20070917824329A

Accident · Substantial damage

FAA accident report · Piper PA-30 · Harold, FL · September 17, 2007

Date
September 17, 2007 · 11:50 local
Place
Harold, FL
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N8751Y
NTSB investigation
NTSBMIA07LA152
Reported as
Piper PA30
Reported engine
Lycoming IO320*
People aboard
1
Fatal injuries
0
Pilot’s flight hours
5,000 total2,000 in this make and model10 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.

(-23) The pilot stated that the flight departed with between 60 and 65 gallons of fuel onboard for the estimated 1 hour 20 minute flight. The pilot estimated the fuel consumption for the flight would be between 26 and 28 gallons total. The flight departed with each selector positioned to each main tank position. The pilot climbed to 5,500 feet, where he then repositioned each fuel selector to each auxiliary fuel tank position. The fuel selectors remained on the auxiliary fuel tank position for 22 minutes, when he then moved them back to each main tank position. When the flight was between 3,000 and 4,000 feet, both engines quit at the same time. The pilot turned on each auxiliary fuel boost pump and then moved each fuel selector to the auxiliary fuel tank position which restored engine power. The pilot advised the air traffic controller of the situation who vectored the flight to the location where the pilot performed the precautionary landing. The pilot landed at approximately 90-100 miles-per-hour, bounced, then touched down again. He applied the brakes but they were ineffective, he tried to turn right. The fuselage of the airplane traveled between two fence posts which contacted each wing. The upright.

As the FAA filed it

(-23) THE PILOT STATED THAT THE FLIGHT DEPARTED WITH BETWEEN 60 AND 65 GALLONS OF FUEL ONBOARD FOR THE ESTIMATED 1 HOUR 20 MINUTE FLIGHT. THE PILOT ESTIMATED THE FUEL CONSUMPTION FOR THE FLIGHT WOULD BE BETWEEN 26 AND 28 GALLONS TOTAL. THE FLIGHT DEPARTED WITH EACH SELECTOR POSITIONED TO EACH MAIN TANK POSITION. THE PILOT CLIMBED TO 5,500 FEET, WHERE HE THEN REPOSITIONED EACH FUEL SELECTOR TO EACH AUXILIARY FUEL TANK POSITION. THE FUEL SELECTORS REMAINED ON THE AUXILIARY FUEL TANK POSITION FOR 22 MINUTES, WHEN HE THEN MOVED THEM BACK TO EACH MAIN TANK POSITION. WHEN THE FLIGHT WAS BETWEEN 3,000 AND 4,000 FEET, BOTH ENGINES QUIT AT THE SAME TIME. THE PILOT TURNED ON EACH AUXILIARY FUEL BOOST PUMP AND THEN MOVED EACH FUEL SELECTOR TO THE AUXILIARY FUEL TANK POSITION WHICH RESTORED ENGINE POWER. THE PILOT ADVISED THE AIR TRAFFIC CONTROLLER OF THE SITUATION WHO VECTORED THE FLIGHT TO THE LOCATION WHERE THE PILOT PERFORMED THE PRECAUTIONARY LANDING. THE PILOT LANDED AT APPROXIMATELY 90-100 MILES-PER-HOUR, BOUNCED, THEN TOUCHED DOWN AGAIN. HE APPLIED THE BRAKES BUT THEY WERE INEFFECTIVE, HE TRIED TO TURN RIGHT. THE FUSELAGE OF THE AIRPLANE TRAVELED BETWEEN TWO FENCE POSTS WHICH CONTACTED EACH WING. THE UPRIGHT.

NTSB investigation

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