THE PILOT REMOVED THE VACUUM PUMP FROM THE ENGINE PRIOR TO THE FLIGHT BECAUSE OF AN INTERNAL FAILURE IN THE PUMP. THE PILOT DID NOT INSTALL A COVER PLATE ON THE ACCESSORY MOUNTING HOLE VACATED BY THE PUMP. AFTER TAKEOFF ON THE LOCAL FLIGHT, THE PILOT NOTICED THE OIL PRESSURE WAS DROPPING AND THE TEMPERATURE WAS RISING. HE ELECTED TO RETURN TO THE AIRPORT. THE ENGINE SIEZED AND THE PILOT MADE A…
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
Airframe (M20E)Only with: Equipped with an O & N Bladder Fuel Cell installed per STC SA2277CE or STC SA2350CE (for M20B, incorporated by field approval).
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (0)
No Service Difficulty Reports found for this airframe since 1995.