# Mooney International M20R

- Type: Aircraft model (FAA registry)
- Registry code: 5870229
- Manufacturer (registry): MOONEY INTERNATIONAL CORP
- Model: M20R
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · Reciprocating
- Seats: 4
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS 2A3](https://openairdocs.org/tcds/2A3) (OpenAirDocs)
- Holder: Mooney International Corporation
- Registered aircraft: 4
- Page: https://openairdocs.org/model/mooney-international-m20r

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2024-14-03](https://openairdocs.org/ad/2024-14-03): Autopilot System · Garmin GFC 500 Autopilot (STC SA01866WI). Effective Aug 20, 2024
- [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2014-15-18](https://openairdocs.org/ad/2014-15-18): Fuselage, Stabilizer Attach Fittings · Mooney International M20C, M20E, M20M and 2 more. Effective Aug 20, 2014
- [AD 2012-05-09](https://openairdocs.org/ad/2012-05-09): Stabilizers · Mooney M20B, M20C, M20D and 10 more. Effective Mar 20, 2012
- [AD 2008-02-06](https://openairdocs.org/ad/2008-02-06): GSM 85 servo gearbox units · Cessna 182T, 206H, LC40-550FG and 11 more. Effective Feb 26, 2008
- [AD 2007-05-04](https://openairdocs.org/ad/2007-05-04): Upper left and upper right engine mount attaching · Mooney M20M and M20R. Effective Apr 9, 2007
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001
- [AD 2001-10-09](https://openairdocs.org/ad/2001-10-09): Automatic Flight Control Systems · Aerostar PA-60-700P (Aerostar 700P), 208, 208B and 15 more. Effective Jun 15, 2001
- [AD 99-11-07](https://openairdocs.org/ad/99-11-07): Air Conditioning System · Mooney M20R. Effective Jun 15, 1999
- [AD 98-24-11](https://openairdocs.org/ad/98-24-11): Aileron Control Links · Mooney M20B, M20C, M20D and 8 more. Effective Dec 28, 1998
- [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998
- [AD 98-21-26](https://openairdocs.org/ad/98-21-26): Main Landing Gear Side Brace Bolt · Mooney M20J, M20K, M20M and 1 more. Effective Nov 26, 1998
- [AD 98-14-03](https://openairdocs.org/ad/98-14-03): Transponders · Cessna 172, 172A, 172B and 230 more. Effective Aug 16, 1998
- [AD 95-12-16](https://openairdocs.org/ad/95-12-16): Exhaust System · Mooney M20R. Effective Jun 22, 1995
- [AD 75-23-04](https://openairdocs.org/ad/75-23-04): Electric Gear Systems · Mooney M20, M20A, M20B and 12 more. Effective Dec 8, 1975

Historical (superseded or no longer in force):

- [AD 2012-03-52](https://openairdocs.org/ad/2012-03-52) (historical): Stabilizers · Mooney M20R and M20TN. Effective Feb 29, 2012

## Information bulletins (advisory) (6)

- [SAIB 2023-02](https://openairdocs.org/saib/2023-02): Landing Gear System. Issued Mar 3, 2023
- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-14-12](https://openairdocs.org/saib/CE-14-12): Landing Gear System. Issued Mar 14, 2014
- [SAIB NE-13-32](https://openairdocs.org/saib/NE-13-32): Propeller Spinner Section. Issued May 9, 2013
- [SAIB CE-09-12](https://openairdocs.org/saib/CE-09-12): Navigation: CRS/BARO Knob Interference in some G1000/G900X/G950 Installations. Issued Feb 11, 2009
- [SAIB SW-02-46](https://openairdocs.org/saib/SW-02-46): . Issued Sep 11, 2002

## Registered aircraft (4)

- [N2011T](https://openairdocs.org/aircraft/N2011T): [Efferson Randal K](https://openairdocs.org/faa-owner/EFFERSON%20RANDAL%20K), [Lapine, AL](https://openairdocs.org/faa-place/AL/Lapine), built 2016, S/N 29-0524
- [N521FH](https://openairdocs.org/aircraft/N521FH): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 2015, S/N 29-0521
- [N5251F](https://openairdocs.org/aircraft/N5251F): [Waypoint Services LLC](https://openairdocs.org/faa-owner/WAYPOINT%20SERVICES%20LLC), [Missoula, MT](https://openairdocs.org/faa-place/MT/Missoula), built 2016, S/N 29-0525
- [N79339](https://openairdocs.org/aircraft/N79339): [Wetzel Matthew DBA](https://openairdocs.org/faa-owner/WETZEL%20MATTHEW%20DBA), [Round Mountain, TX](https://openairdocs.org/faa-place/TX/Round%20Mountain), built 1998, S/N 29-0171

