No fatalities

1982-06-18: Beechcraft H18 (N74JT) — Western States Express — Fresno, United States of America

Fresno, United States of AmericaTakeoff (climb)

On June 18, 1982, a Beechcraft H18 (registration N74JT) operated by Western States Express was involved in an aviation accident near Fresno, United States of America during takeoff. No fatalities were reported. Investigators recorded the probable cause as: Occurrence #1: loss of control - in flight Phase of operation: takeoff - initial climb Findings 1. (f) aircraft weight and balance - exceeded - pilot in command 2. (c) tie down - not performed - pilot in command 3. 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 1781221417Data APIEditorial standards

An aircraft lost control after liftoff from runway 29R, collided with a fence, and burned. Investigation revealed cargo weight exceeded bulkhead limits and was not tied down.

Summary

Shortly after departing from runway 29R, the aircraft experienced an uncontrolled pitch-up. The pilot applied right aileron and full right rudder, causing the aircraft to roll right and the nose to drop. The pilot recovered before ground impact but the aircraft struck a six-foot wire fence. The fence tore off the engines and induced a clockwise rotation on the ground. Cargo broke through the fuselage side. The pilot exited uninjured. The aircraft then burst into flames and the fuselage sustained severe fire damage.

Investigation Findings

Examination revealed that 2,989 lbs of freight and a 359 lb motorcycle were loaded between bulkheads 5 and 11. The bulkhead load limits were 450 lbs for stations 5-8 and 300 lbs for stations 8-10. The estimated maximum gross weight at takeoff was 10,310 lbs. The pilot reported that none of the freight was secured with tie-downs.

Probable Cause Statement

The official investigation determined two occurrences. In Occurrence #1 (loss of control during initial climb), findings included: aircraft weight and balance exceeded by the pilot-in-command, tie-down not performed by the pilot-in-command, and aircraft handling not possible. In Occurrence #2 (in-flight collision with object during takeoff), the finding was that the object was a fence.