Safety record in brief:1 NTSB accident (substantial damage, Jul 2008)5 ADs may apply1 service difficulty report
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.
The pilot's failure to maintain aircraft control during a go-around, resulting in an aerodynamic stall. Contributing to the accident was the high density altitude.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DEN08LA118)
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 |
|---|---|---|---|
| 2014-15-18 | Fuselage, Stabilizer Attach Fittings | Aug 20, 2014 | Airframe (M20M)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 (M20M) |
| 2007-05-04 | Mooney Airplane Company, Inc., (Mooney) Models M20M and M20R Airplanes | Apr 9, 2007 | Airframe (M20M)Certain serial numbers: M20M 27-0317–27-0355; M20R 29-0290–29-0448 |
| 2004-23-17 | Mooney Airplane Company, Inc., Model M20M Airplanes | Dec 1, 2004 | Airframe (M20M)Certain serial numbers: M20M 27-0001–27-0321 |
| 98-21-26 | Mooney Aircraft Corporation Models M20J, M20K, M20M, and M20R Airplanes | Nov 26, 1998 | Airframe (M20M)Certain serial numbers: M20J 24-3415; M20J 24-3416; M20K 25-2018–25-2021; M20M 27-0241; M20R 29-0135–29-0138 |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
TURBOCHARGER V BAND CLAMP PN NH1009399-10/40D23255-340M FOUND CRACKED .7500 THRU OUTER STRAP. AD2004-23-17, EFF. DATE 12/1/2004 CALLS FOR REPLACEMENT OF THIS CLAMP. THIS IS THE NEW STYLE CLAMP THAT WAS FOUND CRACKED. CLAMP OUTER STRAP CRACK IS WITHIN .1250 INCH OF FAILURE. RECORDS INDICATE NO…
From FAA Service Difficulty Reports; matched by N-number and serial number.