N1068G2004 Mooney M20R
Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply2 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Canopy Ministries INC
- Owner type
- Corporation
- City, state
- Mountain City, TN
- Certificate issued
- May 26, 2010
- Expires
- Apr 30, 2030
- Airworthiness
- Standard · Normal
- Airworthiness date
- Jun 8, 2004
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Mooney
- Model
- M20R
- Year
- 2004
- Serial number
- 29-0328
- Aircraft type
- Fixed wing single engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 2
- Engines
- 1
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A01E75
Engine
- Make and model
- Cont Motor Io-550 Series
- Type
- Reciprocating
- Power
- 300 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2010 – nowCanopy Ministries INCMountain City, TN · current
- 1998 – 1999Individual ownerColumbus, IN · different airframe: Solmos Bryan Exec 90 S/N 1068
- until 1990Individual ownerdifferent airframe: Mooney M20k S/N 251219
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (6)
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 (M20R)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 (M20R) |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (IO-550 SERIES)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed. |
| 2007-05-04 | Mooney Airplane Company, Inc., (Mooney) Models M20M and M20R Airplanes | Apr 9, 2007 | Airframe (M20R)Certain serial numbers: M20M 27-0317–27-0355; M20R 29-0290–29-0448 |
| 99-11-07 | Mooney Aircraft Corporation Model M20R Airplanes | Jun 15, 1999 | Airframe (M20R)Certain serial numbers: M20R 29-0033; M20R 29-0062; M20R 29-0088; M20R 29-0090; M20R 29-0092; M20R 29-0096; … |
Show all 6 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 98-21-26 | Mooney Aircraft Corporation Models M20J, M20K, M20M, and M20R Airplanes | Nov 26, 1998 | Airframe (M20R)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.
Service Difficulty Reports (2)
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.
- Reciprocating engine · oil cooler · damagedAug 9, 2017
DURING AN ANNUAL INSPECTION, MINOR EVIDENCE OF FRETTING FROM VIBRATION WAS SEEN AT OIL COOLER CROSSBAR LOWER AFT CORNER. FURTHER INSPECTION REVEALED A CRACKED WELD ON THE UPPER RT FWD CORNER THAT WAS 1 INCH LONG. REMOVED THE OIL COOLER FOR INSPECTION. THE TERMINATION OF THE WELD BEAD WAS LEFT…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Reciprocating engine · cylinder head · crackedJan 26, 2015
FOUND CRACK IN CYLINDER HEAD BETWEEN THE SPARK PLUG HOLE AND THE INJECTOR HOLE AT ANNUAL INSPECTION AT 1,314.4 HRS. CYLINDER LEAK DOWN WAS 24/80 AND IT WAS DISCOVERED THAT THE MAJORITY OF THE AIR WAS GOING PAST THE INTAKE VALVE DUE TO CORE SHIFT IN THE CASTING CAUSED BY THE CRACK. CYLINDER WAS…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026