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FTW91LA048

1991-03-07 · HIGH ISLAND, Texas, United States · Fatal · 1 aircraft · Status: Completed

Aircraft involved

Probable cause & findings

FOR OCCURRENCE #1 - INADEQUATE SUPERVISION BY THE OPERATOR IN LAUNCHING A HAZARDOUS MISSION WITHOUT AN ADEQUATE SLING/HARNESS, THE PILOT'S POOR JUDGEMENT IN ACCEPTING AND CONTINUING THE MISSION INTO LOW LIGHT CONDITIONS, AND THE CREWMEMBER'S INADVERTENT RELEASE OF HIS HOLD OF THE NYLON STRAP. FOR OCCURRENCES #2-4 - FAILURE OF THE TAIL ROTOR DRIVE SHAFT AS A RESULT OF ENTANGLEMENT OF AN UNSECURED NYLON STRAP.

Factual narrative

THE MISSION WAS TO LOCATE AND MARK A DOWNED HELICOPTER FLOATING INVERTED OFFSHORE. A CREWMAN WAS LOWERED BY A NYLON STRAP TO ATTACH THE MARKER BOUY. AS DARKNESS SET IN, THE CREWMAN SIGNALED TO COME BACK ABOARD. THE OTHER OBSERVER THREW THE NYLON STRAP TO THE CREWMAN ON THE FLOATING HELICOPTER. THE INBOARD END OF THE STRAP WAS ATTACHED TO A SEAT BELT ANCHOR POINT. DURING THE RETRIEVAL THE CREWMAN RELEASED HIS HOLD ON THE STRAP AND FELL INTO THE WATER. DURING THE SUBSEQUENT SEARCH ACTIVITY THE CREWMAN WAS FOUND DROWNED. THE PILOT SUBSEQUENTLY REPORTED A LOW FUEL STATE TO THE PARTICIPATING U.S.COAST GUARD HELICOPTER AND RETURNED TOWARD GALVESTON. AS HE ARRIVED OVER THE BEACH THE PILOT EXPERIENCED A LOSS OF DIRECTIONAL CONTROL AND AUTOROTATED TO A HARD LANDING. THE NYLON STRAP THAT HAD BEEN LEFT HANGING OUTSIDE THE HELICOPTER HAD BECOME ENTANGLED AROUND THE TAIL ROTOR SHEARING THE DRIVE SHAFT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1991_FTW91LA048.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

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