Skip to content
KnownTail
Aircraft record

N101DX2000 Mooney M20R

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply2 service difficulty reports

Registration
Valid
expires Aug 31, 2028
Based in
Templeton, CA
owner city / state
Engine
IO-550 SERIES · 300 hp
Cont Motor
Owners
1
since 2018
NTSB events
None
since 1982
ADs may apply
6
confirm with A&P
Service reports
2
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Individual owner
City, state
Templeton, CA
Certificate issued
Aug 2, 2018
Expires
Aug 31, 2028
Airworthiness
Standard · Normal
Airworthiness date
Apr 7, 2000

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 data

Airframe

Manufacturer
Mooney
Model
M20R
Year
2000
Serial number
29-0221
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
A008CC

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
  1. 2018 – nowIndividual ownerTempleton, CA · current
  2. until 1988Individual ownerdifferent airframe: Beechcraft 200 S/N Bb256

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs 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.

ADSubjectEffectiveApplies to
2014-15-18Fuselage, Stabilizer Attach FittingsAug 20, 2014Airframe (M20R)Certain serial numbers: M20C 2313; M20E 761; M20M 27-0057; M20R 29-0141; M20R 29-0513–29-0519; M20TN 31-0101–31-0127
2012-05-09Mooney Aviation Company, Inc. (Mooney) AirplanesMar 20, 2012Airframe (M20R)
2009-16-03Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating…Sep 9, 2009Engine (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.
2007-05-04Mooney Airplane Company, Inc., (Mooney) Models M20M and M20R AirplanesApr 9, 2007Airframe (M20R)Certain serial numbers: M20M 27-0317–27-0355; M20R 29-0290–29-0448
99-11-07Mooney Aircraft Corporation Model M20R AirplanesJun 15, 1999Airframe (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 ADs
ADSubjectEffectiveApplies to
98-21-26Mooney Aircraft Corporation Models M20J, M20K, M20M, and M20R AirplanesNov 26, 1998Airframe (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.

  • Engine controls · clamp · wornOct 12, 2002

    OWNER COMPLAINED THAT HE WAS UNABLE TO CLOSE THROTTLE TO LAND. THE MIXTURE HAD TO BE MOVED TO CUT-OFF TO LAND. INVESTIGATION REVEALED THAT THE THROTTLE CABLE HOUSING WAS MOVING IN THE CLAMP LOCATED AT THE THROTTLE BODY PREVENTING THE THROTTLE FROM CLOSING ALL THE WAY. THE CLAMP HALVES WERE WORN…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Propellers · bulkhead · crackedSep 30, 2002

    THE SPINNER BULKHEAD WAS FOUND CRACKED COMPLETELY AROUND THE CIRCUMFERENCE OF THE MOUNTING FLANGE. THE TOTAL TIME ON THE SPINNER ASSEMBLY IS 315.5 HOURS. THIS IS THE THIRD CRACKED BULKHEAD FOUND ON THIS AIRCRAFT. THE TIME IN SERVICE OF THIS BULKHEAD IS 42.8 HOURS. THE FIRST BULKHEAD WAS FOUND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

Request owner name removalReport an error in this record