FTW82DA028

NTSB accident investigation · Bell 206B · Gulf Of Mexico (Atlantic Ocean) · December 3, 1981

Accident · No injuriesClosed
Date
December 3, 1981
Place
Gulf Of Mexico (Atlantic Ocean) · GULF OF MEXICO, AO
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N5006YBell 206B
Status
Completed · report June 19, 1982
Report
Brief approved by the director
FAA report
19811203080769A
Case key
122660

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
----------------------------------------------------------------------------------------------------------------------------
3-3633   81/12/3   GULF OF MEXICO      BELL 206B           CR-  0  0  1  COMMERCIAL                AIRLINE TRANSPORT, AGE
        TIME - 1430                    N5006Y              PX-  0  0  1  AIR TAXI-PASSG            34, 6056 TOTAL HOURS, 131
                                       DAMAGE-SUBSTANTIAL  OT-  0  0  0                            IN TYPE, INSTRUMENT
                                                                                                   RATED.
        NAME OF AIRPORT - VERMILLION 245A
        DEPARTURE POINT             INTENDED DESTINATION
          GULF OF MEXICO              LOCAL
        TYPE OF ACCIDENT                                         PHASE OF OPERATION
           ENGINE FAILURE OR MALFUNCTION                            TAKEOFF: VERTICAL
           HARD LANDING                                             TAKEOFF: ABORTED
        PROBABLE CAUSE(S)
           POWERPLANT - COMPRESSOR ASSEMBLY: DISC, COMPRESSOR ROTOR
           MISCELLANEOUS ACTS,CONDITIONS - FATIGUE FRACTURE
           MISCELLANEOUS - EVASIVE MANEUVER TO AVOID COLLISION
        FACTOR(S)
           MISCELLANEOUS ACTS,CONDITIONS - AIRCRAFT CAME TO REST IN WATER
        COMPLETE POWER LOSS - COMPLETE ENGINE FAILURE/FLAMEOUT-1 ENGINE
        EMERGENCY CIRCUMSTANCES - FORCED LANDING OFF AIRPORT ON WATER
        REMARKS- 6TH STAGE COMP WHL,P/N 6871296 S/N BU10118,FATIGUED. PLT HAD TO EXTEND GLIDE OVER OBST ON RIG.

Aircraft

Registration
N5006Y
Reported as
Bell 206B
Category
Helicopter
Engine
turbo shaft
Damage
Substantial damage
Airport
Vermillion 245a

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 N5006Y · 1

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