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1966 Felthorpe Trident crash
Crash of a Trident airliner in a pre-delivery flight in 1966
Crash of a Trident airliner in a pre-delivery flight in 1966
| Field | Value |
|---|---|
| name | Felthorpe Trident crash |
| occurrence_type | Accident |
| image | Trident 62a.jpg |
| image_upright | 1.15 |
| caption | A Trident identical to the accident aircraft, here photographed during a display flight |
| date | |
| summary | Deep stall due to pilot error |
| site | Felthorpe, Norfolk, United Kingdom |
| coordinates | |
| aircraft_type | Hawker Siddeley Trident 1C |
| operator | Hawker Siddeley |
| tail_number | G-ARPY |
| origin | Hatfield Aerodrome |
| destination | Hatfield Aerodrome |
| occupants | 4 |
| crew | 4 |
| fatalities | 4 |
| survivors | 0 |
On 3 June 1966, a newly built Hawker Siddeley Trident jetliner crashed during a pre-delivery test flight near the village of Felthorpe, Norfolk, England, killing all four crew. The aeroplane had entered a deep stall from which the crew were unable to recover. It was the first loss of a Trident aircraft.
Aircraft and crew
Aircraft
The aircraft involved was a tri-jet Hawker Siddeley Trident 1C, registration that was about to be delivered to British European Airways.
Crew
The crew were pilots Peter Barlow and George Errington, and technicians E. Brackstone-Brown and G.W. Patterson.
Accident flight
The aircraft was making its first flight, which was a routine test flight to enable the aircraft's Certificate of Airworthiness to be issued. There were four crew on board. The aircraft took off from Hatfield Aerodrome at 16:52. Tests established that the stick shaker operated at 102 kn, and that stall recovery system operated at 93 kn. The crew then disconnected the stall warning systems in order to ascertain the actual margin left after the warning had been given before the aircraft stalled. On this particular flight, the aircraft was being operated with its centre of gravity towards its aft limit.
Shortly after 18:30, the pilot reported that the aircraft was in a "superstall". At the time, the aircraft was observed to be configured for landing.
Investigation
The Accidents Investigation Branch opened an inquiry into the accident. The investigation found that accident was the result of the pilot delaying recovery manoeuvres for too long, thereby allowing the aircraft to enter a deep stall from which it was impossible to recover.
References
Sources
- Deep Stall Disaster Flight International, 20 November 1968 p909-910
References
- "Hawker Siddeley Trident Accidents". Shockcone.
- "G-ARPY Accident description". Aviation Safety Network.
- "DH121 Trident". de Havilland.
- "History". Felthorpe Flying Group.
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