IAD76FKW17

NTSB accident investigation · Bell 47H1 · Nashville, TN · May 20, 1975

Accident · Serious injuriesClosed
Date
May 20, 1975
Place
Nashville, TN · NASHVILLE, TN
Injuries
2 serious
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N13172Bell 47H1
Status
Completed · report October 28, 1975
Report
Brief approved by the director
FAA report
19750520011259A
Case key
149087

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
----------------------------------------------------------------------------------------------------------------------------
3-2734  75/5/20  NR.NASHVILLE,TN       BELL 47H1           CR-  0  2  0  INSTRUCTIONAL             COMMERCIAL, FL.INSTR.,
        TIME - 1115                    N13172              PX-  0  0  0  DUAL                      AGE 28, 3242 TOTAL HOURS,
                                       DAMAGE-SUBSTANTIAL  OT-  0  0  0                            405 IN TYPE, INSTRUMENT
                                                                                                   RATED.
        NAME OF AIRPORT - CONELIA FORT
        DEPARTURE POINT             INTENDED DESTINATION
         NASHVILLE,TN                 LOCAL
        TYPE OF ACCIDENT                                         PHASE OF OPERATION
           PROPELLER/ROTOR FAILURE: TAIL ROTOR                      LANDING: POWER-ON LANDING
           COLLISION WITH GROUND/WATER: CONTROLLED                  LANDING: POWER-OFF AUTOROTATIVE LANDING
        PROBABLE CAUSE(S)
           ROTORCRAFT - ROTOR ASSEMBLIES: OTHER
           MISCELLANEOUS ACTS,CONDITIONS - FATIGUE FRACTURE
        FACTOR(S)
           MISCELLANEOUS ACTS,CONDITIONS - SEPARATION IN FLIGHT
        EMERGENCY CIRCUMSTANCES - FORCED LANDING ON AIRPORT/SEAPLANE BASE/HELIPT.
                                  DIRECTIONAL CONTROL PROBLEM
        REMARKS- TAIL ROTOR HUB BOLT P/N 47-641-052-3 FAILED.BOLT HAD RETIREMENT LIFE 600 HR FAILED AT 499.8 HR.

Aircraft

Registration
N13172
Reported as
Bell 47H1
Category
Helicopter
Engine
reciprocating
Damage
Substantial damage
Airport
Conelia Fort

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.