FLIGHT FINDINGSAVIATION OCCURRENCE MAP
Back to map

ANC93IA176 · Sikorsky C54A

12 Sept 1993 · ANITA BAY, AK, United States

Chet Rasberry Sikorsky C54A · Incident: total loss of engine power (mechanical failure) while maneuvering

Report a problem

Event

NTSB case
ANC93IA176
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Incident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
0 · all aircraft and ground
Ground fatalities
0
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Sikorsky C54A

Aircraft type
Sikorsky C54
Category
Helicopter
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N44094
Onboard fatalities
Unknown
Route
From not recordedTo not recorded
Aircraft age
Not recorded
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 133: Rotorcraft Ext. Load
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Maneuvering · hover
First occurrenceThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Total loss of engine power (mechanical failure)
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Minor

Cause areas

  • Turbine assembly, turbine blade › Separation

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

THE HELICOPTER EXPERIENCED A #2 ENGINE FAILURE DURING A HOVER FOR LANDING WITH AN EXTERNAL LOAD. EXAMINATION OF THE ENGINE SHOWED THAT THE POWER TURBINE DISC REMAINED INTACT. HOWEVER, ALL THE TURBINE BLADES WERE BENT, BROKEN, OR MISSING THE ENGINE CASE WAS SEVERED IN TWO PARTS IMMEDIATELY ADJACENT TO THE PLANE OF ROTATION OF THE POWER TURBINE. THE MANUFACTURER'S TBO WAS 1800 HRS. THE COMPANY HAD A MILITARY TBO EXTENSION, APPROVED BY THE FAA, TO 2100 HRS. THE ENGINE HAD A TOTAL TIME OF 2058 HRS AT THE TIME OF THE FAILURE.

Probable cause

THE SEPARATION OF THE TURBINE BLADE FROM THE POWER TURBINE DISC.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ANC93IA176
Event ID
20001211X13282
Case number
ANC93IA176
Dataset
historical-pre2008
Source SHA-256
89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: 8ff0d37afed16b743066218f4c528d5760c2b1b517a0cba641d6827e4d477b6a; retrieved 2026-09-23T01:38:22.120Z.