19980705032229I

Incident · Minor damage

FAA incident report · Cessna 210K · Shaver Lake, CA · July 5, 1998

Date
July 5, 1998 · 08:10 local
Place
Shaver Lake, CA
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N5763J
Reported engine
Continental IO520L
People aboard
2
Fatal injuries
0
Pilot’s flight hours
800 total

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.

On July 10 1998, aircraft N5763J was transported to del-air aviation, in proterville, CA. Where a closer engine inspection was performed. This confirmed that an aeroquip e-z drain sump valve, part number AE99950G, faa-pma approved, was a possible contributing factor, in the complete loss of engine oil. A landing gear retract functional check was performed evidence shows that the nose wheel strut assemble, contacted the e-z drain sump valve. The a safety recommendation will be given consideration. Damage to propeller indicates the engine was not developing power at time of impact. Examination of the engine revealed a three to four inch hole in the top of the crankcase inboard of the number four cylinder. The engine oil dipstick did not indicate any oil in the engine.

As the FAA filed it

ON JULY 10 1998, AIRCRAFT N5763J WAS TRANSPORTED TO DEL-AIR AVIATION, IN PROTERVILLE, CA. WHERE A CLOSER ENGINE INSPECTION WAS PERFORMED. THIS CONFIRMED THAT AN AEROQUIP E-Z DRAIN SUMP VALVE, PART NUMBER AE99950G, FAA-PMA APPROVED, WAS A POSSIBLE CONTRIBUTING FACTOR, IN THE COMPLETE LOSS OF ENGINE OIL. A LANDING GEAR RETRACT FUNCTIONAL CHECK WAS PERFORMED EVIDENCE SHOWS THAT THE NOSE WHEEL STRUT ASSEMBLE, CONTACTED THE E-Z DRAIN SUMP VALVE. THE A SAFETY RECOMMENDATION WILL BE GIVEN CONSIDERATION. DAMAGE TO PROPELLER INDICATES THE ENGINE WAS NOT DEVELOPING POWER AT TIME OF IMPACT. EXAMINATION OF THE ENGINE REVEALED A THREE TO FOUR INCH HOLE IN THE TOP OF THE CRANKCASE INBOARD OF THE NUMBER FOUR CYLINDER. THE ENGINE OIL DIPSTICK DID NOT INDICATE ANY OIL IN THE ENGINE.

Other reports on N5763J · 1

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