ANC81FA098

NTSB accident investigation · Bell 212 · Kenai, AK · August 23, 1981

Accident · Serious injuriesClosed
Date
August 23, 1981
Place
Kenai, AK · KENAI, AK
Injuries
1 serious
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N392EHBell 212
Status
Completed · report June 25, 1982
Report
Brief approved by the director
FAA report
19810823051089A
Case key
123661

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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NTSB brief

NTSB’s brief of the accident, as it was printed: the coded facts, with the probable cause and factors.

----------------------------------------------------------------------------------------------------------------------------
 FILE    DATE          LOCATION          AIRCRAFT DATA       INJURIES       FLIGHT                        PILOT DATA
                                                               F  S M/N     PURPOSE
----------------------------------------------------------------------------------------------------------------------------
3-3655  81/8/23  NR.KENAI,AK           BELL 212            CR-  0  1  0  COMMERCIAL                COMMERCIAL, AGE 37, 9500
        TIME - 2304                    N392EH              PX-  0  0  0  CTR PASSG-D               TOTAL HOURS, 1150 IN
                                       DAMAGE-SUBSTANTIAL  OT-  0  0  0                            TYPE, INSTRUMENT RATED.
        DEPARTURE POINT             INTENDED DESTINATION         LAST ENROUTE STOP
          KENAI,AK                    RETURN                       OIL PLATFORM
        TYPE OF ACCIDENT                                         PHASE OF OPERATION
           ENGINE FAILURE OR MALFUNCTION                            IN FLIGHT: DESCENDING
           DITCHING                                                 LANDING: POWER-OFF AUTOROTATIVE LANDING
        PROBABLE CAUSE(S)
           POWERPLANT - FUEL SYSTEM: PUMP,FUEL
           MISCELLANEOUS ACTS,CONDITIONS - EXCESSIVE-WEAR/PLAY
           PILOT IN COMMAND - FAILED TO FOLLOW APPROVED PROCEDURES,DIRECTIVES,ETC.
           PILOT IN COMMAND - DELAYED IN INITIATING GO-AROUND
           PILOT IN COMMAND - FAILED TO MAINTAIN ADEQUATE ROTOR R.P.M.
        FACTOR(S)
           MISCELLANEOUS ACTS,CONDITIONS - AIRCRAFT CAME TO REST IN WATER
        COMPLETE POWER LOSS - COMPLETE ENGINE FAILURE/FLAMEOUT-1 ENGINE
        EMERGENCY CIRCUMSTANCES - FORCED LANDING OFF AIRPORT ON WATER
        REMARKS- SPLINES OF NO 1 ENG FUEL PUMP DRIVE SHAFT,PN 02-14910-01, WORN.FLOATS POPPED OUT FM IMPACT.CO PLN.

Aircraft

Registration
N392EH
Reported as
Bell 212
Category
Helicopter
Engine
turbo shaft
Damage
Substantial damage

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.