No fatalities

Hard Landing and Post-Crash Fire Destroy Aircraft; Pilots Uninjured (N444LM)

Livermore, United States of AmericaLanding (descent or approach)

On May 3, 1985, a Swearingen SA226T Merlin III (registration N444LM) operated by Landmark Land Company was involved in an aviation accident near Livermore, United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: Improper descent by pilot in command, delayed pull-up, and failure to maintain airspeed, leading to in-flight collision with terrain. Additionally, overload of the main landing gear during landing. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

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

An aircraft landed hard and short of the runway, collapsing the right main landing gear and causing a post-crash fire. Both pilots were uninjured. Investigation found no pre-impact failure.

Introduction

A post-crash fire destroyed an aircraft after it landed hard and short of the runway. The impact collapsed the right main landing gear. Both pilots were uninjured.

Sequence of Events

The pilot reported that on short final, a muffled 'pop' was heard and the aircraft yawed to the right. Directional control was regained, and the aircraft landed hard. The hard landing occurred short of the runway, collapsing the right main landing gear. A fire ensued, destroying the aircraft.

Investigation

A post-accident inspection failed to disclose any pre-impact failure or malfunction of the aircraft or engines. Evidence from right engine propeller slash marks on the runway indicated that the engine was producing power at touchdown.

Probable Cause

The official findings identified two occurrences. Occurrence #1: in-flight collision with terrain/water during the approach phase (VFR pattern final approach). The findings were improper descent by the pilot in command, delayed pull-up, and failure to maintain airspeed. Occurrence #2: main gear collapsed during the landing flare/touchdown phase, caused by overload of the main landing gear.