20180602006909I

Incident · Minor damage

FAA incident report · Mooney M20C · Perry, OK · June 2, 2018

Date
June 2, 2018 · 08:05 local
Place
Perry, OK
Airport
Perry Municipal
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N6553U
Reported as
Mooney M20C
Reported engine
Lycoming O360-A1D
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
2,000 total150 in this make and model7 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.

The pilot was on a part 91 day VFR pleasure flight. The pilot completed his preflight and run up normally. Prior to the takeoff roll the pilot switch from the left fuel tank to the right fuel tank. The switching of fuel tanks was not a normal procedures for the pilot. Normal the pilot would takeoff on the same fuel tank the engine run up was competed.

The takeoff was normal, after the gear was retracted the engine quit, the pilot lowered the nose and the engine ran again. But the engine quit shortly after and did not restart.

The pilot attempted to lower the landing but there was not significant altitude to lower the landing gear. The aircraft contacted the runway, gear up, slide to a stop 150 feet beyond the end of the runway. Both prop blades were bent back and prop hit marks were found on the runway.

The aircraft was inspected in the grass at the end of 35 and was found to more than half fuel in each tank. The fuel selector was set to the right position and in the detent. With the master switch on, each tanks showed more than half full.

The aircraft owner recovered the aircraft and returned it to his hanger. Further inspection of the aircraft was completed four days after the recovery. The fuel in both fuel tanks were checked, no contaminates were found. The fuel gascolator showed a small air gap in the top. The electric fuel pump was checked and produced 4.5 PSI, within the green arc of the fuel pressure gauge. The carburetor was drained, it was full of fuel and no contaminates were found. The engine was started and ran normally below 1000 RPM.

The loss of engine power could not be determended.

As the FAA filed it

THE PILOT WAS ON A PART 91 DAY VFR PLEASURE FLIGHT. THE PILOT COMPLETED HIS PREFLIGHT AND RUN UP NORMALLY. PRIOR TO THE TAKEOFF ROLL THE PILOT SWITCH FROM THE LEFT FUEL TANK TO THE RIGHT FUEL TANK. THE SWITCHING OF FUEL TANKS WAS NOT A NORMAL PROCEDURES FOR THE PILOT. NORMAL THE PILOT WOULD TAKEOFF ON THE SAME FUEL TANK THE ENGINE RUN UP WAS COMPETED.

THE TAKEOFF WAS NORMAL, AFTER THE GEAR WAS RETRACTED THE ENGINE QUIT, THE PILOT LOWERED THE NOSE AND THE ENGINE RAN AGAIN. BUT THE ENGINE QUIT SHORTLY AFTER AND DID NOT RESTART.

THE PILOT ATTEMPTED TO LOWER THE LANDING BUT THERE WAS NOT SIGNIFICANT ALTITUDE TO LOWER THE LANDING GEAR. THE AIRCRAFT CONTACTED THE RUNWAY, GEAR UP, SLIDE TO A STOP 150 FEET BEYOND THE END OF THE RUNWAY. BOTH PROP BLADES WERE BENT BACK AND PROP HIT MARKS WERE FOUND ON THE RUNWAY.

THE AIRCRAFT WAS INSPECTED IN THE GRASS AT THE END OF 35 AND WAS FOUND TO MORE THAN HALF FUEL IN EACH TANK. THE FUEL SELECTOR WAS SET TO THE RIGHT POSITION AND IN THE DETENT. WITH THE MASTER SWITCH ON, EACH TANKS SHOWED MORE THAN HALF FULL.

THE AIRCRAFT OWNER RECOVERED THE AIRCRAFT AND RETURNED IT TO HIS HANGER. FURTHER INSPECTION OF THE AIRCRAFT WAS COMPLETED FOUR DAYS AFTER THE RECOVERY. THE FUEL IN BOTH FUEL TANKS WERE CHECKED, NO CONTAMINATES WERE FOUND. THE FUEL GASCOLATOR SHOWED A SMALL AIR GAP IN THE TOP. THE ELECTRIC FUEL PUMP WAS CHECKED AND PRODUCED 4.5 PSI, WITHIN THE GREEN ARC OF THE FUEL PRESSURE GAUGE. THE CARBURETOR WAS DRAINED, IT WAS FULL OF FUEL AND NO CONTAMINATES WERE FOUND. THE ENGINE WAS STARTED AND RAN NORMALLY BELOW 1000 RPM.

THE LOSS OF ENGINE POWER COULD NOT BE DETERMENDED.