No fatalities

Engine Failure on Takeoff Leads to Crash and Post-Crash Fire (N65DA)

Lawton-Fort Sill, United States of AmericaTakeoff (climb)

On May 24, 1988, an Embraer EMB-110 Bandeirante (registration N65DA) operated by Atlantic Southeast Airlines - ASA was involved in an aviation accident near Lawton-Fort Sill, United States of America during takeoff. No fatalities were reported. Investigators recorded the probable cause as: Occurrence #1: loss of engine power (total) - mech failure/malf Phase of operation: takeoff - initial climb Findings 1. 1 engine 2. (f) compressor assembly, blade - previous damage 3. (f) compressor assembly, blade - overtemperature 4. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards

Left engine failed during takeoff from runway 35. Aircraft yawed left, climbed briefly, then descended, struck ground, hit fence, and caught fire. Eight occupants injured, two seriously. Aircraft destroyed.

Engine Failure During Takeoff

The number one (left) engine failed during the takeoff from runway 35. The aircraft yawed sharply left and climbed to between 50 and 100 feet above ground level before it began losing altitude. It struck the ground and continued moving forward for several hundred feet until it struck the airport perimeter fence. The aircraft came to rest 1,600 feet west of the runway, on a heading of 290°.

Post-Crash Fire and Damage

A post-crash fire destroyed the cargo area of the aircraft. The aircraft was damaged beyond repair. All eight occupants were injured, two seriously. The captain reportedly made the takeoff.

Examination Findings

Examination of the left engine revealed a compressor turbine blade airfoil separation. Disassembly of the propeller on the left engine indicated that the propeller had autofeathered normally after the engine failed.

Probable Cause

Official findings identified two occurrences: loss of engine power (total) due to mechanical failure/malfunction during takeoff initial climb, followed by in-flight collision with terrain/water during the same phase. Contributing factors included previous damage and overtemperature of the compressor assembly blade leading to separation, improper emergency procedure by the pilot in command, and failure to maintain directional control.