SEA70DWA06

NTSB accident investigation · Hiller Acft FH1100 · Beaverton, OR · March 9, 1970

Accident · No injuriesClosed
Date
March 9, 1970
Place
Beaverton, OR · BEAVERTON, OR
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N750FHHiller Acft FH1100
Status
Completed · report August 25, 1970
Report
Brief approved by the director
Case key
135493

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
----------------------------------------------------------------------------------------------------------------------------
3-0769   70/3/9    BEAVERTON,OREG      HILLER ACFT FH1100  CR-  0  0  1  NONCOMMERCIAL             PRIVATE, AGE 54, 592
        TIME - 1730                    N750FH              PX-  0  0  0  PLEASURE/PERSONAL TRANSP  TOTAL HOURS, 99 IN TYPE,
                                       DAMAGE-SUBSTANTIAL  OT-  0  0  0                            NOT INSTRUMENT RATED.
        DEPARTURE POINT             INTENDED DESTINATION
          BEAVERTON,OREG              BEAVERTON,OREG
        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 - COMPRESSOR ASSEMBLY: OTHER
           MISCELLANEOUS ACTS,CONDITIONS - MATERIAL FAILURE
           PILOT IN COMMAND - IMPROPER OPERATION OF FLIGHT CONTROLS
        COMPLETE POWER LOSS - COMPLETE ENGINE FAILURE/FLAMEOUT-1 ENGINE
        REMARKS- PLASTIC COATING ON 5TH STAGE COMPRESSOR SECTION BROKE LOOSE FAILED 6TH STAGE BLADES AND STATORS.

Aircraft

Registration
N750FH
Reported as
Hiller Acft FH1100
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.