MIA77FA080

NTSB accident investigation · Beech 65-80 · Vancleave, MS · August 13, 1977

Accident · FatalClosed
Date
August 13, 1977
Place
Vancleave, MS · VANCLEAVE, MS
Injuries
3 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N6DGBeech 65-80
Status
Completed · report March 15, 1978
Report
Brief approved by the director
FAA report
19770813039319A
Case key
145507

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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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
----------------------------------------------------------------------------------------------------------------------------
3-4189  77/8/13  NR.VANCLEAVE,MS       BEECH 65-80         CR-  2  0  0  NONCOMMERCIAL             COMMERCIAL, AGE 69, 18417
        TIME - 1046                    N6DG                PX-  1  0  0  PLEASURE/PERSONAL TRANSP  TOTAL HOURS, 35 IN TYPE,
                                       DAMAGE-DESTROYED    OT-  0  0  0                            NOT INSTRUMENT RATED.
        DEPARTURE POINT             INTENDED DESTINATION
          GULFPORT,MS                 MOBIL,AL
        TYPE OF ACCIDENT                                         PHASE OF OPERATION
           ENGINE FAILURE OR MALFUNCTION                            IN FLIGHT: NORMAL CRUISE
           FIRE OR EXPLOSION: IN FLIGHT                             IN FLIGHT: NORMAL CRUISE
        PROBABLE CAUSE(S)
           POWERPLANT - ENGINE STRUCTURE: CRANKSHAFT
           MISCELLANEOUS ACTS,CONDITIONS - FATIGUE FRACTURE
           MISCELLANEOUS ACTS,CONDITIONS - FIRE IN ENGINE
           POWERPLANT - LUBRICATING SYSTEM: TUBING
           MISCELLANEOUS ACTS,CONDITIONS - LEAK/LEAKAGE
           MISCELLANEOUS ACTS,CONDITIONS - FIRE IN BRAKES,WHEEL ASSEMBLY,WHEEL WELL
        FACTOR(S)
           MISCELLANEOUS ACTS,CONDITIONS - SEPARATION IN FLIGHT
        COMPLETE POWER LOSS - COMPLETE ENGINE FAILURE/FLAMEOUT-1 ENGINE
         FIRE AFTER IMPACT
        REMARKS- CRANKSHAFT S/N 21772 FAILED DUE FATIGUE CRACK AT #5 CONNECTING ROD THROW.

Aircraft

Registration
N6DG
Reported as
Beech 65-80
Category
Airplane
Engine
reciprocating
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.