DCA80AA002
NTSB Identification: DCA80AA002
14 CFR Part 135 Scheduled operation of COMAIR,INC.
Event occurred Monday, October 08, 1979 in COVINGTON, KY
Aircraft: PIPER PA-31, registration: N6642L

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 FILE    DATE          LOCATION          AIRCRAFT DATA       INJURIES       FLIGHT                        PILOT DATA
                                                               F  S M/N     PURPOSE
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3-0101   79/10/8   COVINGTON,KY        PIPER PA-31         CR-  1  0  0  COMMERCIAL                ATP,FLIGHT INSTR., AGE
        TIME - 1008                    N6642L              PX-  7  0  0  COMMUTER AIR CARRIER      30, 2820 TOTAL HOURS,
                                       DAMAGE-DESTROYED    OT-  0  0  0  AIR TAXI-PASSG S-D        UNK/NR IN TYPE,
                                                                                                   INSTRUMENT RATED.
        NAME OF AIRPORT - GRTR CINCINNATI
        DEPARTURE POINT             INTENDED DESTINATION
          COVINGTON,KY                NASHVILLE,TN
        TYPE OF ACCIDENT                                         PHASE OF OPERATION
           ENGINE FAILURE OR MALFUNCTION                            TAKEOFF: INITIAL CLIMB
           COLLISION WITH GROUND/WATER: UNCONTROLLED                TAKEOFF: INITIAL CLIMB
        PROBABLE CAUSE(S)
           POWERPLANT - MISCELLANEOUS: POWERPLANT FAILURE FOR UNDETERMINED REASONS
           PILOT IN COMMAND - FAILED TO FOLLOW APPROVED PROCEDURES,DIRECTIVES,ETC.
           MISCELLANEOUS ACTS,CONDITIONS - IMPROPER EMERGENCY PROCEDURES
        FACTOR(S)
           PERSONNEL - OPERATIONAL SUPERVISORY PERSONNEL: INADEQUATE FLIGHT TRAINING-PROCEDURES
           PERSONNEL - OPERATIONAL SUPERVISORY PERSONNEL: INADEQUATE GROUND TRAINING-PROCEDURES
           PERSONNEL - OPERATIONAL SUPERVISORY PERSONNEL: DEFICIENCY,COMPANY MAINTAINED EQPMT,SERVICES,REGULATION
           PERSONNEL - RULES,REGULATIONS,STANDARDS PERSONNEL
           MISCELLANEOUS ACTS,CONDITIONS - IMPROPERLY LOADED AIRCRAFT-WEIGHT-AND/OR C.G.
        PARTIAL POWER LOSS - PARTIAL LOSS OF POWER - 1 ENGINE
        REMARKS- GR,FLAPS DOWN.195LBS OVR MAX GWT.HURRIED DEPARTURE.INEFFECTIVE FAA CERTIFICATION,SURVEILLANCE.

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