19980626024489A

Accident · Substantial damage

FAA accident report · Tmpson NAVION A · San Andreas, CA · June 26, 1998

Date
June 26, 1998 · 14:30 local
Place
San Andreas, CA
Airport
Calaveras Co-Maury Airport
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N1400Z
NTSB investigation
NTSBLAX98LA212
Reported as
Tmpson Naviona
Reported engine
Continental IO470H
People aboard
1
Fatal injuries
0
Pilot’s flight hours
4,000 total700 in this make and model15 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Worked on fuel selector. On test flight engine quit. Tried return. Impacted nose first. Fuel selector improper. (-23) after performing maintenance on the aircraft fuel system, in particular the fuel selector, the pilot was decided to do a maintenance test flight. Shortly after takeoff from runway 31 @ 003, the aircraft lost power. The pilot tried to return to the runway. The engine regained power momentarily but lost power again. The aircraft struck the ground in a nose down attitude, at approx. a 45 degree heading to runway 13. The aircraft slid across the runway and down a slight embankment, coming to rest about 50 yards off the runway. Investigation found that the fuel selector handle was installed incorrectly after maintnance by the A&P rated owner. (.4) a witness to the accident reported that the airport is located on a plateau and that the surrounding area is not suitable for an off-field landing. The witness reported that he observed the airplane takeoff and as it passed by it looked and sounded normal. He returned to his hangar and heard the engine go to idle. The witness went outside and observed the aircraft losing altitude as it made a 180-degree turn to attempt a return to the runway. The witness reported that the engine caught and sounded as if it was at full power, the airplane regained some altitude, and then the engine stopped. The airplane descended into the ground short of the runway. The pilot stated that he had completed work on the fuel selector handle and had inadvertently reversed the handle when he reinstalled it into the airplane. When he selected the main tank with the fuel selector handle, the fuel valve for the main tank would have been closed and the fuel valve for the aft tank would have been open. The pilot stated that he had refueled the main tank, but the aft tank did not have enough fuel in it to keep the engine running.

As the FAA filed it

WORKED ON FUEL SELECTOR. ON TEST FLIGHT ENGINE QUIT. TRIED RETURN. IMPACTED NOSE FIRST. FUEL SELECTOR IMPROPER. (-23) AFTER PERFORMING MAINTENANCE ON THE AIRCRAFT FUEL SYSTEM, IN PARTICULAR THE FUEL SELECTOR, THE PILOT WAS DECIDED TO DO A MAINTENANCE TEST FLIGHT. SHORTLY AFTER TAKEOFF FROM RUNWAY 31 @ 003, THE AIRCRAFT LOST POWER. THE PILOT TRIED TO RETURN TO THE RUNWAY. THE ENGINE REGAINED POWER MOMENTARILY BUT LOST POWER AGAIN. THE AIRCRAFT STRUCK THE GROUND IN A NOSE DOWN ATTITUDE, AT APPROX. A 45 DEGREE HEADING TO RUNWAY 13. THE AIRCRAFT SLID ACROSS THE RUNWAY AND DOWN A SLIGHT EMBANKMENT, COMING TO REST ABOUT 50 YARDS OFF THE RUNWAY. INVESTIGATION FOUND THAT THE FUEL SELECTOR HANDLE WAS INSTALLED INCORRECTLY AFTER MAINTNANCE BY THE A&P RATED OWNER. (.4) A WITNESS TO THE ACCIDENT REPORTED THAT THE AIRPORT IS LOCATED ON A PLATEAU AND THAT THE SURROUNDING AREA IS NOT SUITABLE FOR AN OFF-FIELD LANDING. THE WITNESS REPORTED THAT HE OBSERVED THE AIRPLANE TAKEOFF AND AS IT PASSED BY IT LOOKED AND SOUNDED NORMAL. HE RETURNED TO HIS HANGAR AND HEARD THE ENGINE GO TO IDLE. THE WITNESS WENT OUTSIDE AND OBSERVED THE AIRCRAFT LOSING ALTITUDE AS IT MADE A 180-DEGREE TURN TO ATTEMPT A RETURN TO THE RUNWAY. THE WITNESS REPORTED THAT THE ENGINE CAUGHT AND SOUNDED AS IF IT WAS AT FULL POWER, THE AIRPLANE REGAINED SOME ALTITUDE, AND THEN THE ENGINE STOPPED. THE AIRPLANE DESCENDED INTO THE GROUND SHORT OF THE RUNWAY. THE PILOT STATED THAT HE HAD COMPLETED WORK ON THE FUEL SELECTOR HANDLE AND HAD INADVERTENTLY REVERSED THE HANDLE WHEN HE REINSTALLED IT INTO THE AIRPLANE. WHEN HE SELECTED THE MAIN TANK WITH THE FUEL SELECTOR HANDLE, THE FUEL VALVE FOR THE MAIN TANK WOULD HAVE BEEN CLOSED AND THE FUEL VALVE FOR THE AFT TANK WOULD HAVE BEEN OPEN. THE PILOT STATED THAT HE HAD REFUELED THE MAIN TANK, BUT THE AFT TANK DID NOT HAVE ENOUGH FUEL IN IT TO KEEP THE ENGINE RUNNING.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.