appropriate parties. 

"In all areas of aircraft manufacturing, and particularly in flight testing, where the risks are greater, leadership must require processes that are complete, clear and include well-defined criteria," said Chairman Deborah A.P. Hersman. "This crash was as much an absence of leadership as it was of lift."
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