20130510007239I

Incident · Minor damage

FAA incident report · Piper PA-28-201T · Corcoran, CA · May 10, 2013

Date
May 10, 2013 · 15:57 local
Place
Corcoran, CA
Airport
Salyer Farms Airport
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N8168Z
Reported as
Piper PA-28-201T
Reported engine
Continental TSIO-360 series
People aboard
3
Fatal injuries
0
Other 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.

Approximately 1 hour into a part 91 flight, at a cruising altitude of 10,500 ft, the pilot noted an uncommanded decrease of manifold pressure, which was followed by a loss of oil pressure and engine performance. With the assistance of oakland center, the pilot was directed to 24CL. Approximately 2 miles from the airport, the pilot reported the a loud ?pop? And the engine ceased to produce power. The pilot performed successful emergency landing at 24CL. Inspection of the aircraft/engine at 24CL revealed approximately a 4?? Inch in diameter hole in the engine casing at base of the #2 cylinder connecting rod. Engine serial number: 237400.r engine tsmoh: 1240.0

As the FAA filed it

APPROXIMATELY 1 HOUR INTO A PART 91 FLIGHT, AT A CRUISING ALTITUDE OF 10,500 FT, THE PILOT NOTED AN UNCOMMANDED DECREASE OF MANIFOLD PRESSURE, WHICH WAS FOLLOWED BY A LOSS OF OIL PRESSURE AND ENGINE PERFORMANCE. WITH THE ASSISTANCE OF OAKLAND CENTER, THE PILOT WAS DIRECTED TO 24CL. APPROXIMATELY 2 MILES FROM THE AIRPORT, THE PILOT REPORTED THE A LOUD ?POP? AND THE ENGINE CEASED TO PRODUCE POWER. THE PILOT PERFORMED SUCCESSFUL EMERGENCY LANDING AT 24CL. INSPECTION OF THE AIRCRAFT/ENGINE AT 24CL REVEALED APPROXIMATELY A 4?? INCH IN DIAMETER HOLE IN THE ENGINE CASING AT BASE OF THE #2 CYLINDER CONNECTING ROD. ENGINE SERIAL NUMBER: 237400.R ENGINE TSMOH: 1240.0