WHILE CLIMBING, APRX 10 MILES WEST OF THE DEPARTURE AIRPORT, THE ENG LOST POWER. THE PLT ATTEMPTED TO GLIDE BACK TO THE ARPT. WHEN HE REALIZED HE COULD NOT REACH THE ARPT, HE SELECTED A GRASSY FIELD FOR AN EMERGENCY LANDING. DURING THE LANDING ROLL, THE RIGHT WING COLLIDED WITH A FENCE POST. DURING AN EXAM OF THE ENG, FOREIGN MATERIAL WAS FOUND IN THE BENDIX FUEL INJECTOR.
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.