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Estado:Final
Fecha:viernes 3 junio 1966
Hora:ca 18:35
Tipo:Silhouette image of generic TRID model; specific model in this crash may look slightly different
Hawker Siddeley HS-121 Trident 1C
Operador:Hawker Siddeley Aviation
Registración: G-ARPY
Numéro de série: 2126
Año de Construcción: 1966-06-03 ()
Horas Totales de la Célula:1
Ciclos:0
Motores: 3 Rolls-Royce Spey 505-5
Tripulación:Fatalidades: 4 / Ocupantes: 4
Pasajeros:Fatalidades: 0 / Ocupantes: 0
Total:Fatalidades: 4 / Ocupantes: 4
Daños en la Aeronave: Destruido
Consecuencias: Written off (damaged beyond repair)
Ubicación:1,6 km (1 milles) SSW of Felthorpe (   Reino Unido)
Fase: Maniobras (MNV)
Naturaleza:Prueba
Aeropuerto de Salida:Hatfield Airport (HTF/EGTH), Reino Unido
Aeropuerto de Llegada:Hatfield Airport (HTF/EGTH), Reino Unido
Descripción:
HS-121 Trident G-ARPY departed Hatfield at 16:52 to carry out the first of a series of production test flights to qualify for a Series Certificate of Airworthiness. At 18:30, after completing a large part of the tests, the stalling tests were begun. Three approaches to stall were made to check the stall warning and stall recovery systems. The fourth stalling run was made at a height of 11600 ft in landing configuration with the stall warning and recovery systems made inoperative. The Trident entered a superstall with the nose pitched up to 30-40 degrees. The plane turned to the left, the right wing dropped and the plane then went into a flat spin to the right.

Probable Cause:

PROBABLE CAUSE: "During a stalling test decisive recovery action was delayed too long to prevent the aircraft from entering a superstall from which recovery was not possible."

Fuentes:
» ICAO Circular 88-AN/74 Volume II (86-107)


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This information is not presented as the Flight Safety Foundation or the Aviation Safety Network’s opinion as to the cause of the accident. It is preliminary and is based on the facts as they are known at this time.
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