ANC79FA002

NTSB accident investigation · Bell 205A-1 · Kenai, AK · October 8, 1978

Accident · FatalClosed
Date
October 8, 1978
Place
Kenai, AK · KENAI, AK
Injuries
2 fatal, 4 serious
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N2215WBell 205A-1
Status
Completed · report August 6, 1979
Report
Brief approved by the director
FAA report
19781008043849A
Case key
138121

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

On this page

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
----------------------------------------------------------------------------------------------------------------------------
3-4422   78/10/8 NR.KENAI,AK           BELL 205A-1         CR-  0  1  0  COMMERCIAL                AIRLINE TRANSPORT, AGE
        TIME - 0925                    N2215W              PX-  2  3  0  AIR TAXI-PASSG            34, 7358 TOTAL HOURS,
                                       DAMAGE-DESTROYED    OT-  0  0  0                            3990 IN TYPE, NOT
                                                                                                   INSTRUMENT RATED.
        NAME OF AIRPORT - GRAYLING PLATFORM
        DEPARTURE POINT             INTENDED DESTINATION         LAST ENROUTE STOP
          KENAI,AK                    RETURN                       OIL PLATFORMS
        TYPE OF ACCIDENT                                         PHASE OF OPERATION
           PROPELLER/ROTOR FAILURE: TAIL ROTOR                      IN FLIGHT: NORMAL CRUISE
           HARD LANDING                                             IN FLIGHT: POWER-ON DESCENT
        PROBABLE CAUSE(S)
           ROTORCRAFT - FLIGHT CONTROL SYSTEMS: TAIL ROTOR PITCH CONTROL SYSTEM
           MISCELLANEOUS ACTS,CONDITIONS - MATERIAL FAILURE
        FACTOR(S)
           MISCELLANEOUS ACTS,CONDITIONS - AIRCRAFT CAME TO REST IN WATER
        EMERGENCY CIRCUMSTANCES - FORCED LANDING OFF AIRPORT ON WATER
        REMARKS- FLOAT EQUIPPED.TAIL ROTOR PITCH CONTROL CHANGE CHAIN HAD 21.5 HOURS SINCE INSTALLATION.

Aircraft

Registration
N2215W
Reported as
Bell 205A-1
Category
Helicopter
Engine
turbo shaft
Damage
Destroyed
Airport
Grayling Platform

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.

Other investigations on N2215W · 1

Matched to the same aircraft by N-number and date.