POWER LOSS OCCURRED ABOUT 7 MIN AFTER TAKEOFF. THE PLT TURNED BACK TOWARD THE ARPT BUT WAS UNABLE TO REACH THE ARPT DUE TO A 15-20 KT HEADWIND. THE ACFT LANDED HARD COLLAPSING THE LANDING GEAR AFTER THE PLT MUSHED THE ACFT TO CLEAR WIRES. EXAMINATION & FLOW TEST OF THE FUEL CONTROLLER REVEALED NUMEROUS DISCREPANCIES, OBSOLETE PARTS & FLOW CHARACTERISTICS WELL BELOW ACCEPTABLE STANDARDS. THE ENG…
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.