Skip to content

MIA89LA045

1988-11-28 · CRESTVIEW, Florida, United States · None · 1 aircraft · Status: Completed

Airport CEW

Aircraft involved

Factual narrative

WHILE IN CRUISE FLT NEAR AN ARPT, THE PROP SEPARATED. PLT WAS GIVEN VECTORS TO ARPT & ENTERED PATTERN FOR LNDG. DOWNWIND LEG WAS EXTENDED DUE TO STRONG TAILWIND. STRONG HEADWIND ON FINAL CAUSED ACFT TO LAND SHORT. DURING LANDING ROLL ACFT COLLIDED WITH TWO FENCES. EXAMINATION OF ACFT REVEALED 6 PROP MOUNT BOLTS FAILED DUE TO FATIGUE AS A RESULT OF IMPROPER PLACEMENT OF PROP MOUNTING SHIM BETWEEN ENGINE CRANKSHAFT FLANGE AND STARTER GEAR FLANGE. ACFT MANUAL STATED PROP MOUNT BOLTS MAY FAIL DUE TO RELATIVE MOVEMENT BETWEEN THE TWO FLANGES IF SHIM IS NOT INSTALLED. CORRECT PLACEMENT OF THE SHIM IS BETWEEN THE PROP FLANGE & THE STARTER GEAR FLANGE. SUDDEN ENG STOPPAGE APROX 45 HRS EARLIER RESULTED IN PROP REMOVAL, OVERHAUL, & REINSTALLATION. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1988_MIA89LA045.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Search this event elsewhere

External sources are reported, not agency: signal that something happened, not fact about what happened.

Related research

Matched on aircraft type or causal vocabulary (stall). All research papers