SEA75FYC03

NTSB accident investigation · Hiller Acft UH-12E · Dayton, OR · July 16, 1974

Accident · No injuriesClosed
Date
July 16, 1974
Place
Dayton, OR · DAYTON, OR
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N104HAHiller Acft UH-12E
Status
Completed · report October 15, 1974
Report
Brief approved by the director
FAA report
19740716030029A
Case key
130648

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
----------------------------------------------------------------------------------------------------------------------------
3-2810  74/7/16    DAYTON,OREG         HILLER ACFT UH-12E  CR-  0  0  1  COMMERCIAL                AIRLINE TRANSPORT, AGE
        TIME - 1200                    N104HA              PX-  0  0  0  ASSOC CROP CTL ACTIVITY   27, 3800 TOTAL HOURS, 190
                                       DAMAGE-SUBSTANTIAL  OT-  0  0  0                            IN TYPE, INSTRUMENT
                                                                                                   RATED.
        DEPARTURE POINT             INTENDED DESTINATION
          DAYTON,OREG                 LOCAL
        TYPE OF ACCIDENT                                         PHASE OF OPERATION
           COLLISION WITH GROUND/WATER: UNCONTROLLED                TAKEOFF: INITIAL CLIMB
        PROBABLE CAUSE(S)
           PILOT IN COMMAND - FAILED TO MAINTAIN ADEQUATE ROTOR R.P.M.
        FACTOR(S)
           PERSONNEL - MAINTENANCE,SERVICING,INSPECTION: IMPROPER MAINTENANCE (OWNER PERSONNEL)
           ROTORCRAFT - TRANSMISSION ROTOR DRIVE SYSTEM: CLUTCH ASSEMBLY
        REMARKS- CLUTCH SHOE WORN.HIGH IDLE RPM.M/R DRIVE SHAFT FAILED DUE TO IMPACT.M/R SYS SEPARATED.

Aircraft

Registration
N104HA
Reported as
Hiller Acft UH-12E
Category
Helicopter
Engine
reciprocating
Damage
Substantial damage
Airport
Dayton,Ore

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.