ANC70A0003

NTSB accident investigation · Hiller Acft UH12E · Bettles, AK · July 9, 1969

Accident · No injuriesClosed
Date
July 9, 1969
Place
Bettles, AK · BETTLES, AK
Injuries
3 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N5362VHiller Acft UH12E
Status
Completed · report April 6, 1970
Report
Brief approved by the director
Case key
162670

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
----------------------------------------------------------------------------------------------------------------------------
3-3527   69/7/9  NR.BETTLES,ALAS       HILLER ACFT UH12E   CR-  0  0  1  COMMERCIAL                COMMERCIAL, AGE 36, 4212
        TIME - 0845                    N5362V              PX-  0  0  2  AIR TAXI-PASSG            TOTAL HOURS, 470 IN TYPE,
                                       DAMAGE-SUBSTANTIAL  OT-  0  0  0                            NOT INSTRUMENT RATED.
        DEPARTURE POINT             INTENDED DESTINATION
          ERNIE LAKE,ALAS             SIXTY MILE CK,ALAS
        TYPE OF ACCIDENT                                         PHASE OF OPERATION
           ENGINE FAILURE OR MALFUNCTION                            IN FLIGHT: NORMAL CRUISE
           HARD LANDING                                             LANDING: POWER-OFF AUTOROTATIVE LANDING
        PROBABLE CAUSE(S)
           POWERPLANT - ENGINE STRUCTURE: MASTER AND CONNECTING RODS
           MISCELLANEOUS ACTS,CONDITIONS - FATIGUE FRACTURE
           PILOT IN COMMAND - FAILED TO MAINTAIN ADEQUATE ROTOR R.P.M.
        COMPLETE POWER LOSS - COMPLETE ENGINE FAILURE/FLAMEOUT-1 ENGINE
        EMERGENCY CIRCUMSTANCES - FORCED LANDING OFF AIRPORT ON LAND
        REMARKS- NR 5 CYL CON ROD CAP AND BOLTS FAILED.

Aircraft

Registration
N5362V
Reported as
Hiller Acft UH12E
Category
Helicopter
Engine
reciprocating
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.