No fatalities

1950-11-22: De Havilland DH.104 Dove (XY-ABR) — Union of Burma Airways — Yangon, Myanmar

Yangon, MyanmarTakeoff (climb)

On November 22, 1950, a De Havilland DH.104 Dove (registration XY-ABR) operated by Union of Burma Airways was involved in an aviation accident near Yangon, Myanmar during takeoff. No fatalities were reported. Investigators recorded the probable cause as: The accident was caused by the combination of the following factors: - The aircraft was pulled off after too short a take-off run at a low speed. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781257281Data APIEditorial standards

During takeoff, the undercarriage was retracted early causing the aircraft to sink back onto the runway. It slid, caught fire, but all occupants evacuated safely. No flap was used despite pilot notes recommending 20 degrees.

Sequence of Events

The aircraft commenced a normal takeoff. After becoming airborne, the pilot selected "wheels up." Because the undercarriage selector knob was sticking, the radio operator was asked to operate the undercarriage safety switch. The undercarriage retracted normally, but immediately after retraction, the aircraft sank and struck the runway. The pilot shut off power, and the aircraft slid at high speed for a considerable distance down the runway. A fire erupted, and the aircraft was almost completely destroyed. However, all passengers and crew evacuated safely before the aircraft was consumed by fire.

Pilot's Actions

The pilot-in-command stated in evidence that he had no knowledge of the airspeed at the time of undercarriage retraction but was satisfied that he had achieved safety speed. Despite the pilot's notes recommending 20 degrees of flap for takeoff, no flap was used. The pilot explained that he believed 20 degrees of flap would make the aircraft more difficult to handle on one engine in the event of an engine failure after takeoff. Evidence indicated that handling the undercarriage lever, which can be awkward to operate in Dove aircraft, may distract the pilot from flying.

Official Findings

The accident was attributed to a combination of factors. The aircraft was pulled off the runway after too short a takeoff run at low speed. The undercarriage was retracted too early, before safety speed was reached and while at very low altitude. The aircraft then sank back onto the runway before reaching safety speed. This may have been due to a thermal disturbance or distraction from the difficulty in retracting the undercarriage. The fire, which originated to the rear of the starboard engine nacelle, was possibly caused by fractured petrol pipes and electrical circuits. The pilot did not operate the engine nacelle fire extinguishers, which might have prevented the fire. The inertia switch for the static fire extinguishers did not operate due to slow acceleration. The airport fire tender arrived late because it took an unserviceable taxi track, and its crew's inexperience prevented optimal use of the foam. The fire eventually burnt itself out, resulting in near-total destruction of the aircraft.

Probable cause

The accident was caused by the combination of the following factors: - The aircraft was pulled off after too short a take-off run at a low speed. - The undercarriage was retracted too early and before safety speed was reached, whilst still at a very low altitude. - The aircraft sank back on to the runway before the safety speed was reached. This may be due to either a thermal disturbance or to the fact that the pilot's attention was distracted by difficulty in retracting the undercarriage. - The aircraft caught fire to the rear of the starboard engine nacelle while still sliding down the PSP runway, due possibly to the fracture of petrol pipes and electrical circuits. - The pilot failed to operate the fire extinguishers in the engine nacelles which might have prevented the outbreak of fire. (The inertia switch of the static fire extinguishers in the engine bays were not operating due to the relatively slow acceleration.) - The airport fire tender delivered its full complement of 2,500 gallons of foam, but was late in arrival as a result of taking the unserviceable taxi track, and the equipment on it was not applied to the best advantage due to the inexperience of the crew. - The fire burnt itself out and the aircraft was almost totally destroyed.