Hawker Aircraft Ltd HAWKER HUNTER MK.58 accident near Oxnard, CA
On October 30, 2014, a Hawker Aircraft Ltd HAWKER HUNTER MK.58 (airplane) was involved in an accident near Oxnard, CA. 1 person died. Damage to the aircraft: destroyed.
- Date
- October 30, 2014
- Place
- Oxnard, CA
- Aircraft
- Hawker Aircraft Ltd HAWKER HUNTER MK.58 · Airplane
- Injuries
- 1 fatal, 0 serious, 0 minor
- Damage
- Destroyed
- Position
- 34.117°N, 119.082°W
- NTSB ID
- 20141029X13346
Official records · WPR15GA030
- Public docket: reports, statements and exhibits from the investigation
NTSB summary
HISTORY OF FLIGHTOn October 29, 2014, at 1711 Pacific daylight time, a Hawker Hunter Mk 58, single-seat turbojet fighter aircraft, N332AX, crashed while on approach to Naval Air Station (NAS) Point Mugu, California (NTD). The airline transport pilot was killed, and the airplane was destroyed by impact forces and postimpact fire. The airplane was registered to Airborne Tactical Advantage Company (ATAC) and the non-military public flight was operated under contract to Naval Air Systems Command (NAVAIR) in accordance with the provisions of 49 United States Code (USC) Sections 40102 and 40125. Visual meteorological conditions existed at the accident site and the flight was operated on a visual flight rules flight plan. The purpose of the flight was to support adversary and electronic warfare training with Carrier Strike Group 15 (CSG15). The accident airplane departed NTD at 1500 as the wingman in a flight of two Hunters, intending to participate in an adversarial support air defense training exercise offshore in warning area W291. The flight's radio call sign was "ATAC 11," and the accident airplane was "ATAC 12." The accident occurred during the "overhead break" arrival to land on runway 21. The procedures were to fly as a flight of two with ATAC 12 making a left break 4 seconds after the lead airplane, ATAC 11. ATAC 12 was to follow the lead in a descending, 270-degree turn to enter the downwind leg for runway 21. At the initiation of the base leg, the pilot was to make a continuous, descending, 180-degree turn, and roll out on final approach to land on runway 21. The normal
Probable cause
The pilot's failure to maintain adequate airspeed during the approach for landing, which resulted in the airplane exceeding its critical angle of attack and experiencing an aerodynamic stall/spin at an altitude too low for recovery.
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Source: NTSB aviation accident database (US government, public domain). Findings may be preliminary or later revised by the NTSB. Not a complete global record.