ASN Wikibase Occurrence # 334592
| Date: | Thursday 15 November 1956 |
| Time: | |
| Type: |  Martin 4-0-4 |
| Owner/operator: | Trans World Airlines - TWA |
| Registration: | N40404 |
| MSN: | 14104 |
| Fatalities: | Fatalities: 0 / Occupants: 38 |
| Aircraft damage: | Destroyed, written off |
| Category: | Accident |
| Location: | Las Vegas-McCarran International Airport, NV (LAS) -
 United States of America
|
| Phase: | Landing |
| Nature: | Passenger - Scheduled |
| Departure airport: | Las Vegas-McCarran International Airport, NV (LAS/KLAS) |
| Los Angeles International Airport, CA (LAX/KLAX) | |
| Investigating agency: | CAB |
| Confidence Rating: |  Accident investigation report completed and information captured |
The aircraft was on its last leg of a flight to Los Angeles when it taxied to runway 07 at 14:49 PST. The Martin 4-0-4 took off at 14:56 and made a climbing left turn, heading for Los Angeles. A few minutes later the no. 2 engine lost power and backfired, forcing the crew to feather the prop. They elected to return to Las Vegas, which was radioed to air traffic control at 15:01. The aircraft flew a wide base leg before turning to runway 07. Airspeed was excessive as the aircraft crossed the threshold (115-120 knots, were 95-100 knots should have been normal). The Martin floated for 2749 feet before touching down and bouncing a few times. Airspeed during the last bounce was 100-105 knots and the pilot-in-command ordered full power and 12deg flaps for a go-around. The aircraft climbed, veered to the left and struck the ground left wing-low, sliding for 225 feet before coming to rest.
It appeared that the no. 2 engine failed because of the failure of the no. 2 cylinder exhaust push rod. This caused the exhaust valve to remain closed, trapping exhaust gases under pressure. When the intake valve was opened these gases entered the induction system of the engine, causing loss of power and backfiring.
PROBABLE CAUSE: "During an emergency situation the captain failed to reduce speed during the latter portion of a single-engine approach; this excessive speed resulted in an overshoot and an attempted go-around which was beyond the performance capability of the aircraft under existing conditions."
Accident investigation:
 |
|
Sources:
ICAO Accident Digest No.8, Circular 54-AN/49 (148-151)
Location
Revision history:
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