Safety record in brief:1 NTSB accident (substantial damage, Jul 1998)4 ADs may apply
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
Fatigue cracking of the propeller blade which originated from corrosion pitting on its camber side, resulting in the blade tip separation during cruise flight.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for FTW99LA025)
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.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2023-02-04 | Mooney International Corporation Airplanes | Feb 13, 2023 | Airframe (M20C)Certain serial numbers: …–680170 |
| 2014-15-18 | Fuselage, Stabilizer Attach Fittings | Aug 20, 2014 | Airframe (M20C)Certain serial numbers: M20C 2313; M20E 761; M20M 27-0057; M20R 29-0141; M20R 29-0513–29-0519; M20TN 31-0101–31-0127 |
| 2012-05-09 | Mooney Aviation Company, Inc. (Mooney) Airplanes | Mar 20, 2012 | Airframe (M20C) |
| 2004-25-04 | Mooney Aircraft Corporation Models M20B, M20C, M20D, M20E, M20F, M20G, and M20J Airplanes | Jan 21, 2005 | Airframe (M20C)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.
No Service Difficulty Reports found for this airframe since 1995.