Casualties unknown

1997-09-19: Piper PA-28R-200 (N4315X) — Cap Flying Club — Miami, FL

Miami, FL, US

On September 19, 1997, a Piper PA-28R-200 (registration N4315X) operated by Cap Flying Club was involved in an aviation accident near Miami, FL. Investigators recorded the probable cause as: The mixture control cable hold down bracket had broken near the engine and a clamp holding the cable to the engine mount was missing the rubber insert, allowing the clamp to slide freely on the engine mount arm. 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

At cruising altitude, the pilot leaned the fuel mixture. The mixture continued to lean and the engine lost power. During a forced landing, insufficient altitude on final approach led to a touchdown on soft terrain with landing gear collapse. Post-crash examination revealed a broken mixture control cable hold down bracket and a missing clamp rubber insert.

Event Narrative

After reaching cruising altitude of 8,500 feet, the pilot adjusted the engine fuel mixture to a lean setting. Several minutes later, the fuel mixture began to lean further without pilot input, and the engine subsequently lost power. Attempts to adjust the mixture using the mixture control handle were ineffective, as the handle had no effect on engine operation.

The flight initiated a descent for a forced landing at a nearby airport. During the turn onto final approach, the aircraft lacked sufficient altitude and airspeed to reach the runway. The landing was made on soft terrain short of the runway, causing the landing gear to collapse.

Post-Crash Examination

Inspection of the engine following the event found that the mixture control cable hold down bracket had broken near the engine. Additionally, a clamp that secured the cable to the engine mount was missing its rubber insert, which allowed the clamp to slide freely on the engine mount arm.

Maintenance Requirements

Manufacturer inspection requirements state that the mixture control cable should be inspected for security every 100 flight hours.

Probable cause

The mixture control cable hold down bracket had broken near the engine and a clamp holding the cable to the engine mount was missing the rubber insert, allowing the clamp to slide freely on the engine mount arm.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X08902. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.