Jump to content

BKS Air Transport Flight C.6845

Coordinates: 51°28′24″N 0°27′00″W / 51.4734°N 0.4501°W / 51.4734; -0.4501
From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by GalacticOrbits (talk | contribs) at 16:29, 22 June 2023. The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

BKS Air Transport Flight C.6845[1]
Twin-engined, triple-tailed, high-winged propeller-driven passenger aircraft, in profile on an airport taxiway. Natural metal finish except for airline insignia and a lengthwise stripe along the length of the fuselage.
Airspeed Ambassador G-AMAD in 1966
Accident
Date3 July 1968
SummaryMechanical failure caused by metal fatigue
SiteHeathrow Airport, England
51°28′24″N 0°27′00″W / 51.4734°N 0.4501°W / 51.4734; -0.4501
Aircraft
Aircraft typeAirspeed Ambassador
OperatorBKS Air Transport
RegistrationG-AMAD
Occupants8
Passengers5
Crew3
Fatalities6 people and 8 horses
Survivors2

On 3 July 1968, BKS Air Transport Flight C.6845, an Airspeed Ambassador registration G-AMAD of BKS Air Transport crashed at Heathrow Airport, damaging two parked Trident airliners as it cartwheeled into the incomplete Heathrow Terminal 1, then under construction. Six of the eight people on board the Ambassador were killed, along with the eight racehorses being transported on it.[1] The crash was blamed on the failure of a flap-operating rod due to metal fatigue, resulting in asymmetrical lift.

Accident

The Ambassador, construction number 5211,[2] had previously been British European Airways' Sir Francis Drake. It had recently been converted to a "horsebox" transport and was on a flight from Deauville, France, to Heathrow Airport. Flight C.6845 was transporting eight racehorses belonging to businessman William Hill together with five grooms. As the aircraft was landing on Heathrow's runway 28R the left wing dropped, and the wing tip and left landing gear touched the grass adjacent to the runway. The crew tried to increase power to go-around and climb away, but the bank angle increased. The aircraft hit two parked empty British European Airways Hawker Siddeley Tridents, knocking the tail fin off one (G-ARPI) and slicing off the entire tail section of the other (G-ARPT). The Ambassador cartwheeled following the impact and slid upside down coming up against the ground floor of the terminal building where there was an explosion.[3]

G-APKF, one of the aircraft involved in the accident

Six people on board the Ambassador died, including the flight crew and three of five grooms, along with all eight horses. The other two grooms were seriously injured as were two people on the ground. A further 29 people on the ground received slight injuries.

Of the two Trident aircraft, G-ARPT was damaged beyond economic repair and G-ARPI was subsequently repaired. G-ARPI was involved in an accident in 1972 resulting in the deaths of 118 people and becoming the deadliest non-terrorist aviation accident in the UK. A Viscount (G-APKF) received slight damage.[3] The Viscount was also repaired but later too involved in a fatal hull-loss accident in Cambodia as XW-TDN in 1975.[4]

All other Ambassadors were grounded pending the result of an inquiry.[3] The starboard rod from the aircraft was tested and found satisfactory but rods from some other Ambassadors showed signs of cracking and when tested failed in a similar manner to G-AMAD's port rod. The rods on aircraft were strengthened and shown to be capable of 37,000 hours flight time.

Probable cause

The port (left) flap operating rod had failed due to metal fatigue. While the mechanism had failed, the compensating mechanism between the two sets of flaps remained intact. The port flaps had retracted but the compensator caused the starboard ones to extend further. The resulting asymmetry of lift resulted in the roll to port.

The pilot probably tried to overshoot and set the flaps to the correct 10 degrees, but due to the mechanism design this was not sufficient to cause the starboard flaps to retract (which would have taken 25 seconds in any event). The Department of Transport report concluded that whatever the pilot's actions, it was "doubtful" whether an accident could have been avoided.

After the accident all Ambassadors were fitted with steel reinforcements to the flap operating rods.[1]

See also

References

  1. ^ a b c Accident description at the Aviation Safety Network citing Aircraft Illustrated Vol.1, nr. 4 (Oct. 1968), p.127
  2. ^ Denham, Terry (1996). World Directory of Airliner Crashes. Sparkford: Patrick Stephens Ltd. pp. 85, 107. ISBN 1-85260-554-5.
  3. ^ a b c "BKS Crash: Fatigue-failure". Flight International: 42. Archived from the original on 7 August 2018.
  4. ^ "Viscount c/N 396 operational record".

Further reading