Safety record in brief:1 NTSB accident (substantial damage, Mar 2012)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 extend the landing gear before landing.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA12CA247)
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 |
|---|---|---|---|
| 2012-05-09 | Mooney Aviation Company, Inc. (Mooney) Airplanes | Mar 20, 2012 | Airframe (M20J) |
| 2004-25-04 | Mooney Aircraft Corporation Models M20B, M20C, M20D, M20E, M20F, M20G, and M20J Airplanes | Jan 21, 2005 | Airframe (M20J)Only with: Equipped with an O & N Bladder Fuel Cell installed per STC SA2277CE or STC SA2350CE (for M20B, incorporated by field approval). |
| 98-21-26 | Mooney Aircraft Corporation Models M20J, M20K, M20M, and M20R Airplanes | Nov 26, 1998 | Airframe (M20J)Certain serial numbers: M20J 24-3415; M20J 24-3416; M20K 25-2018–25-2021; M20M 27-0241; M20R 29-0135–29-0138 |
| 97-26-08 | Mooney Aircraft Corporation Models M20F, M20J, and M20L Airplanes | Jan 20, 1998 | Airframe (M20J)Certain serial numbers: M20J 24-0001–24-3381; M20L 26-0001–26-0041 |
| 95-26-16 R1 | Mooney Aircraft Corporation Model M20J Airplanes | May 16, 1996 | Airframe (M20J)Certain serial numbers: M20J 24-0001–24-3250; M20J 24-3252–24-3374 |
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.
DURING INSPECTION, A CRACK WAS FOUND AT THE LEFT LOWER FUSELAGE SKIN AT BS -5.375 WHERE THE FUSELAGE SKIN ENDS AT THE FIREWALL AREA. THE CRACK EMANATED FROM THE EDGE OF THE SKIN, EXTENDED THROUGH A RIVET HOLE AND BACK OUT, ANGLING BACK TOWARDS THE SKIN EDGE AGAIN. THE CRACK WAS APPROXIMATELY 1.5…
From FAA Service Difficulty Reports; matched by N-number and serial number.