DEN80FA051

NTSB accident investigation · Aerospatle 315B · Dell, MT · July 28, 1980

Accident · FatalClosed
Date
July 28, 1980
Place
Dell, MT · DELL, MT
Injuries
1 fatal
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N67103Aerospatle 315B
Status
Completed · report April 3, 1981
Report
Brief approved by the director
Safety recommendations
Yes
FAA report
19800728032339A
Case key
80137

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
----------------------------------------------------------------------------------------------------------------------------
3-3616  80/7/28    DELL,MT             AEROSPATLE 315B     CR-  1  0  0  COMMERCIAL                COMMERCIAL, AGE 43, 8039
        TIME - 1500                    N67103              PX-  0  0  0  AIR TAXI-CARGO            TOTAL HOURS, 1559 IN
                                       DAMAGE-SUBSTANTIAL  OT-  0  0  0                            TYPE, INSTRUMENT RATED.
        DEPARTURE POINT             INTENDED DESTINATION
          DELL,MT                     LOCAL
        TYPE OF ACCIDENT                                         PHASE OF OPERATION
           PROPELLER/ROTOR FAILURE: TAIL ROTOR                      TAKEOFF: VERTICAL
        PROBABLE CAUSE(S)
           PERSONNEL - MAINTENANCE,SERVICING,INSPECTION: IMPROPER MAINTENANCE (MAINTENANCE PERSONNEL)
           ROTORCRAFT - TRANSMISSION ROTOR DRIVE SYSTEM: TAIL ROTOR DRIVE SHAFT ASSEMBLY
           MISCELLANEOUS ACTS,CONDITIONS - IMPROPERLY SECURED
           MISCELLANEOUS ACTS,CONDITIONS - UNDER TORQUED
           MISCELLANEOUS ACTS,CONDITIONS - LOOSE,PART/FITTING
        FACTOR(S)
           MISCELLANEOUS ACTS,CONDITIONS - JETTISONED LOAD
         FIRE AFTER IMPACT
        REMARKS- FAILURE OF THE SPLINES ON THE BEVEL GEAR & VERTICAL SHAFT OF THE BEVEL GEAR ASSEMBLY.

Aircraft

Registration
N67103
Reported as
Aerospatle 315B
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.

Other investigations on N67103 · 1

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