20031121035889I

Incident

FAA incident report · Piper PA-28-140 · Niagara Falls, NY · November 21, 2003

Date
November 21, 2003 · 15:35 local
Place
Niagara Falls, NY
Phase of flight
Normal Cruise
Operating rules
General operating rules (Part 91)
Aircraft
N6910W
Reported as
Piper PA28140
Reported engine
Lycoming O320*
People aboard
2
Fatal injuries
0

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) On November 21, 2003 at 1535 EST a Piper PA-28-140, N6910W during cruise flight lost engine power. The pilot tried to reach the Niagara Falls international airport but as he got closer, decided he could not make it. He chose a vacant parking lot across the street from the airport and landed the aircraft without further incident or damage to the aircraft. The inspector on scene checked the fuel quantity and the tanks were half full and no other visible discrepancies were noted. The aircraft was towed across the street to the airport and secured in its hangar. (-23 amendment) after a more complete inspection of the engine, it was determined that the #3 cylinder exhaust valve broke apart and that caused the power loss.

As the FAA filed it

(-23) ON NOVEMBER 21, 2003 AT 1535 EST A PIPER PA-28-140, N6910W DURING CRUISE FLIGHT LOST ENGINE POWER. THE PILOT TRIED TO REACH THE NIAGARA FALLS INTERNATIONAL AIRPORT BUT AS HE GOT CLOSER, DECIDED HE COULD NOT MAKE IT. HE CHOSE A VACANT PARKING LOT ACROSS THE STREET FROM THE AIRPORT AND LANDED THE AIRCRAFT WITHOUT FURTHER INCIDENT OR DAMAGE TO THE AIRCRAFT. THE INSPECTOR ON SCENE CHECKED THE FUEL QUANTITY AND THE TANKS WERE HALF FULL AND NO OTHER VISIBLE DISCREPANCIES WERE NOTED. THE AIRCRAFT WAS TOWED ACROSS THE STREET TO THE AIRPORT AND SECURED IN ITS HANGAR. (-23 AMENDMENT) AFTER A MORE COMPLETE INSPECTION OF THE ENGINE, IT WAS DETERMINED THAT THE #3 CYLINDER EXHAUST VALVE BROKE APART AND THAT CAUSED THE POWER LOSS.

Other reports on N6910W · 1

Matched to the same aircraft by N-number and date.