TEHACHAPI, CA, USA
N95907
TAYLORCRAFT BC-12D
THE PILOT WAS A TOW PLANE PILOT FOR SAILPLANES. ACCORDING TO HIS LOG BOOK, HE HAD PERFORMED 14 TOWS DURING THE DAY OF THE ACCIDENT. DURING THE DAY HE HAD BORROWED SOME FUEL CONTAINERS TO PURCHASE AUTOMOBILE FUEL. HE THEN PLANNED TO DEPART IN THE EARLY EVENING FOR A CROSS-COUNTRY FLIGHT OF ABOUT 2 HRS. THE AIRPLANE DID NOT HAVE AN ELECTRICAL SYSTEM OR LIGHTS. DURING THE INITIAL CLIMB, THE ENGINE QUIT. WITNESSES OBSERVED THE AIRPLANE START TO TURN BACK TOWARD THE RUNWAY, AT WHICH TIME THE NOSE DROPPED AND THE AIRPLANE IMPACTED THE GROUND IN ABOUT AN 80 DEG NOSE-DOWN ATTITUDE. WRECKAGE EXAMINATION REVEALED THAT ALL 3 FUEL SELECTOR VALVES WERE IN THE OFF POSITION. THE AIRPLANE WAS ABOUT 29 LBS OVER MAX GROSS WEIGHT, AND THE AFT CENTER OF GRAVITY LIMIT WAS EXCEEDED BY ABOUT 0.5 INCHES. WITNESSES STATED THAT THE PILOT DID NOT PERFORM A RUNUP OR MAGNETO CHECK PRIOR TO TAKEOFF, AND THE ENGINE SOUNDED AS THOUGH IT WAS NOT DEVELOPING POWER.
On August 3, 1993, about 1730 hours Pacific daylight time, a Taylorcraft BC-12-D, N95907, collided with terrain while attempting a return to runway maneuver at the Mountain Valley Airport, Tehachapi, California. The return to runway attempt was precipitated by a total loss of engine power during the takeoff initial climb. Visual meteorological conditions prevailed for the operation and a VFR flight plan was filed. The airplane was destroyed in the ground collision sequence and the commercial pilot, the sole occupant, sustained fatal injuries. The flight was originating at the time of the mishap as a personal cross country flight to Thermal, California. The pilot was working as a tow plane pilot for sailplanes. According to his log book, he performed 14 tows during the day of the accident. During the day, the pilot borrowed some fuel containers to purchase automobile fuel for the Taylorcraft. The airport manager reported during the initial accident notification that the aircraft experienced a loss of engine power during the takeoff and initial climb. The manager stated that the aircraft was attempting a return to runway maneuver when it apparently stalled in the turn and descended nose first to ground impact. An FAA airworthiness inspector from the Van Nuys Flight Standards District Office responded to the accident site and examined the aircraft. He reported that he found the fuel selector valves in the "OFF" position. The FAA inspector performed a weight and balance on the airplane and its contents at the time of the accident. According to the calculations, the airplanes weight at takeoff was 1,229 pounds with a most rearward center of gravity of 20.5 inches. According to the FAA Type Certificate Data, the maximum gross weight is 1,200 pounds with an aft center of gravity limit of 20.0 inches. Further examination, according to the inspector, revealed that the pilot was using automobile gasoline and had borrowed gasoline containers earlier in the day to purchase gasoline at a local automobile station for the airplane. The airplane did not have a Supplemental Type Certificate for the use of automobile fuel and the carburetor did not have the manufacturers recommended needle valve to be compatible with automobile gasoline.
FUEL STARVATION DUE TO THE PILOT'S FAILURE TO CORRECTLY POSITION THE FUEL SELECTOR PRIOR TO DEPARTURE, AND HIS FAILURE TO MAINTAIN AN ADEQUATE AIRSPEED MARGIN ABOVE STALL WHILE ATTEMPTING TO RETURN TO THE RUNWAY. FACTORS IN THE ACCIDENT WERE: THE PILOT'S FAILURE TO PERFORM A PREFLIGHT CHECK OR USE A PRETAKEOFF CHECKLIST, HIS FAILURE TO PROPERLY LOAD THE AIRCRAFT WITHIN THE ALLOWABLE WEIGHT AND CENTER OF GRAVITY LIMITS, AND PRESSURE TO COMPLETE THE FLIGHT PRIOR TO DARKNESS.
Source: NTSB Aviation Accident Database
Aviation Accidents App
In-Depth Access to Aviation Accident Reports
