FlarePathAir-accident investigation intelligence
Investigation brief · generated 2026-10-09 · source: NTSB public docket and accident database

GULFSTREAM GVI — Roswell, NM, USA, 2011-04-02

NTSB number
DCA11MA076
Operator
GULFSTREAM AEROSPACE CORPORATION
Registration
N652GD
Highest injury
Fatal · 4 fatal
Regulation
Part 091
Damage
Substantial
Cohort
Major investigation
Recorder data
Tier 1 — decoded recorder tables
Every sentence below is taken directly from NTSB records — the accident database, the docket's recorder reports and the Board's findings — with its source noted. Nothing is paraphrased or inferred.

NTSB summary

The Safety Board’s full report is available at http://www.ntsb.gov/investigations/reports_aviation.html. The Aircraft Accident Report number is NTSB/AAR-12-02. On April 2, 2011, about 0934 mountain daylight time, an experimental Gulfstream Aerospace Corporation GVI (G650), N652GD, crashed during takeoff from runway 21 at Roswell International Air Center Airport, Roswell, New Mexico. The two pilots and the two flight test engineers were fatally injured, and the airplane was substantially damaged by impact forces and a postcrash fire. The airplane was registered to and operated by Gulfstream as part of its G650 flight test program. The flight was conducted under the provisions of 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed at the time of the accident.
Verbatim, NTSB aviation accident database (narratives.narr_accf).

Probable cause

The National Transportation Safety Board determines the probable cause(s) of this accident as follows: an aerodynamic stall and subsequent uncommanded roll during a one engine-inoperative takeoff flight test, which were the result of (1) Gulfstream’s failure to properly develop and validate takeoff speeds for the flight tests and recognize and correct the takeoff safety speed (V2) error during previous G650 flight tests, (2) the G650 flight test team’s persistent and increasingly aggressive attempts to achieve V2 speeds that were erroneously low, and (3) Gulfstream’s inadequate investigation of previous G650 uncommanded roll events, which indicated that the company’s estimated stall angle of attack while the airplane was in ground effect was too high. Contributing to the accident was Gulfstream’s failure to effectively manage the G650 flight test program by pursuing an aggressive program schedule without ensuring that the roles and responsibilities of team members had been appropriately defined and implemented, engineering processes had received sufficient technical planning and oversight, potential hazards had been fully identified, and appropriate risk controls had been implemented and were functioning as intended.
Verbatim, NTSB determination.

Flight data recorder

— 293 samples, 11 parameters, 09:33:50.3 to 09:34:01.3.

ParameterMaxatMinatFinalat
Pitch attitude deg14.909:33:57.5-1.309:34:00.20.609:34:01.2
Roll attitude deg30.909:33:58.51.309:34:01.01.309:34:01.0
Vertical acceleration g2.009:34:00.70.009:33:50.30.009:34:01.3
Computed from the docket's tabular attachment; times as recorded (local or SRN as published).

Cockpit voice recorder

222 transcribed utterances from 09:23:43.5 to 09:34:04.7, 10 sources. Final entries:

09:33:57.4HOT-2no no no no. *.
09:33:58.5HOTbank angle, bank angle [electronic voice].
09:34:00.0HOT-1ah sorry guys.
09:34:02.4HOT[sound similar to triple chime alarm].
09:34:04.7HOT-?* * *. End of Transcript 09:34:10.3 [end of recording]
The NTSB cautions that a CVR transcript is not a precise science and should not be used as the sole source of information.

Recorder documents in the docket

GroupTitlePagesType
fdrData Recorder - Attachment 2 - FDR Tabular Data - Flight 153 - (CSV Format)csv
cvrCockpit Voice Recorder 12 - Factual Report of Group Chairman28pdf
performanceAircraft Performance 13 - Group Chairman's Aircraft Performance Study72pdf
performanceAircraft Performance 13 - Errata 1 to Aircraft Performance Study1pdf
performanceAircraft Performance 13 - Aircraft Performance Study Addendum #196pdf
performanceAircraft Performance 13 - Errata 1 to Addendum 13pdf
performanceAircraft Performance 13 - Errata 2 to Aircraft Performance Study1pdf

Docket: data.ntsb.gov/Docket/?NTSBNumber=DCA11MA076. This brief is an analytical aid assembled from public records; it is not an investigative finding.