Beirut - Kuwait City

On June 30, 1966 at 11:46 PM, Beirut - Kuwait City experienced a crash involving Hawker Siddeley HS.121 Trident, operated by Kuwait Airways, with the event recorded near Kuwait City All Kuwait.

The flight was categorized as scheduled revenue flight and the reported phase was landing (descent or approach) at a airport (less than 10 km from airport) crash site.

83 people were known to be on board, 0 fatalities were recorded, 83 survivors were identified or estimated. This corresponds to an estimated fatality rate of 0.0%.

Crew on board: 11, crew fatalities: 0, passengers on board: 72, passenger fatalities: 0, other fatalities: 0.

The listed crash cause is human factor. Flight KU32 was a scheduled international flight from Beirut, Lebanon to Kuwait. It departed Beirut at 1855 hours GMT and apart from a tendency for the autopilot pitch lock to disconnect the flight to the descent point was uneventful. The aircraft was cleared to commence descent at 2028 hours GMT from flight level 300 to flight level 95 by the DY NDB - the pilot-in-command decided to carry out a visual approach and advised the co-pilot accordingly. The aircraft reached flight level 95 some three minutes before reaching the DY NDB and it maintained this level until passing the beacon at about 2039 hours GMT at which time it was cleared to descend to 3 000 ft it being agreed the aircraft would report on left base for runway 33R. By visual navigation and ADF indications from the MG NDB the aircraft was positioned on a left hand base leg for runway 33R passing abeam the MG NDB 1 - 2 miles to the south. The rate of descent was 1500 ft/min with the outboard engines at idle and 10 400 rpm on the centre engine. At about this time and when at flight level 50 the flight reported the field in sight - the pilot-in-command and flight engineer having sighted the airport rotating beacon and the co-pilot the rotating beacon and some airport lights - and the aircraft was cleared for final. A left turn on to final was cow menced at about 4 000 ft and the flight reported its position as 6 miles from the airport when at 2 300 ft. Rate of descent was 1 500 ft/min and airspeed was 178 kt. During all these manoeuvres the aircraft was being flown on the autopilot and the co-pilot had been requested to set 1 500 ft in the "acquire height" box of the autopilot. The ADF was tuned to the KWS locator which is 2 224 m from the runway threshold, and the co-pilot was occupied with the landing checks. At this stage of the flight the aircraft was at 1 830 ft almost abeam of the MG NDB inbound and 80 seconds from impact with the ground. Desired approach speed was 154 kt with a descent rate of 700 ft/min and a threshold speed of 134 kt. The aircraft struck the ground and crashed approximately 4 km short of the runway threshold, slightly to the left of the centreline at an elevation of approximately 185 ft. (Latitude 29013'25"N, Longitude 47058'05"E). The accident occurred at approximately 2046 hours GMT at night.

Aircraft reference details include registration 9K-ACG, MSN 2118, year of manufacture 1965.