Casualties unknown

Parachute Flight Accident: Center of Gravity and Trim Issues Cited (N116CA)

Silvana, WA, US

On August 22, 1983, a Lockheed LEARSTAR, L-18-56 (registration N116CA) operated by Landry Aviation, Inc. was involved in an aviation accident near Silvana, WA. Investigators recorded the probable cause as: The aircraft's center of gravity was behind the aft limit for takeoff and the jump, and the elevator trim actuator was found in the full nose-up trim position. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

A sport parachute flight carrying 24 parachutists for a mass jump ended with the aircraft crashing in a near-vertical descent after entering a steep bank and spiral. Investigation revealed center of gravity was aft of limits and elevator trim was full nose-up.

Incident Overview

A sport parachute flight operating in a cargo configuration carried 24 parachutists to an altitude of 12,500 feet over a designated drop zone for a mass jump. The aircraft had no passenger seats except for one jump seat, and 24 seat belts were attached to the floor of the cargo area. The cabin door had been removed, and an unapproved step along with four handholds were installed outside and forward of the cabin door for the use of parachutists.

Jump Run Procedure

The usual jump-run procedure involved slowing the aircraft to 95 to 100 knots, extending the landing gear and approach flaps, and reducing power on the left engine. Parachutists remained in position without using seat belts until approaching the drop zone. At that point, two jumpers moved outside the aircraft while others moved close to the doorway.

Accident Sequence

The first jumpers were unaware of any problem but subsequently observed the aircraft enter a steep bank, roll over, and spiral nose-down. Sixteen jumpers exited the aircraft, but three of them struck the stabilizer during their exit. The aircraft crashed in a near-vertical descent.

Investigation Findings

Investigation revealed that the aircraft's center of gravity was behind the aft limit for both takeoff and the jump. Additionally, the elevator trim actuator was found in a position corresponding to full nose-up trim.

Conclusion

These findings were documented as part of the official investigation into the accident.

Probable cause

The aircraft's center of gravity was behind the aft limit for takeoff and the jump, and the elevator trim actuator was found in the full nose-up trim position.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001214X44100. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.