20011020032649I

Incident

FAA incident report · Piper PA-28-140 · St. Marys, KS · October 20, 2001

Date
October 20, 2001 · 10:50 local
Place
St. Marys, KS
Phase of flight
Normal Cruise
Operating rules
General operating rules (Part 91)
Aircraft
N1818J
Reported as
Piper PA28140
Reported engine
Lycoming O320D2A
People aboard
2
Fatal injuries
0
Pilot’s flight hours
420 total370 in this make and model30 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) Saturday October 20, 2001 N1818J enroute from topeka (top) to wamego, KS (69K). A loud pop was heard from the engine followed by a decrease and loss of oil pressure. An emergency landing was performed in a field approximately 1.5 miles south of St. Marys, KS, south of white sands road, without further incident. The #3 engine cylinder head was found separated from the cylinder barrel (assembly p/n AEL65102-4.1/CCST4.1CA) just above the 3rd cooling fin of the cylinder head. The push rod tubes for the #3 cylinder were separated from the case allowing the tappet plunger assembly to exit the engine case resulting in the engine oil being pumped out of the tappet body.

As the FAA filed it

(-23) SATURDAY OCTOBER 20, 2001 N1818J ENROUTE FROM TOPEKA (TOP) TO WAMEGO, KS (69K). A LOUD POP WAS HEARD FROM THE ENGINE FOLLOWED BY A DECREASE AND LOSS OF OIL PRESSURE. AN EMERGENCY LANDING WAS PERFORMED IN A FIELD APPROXIMATELY 1.5 MILES SOUTH OF ST. MARYS, KS, SOUTH OF WHITE SANDS ROAD, WITHOUT FURTHER INCIDENT. THE #3 ENGINE CYLINDER HEAD WAS FOUND SEPARATED FROM THE CYLINDER BARREL (ASSEMBLY P/N AEL65102-4.1/CCST4.1CA) JUST ABOVE THE 3RD COOLING FIN OF THE CYLINDER HEAD. THE PUSH ROD TUBES FOR THE #3 CYLINDER WERE SEPARATED FROM THE CASE ALLOWING THE TAPPET PLUNGER ASSEMBLY TO EXIT THE ENGINE CASE RESULTING IN THE ENGINE OIL BEING PUMPED OUT OF THE TAPPET BODY.

Other reports on N1818J · 1

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