FTW76AF087

NTSB accident investigation · Bell 205-A1 · Gulf Of Mexico (Gulf of Mexico) · April 23, 1976

Accident · FatalClosed
Date
April 23, 1976
Place
Gulf Of Mexico (Gulf of Mexico) · GULF OF MEXICO, GM
Injuries
12 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N8167JBell 205-A1
Status
Completed · report September 17, 1976
Report
Brief approved by the director
FAA report
19760423027679A
Case key
153627

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
----------------------------------------------------------------------------------------------------------------------------
3-2324  76/4/23    GULF OF MEXICO      BELL 205-A1         CR-  1  0  0  COMMERCIAL                COMMERCIAL, AGE 47, 7206
        TIME - 0808                    N8167J              PX- 11  0  0  AIR TAXI-PASSG            TOTAL HOURS, 229 IN TYPE,
                                       DAMAGE-DESTROYED    OT-  0  0  0                            NOT INSTRUMENT RATED.
        DEPARTURE POINT             INTENDED DESTINATION
          CAMERON,LA                  WEST CAMERON 266
        TYPE OF ACCIDENT                                         PHASE OF OPERATION
           AIRFRAME FAILURE: IN FLIGHT                              IN FLIGHT: NORMAL CRUISE
        PROBABLE CAUSE(S)
           AIRFRAME - FUSELAGE: OTHER
           ROTORCRAFT - MISCELLANEOUS UNITS AND ASSEMBLIES: TAIL BOOMS/PYLONS/CONES
           MISCELLANEOUS ACTS,CONDITIONS - FATIGUE FRACTURE
        FACTOR(S)
           MISCELLANEOUS ACTS,CONDITIONS - SEPARATION IN FLIGHT
           MISCELLANEOUS ACTS,CONDITIONS - AIRCRAFT CAME TO REST IN WATER
        REMARKS- TAIL BOOM/FUSELAGE ATTACH FITTINGS FAILED. PLT & 4 PAX NOT RECOVERED,PRESUMED FATAL.

Aircraft

Registration
N8167J
Reported as
Bell 205-A1
Category
Helicopter
Engine
turbo shaft
Damage
Destroyed

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.