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (52, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2017FA0000383](https://openairdocs.org/sdr/2017FA0000383), Aug 9, 2017: OIL COOLER. DAMAGED. DURING AN ANNUAL INSPECTION, MINOR EVIDENCE OF FRETTING FROM VIBRATION WAS SEEN AT OIL COOLER CROSSBAR LOWER AFT CORNER. FURTHER INSPECTION REVEALED A CRACKED W
- [SDR 2016FA0000013](https://openairdocs.org/sdr/2016FA0000013), Nov 25, 2015: ENGINE. POWER LOSS. APPROXIMATELY 12 TO 15 MILES FROM AIRPORT, ENGINE BEGAN TO RUN ROUGH. THE TOWER WAS ADVISED AND THE ACFT WAS CLEARED FOR A STRAIGHT IN LANDING. TAXIED TO RAMP W
- [SDR 9PRR2015FA0000283](https://openairdocs.org/sdr/9PRR2015FA0000283), Jun 23, 2015: DISPLAY. FAILED. PILOT REPORTED ODOR OF SMOKE. MFD SCREEN FAILED.
- [SDR 2015FA0000316](https://openairdocs.org/sdr/2015FA0000316), Jun 22, 2015: DISPLAY. FAILED. AIRCRAFT DEPARTED . DUE TO AN ODOR OF SMOKE IN THE COCKPIT THE AIRCRAFT RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT AND WAS TOWED TO THE RAMP. TROUBLESHOOTIN
- [SDR 2015FA0000075](https://openairdocs.org/sdr/2015FA0000075), Jan 26, 2015: CYLINDER HEAD. CRACKED. 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 DISC
- [SDR 2011FA0000746](https://openairdocs.org/sdr/2011FA0000746), Nov 15, 2011: ACTUATOR. NOISY. DURING ROUTINE INSPECTION OF ACFT LANDING GEAR RETRACTION SYS, THE LANDING GEAR ACTUATOR WAS EXCESSIVELY NOISEY WHEN THE LANDING GEAR WAS RETRACTED AND EXTENDED
- [SDR 2010FA0000663](https://openairdocs.org/sdr/2010FA0000663), Jun 30, 2010: HOSE. DETERIORATED. PILOT NOTICED A LOW VAC WARNING OF THE ENGINE DRIVEN VACCUME PUMP. TURN THE SWITCH ON FOR THE STANDBY VAC SYS AND THE CIRCUIT BREAKER POPPED. FOUND THE CAUSE OF
- [SDR 2009FA0000254](https://openairdocs.org/sdr/2009FA0000254), Mar 25, 2009: WIRE. MELTED. PILOT REPORTED THE DEFROST BLOWER CIRCUIT BREAKER POPS WHEN BLOWER IS NOT IN USE. TROUBLESHOOTING REVEALED THE LANDING LIGHTS STAYED ON WHEN THE LANDING LIGHT C
- [SDR FAA1020001](https://openairdocs.org/sdr/FAA1020001), Sep 21, 2006: SELECTOR VALVE. STUCK. FUEL SELECTOR VALVE STUCK IN (OFF) POSITION WHILE AIRCRAFT WAS SITTING ON THE RAMP. ONCE STUCK IN THE OFF POSITION, IT BECAME IMPOSSIBLE TO TURN USING HAND FORC
- [SDR 2007FA0000734](https://openairdocs.org/sdr/2007FA0000734), Jul 24, 2006: VOLT REGULATOR. FAILED. THE INABILITY OF THE VOLTAGE REGULATOR (PN 800397-501, SN 0165) TO CONTROLTHE OUTPUT OF THE ALTERNATOR WHEN THE BATTERY SWITCH WAS TOGGLED BETWEEN THE NR1 AND N
- [SDR 2006FA0000096](https://openairdocs.org/sdr/2006FA0000096), Jan 17, 2006: TRANSMITTER. INTERMITTENT. ELT TRANSMITTER WAS REMOVED DURING ANNUAL FOR BATTERY REPLACEMENT AND TESTING. UPON TEST WITH BATTERIES REPLACED. THE UNIT ON/OFF WAS INTERMITTENT AND THE REMOT
- [SDR 2005FA0001288](https://openairdocs.org/sdr/2005FA0001288), Aug 29, 2005: WIRE HARNESS. BURNED. WHEN TROUBLESHOOTING THE SQUAWK (RECOGNITION LIGHTS ON ALL THE TIME), FOUND CHARED WIRE INSULATION IN THE WIRE HARNESS FEEDING THE OVERHEAD BANK OF SWITCHES THA
- [SDR 2005FA0001287](https://openairdocs.org/sdr/2005FA0001287), Aug 29, 2005: WIRE HARNESS. BURNED. WHEN TROUBLESHOOTING, THE SQUAWK (RECOGNITION LIGHTS ON ALL THE TIME) WE FOUND CARRED WIRE INSULATION IN THE WIRE HARNESS FEEDING THE OVERHEAD BANK OF SWITCHES 
- [SDR 2005FA0001044](https://openairdocs.org/sdr/2005FA0001044), Jul 14, 2005: GASCOLATOR. LEAKING. DURING TROUBLESHOOTING, IT WAS DISCOVERED THAT THE GASCOLATOR WAS ALLOWING AIR TO BE INTRODUED INTO THE SHIPS FUEL SYSTEM PRIOR TO THE FUEL REACHING THE ENGINE 
- [SDR T7419](https://openairdocs.org/sdr/T7419), May 9, 2005: BULKHEAD. CRACKED. SPINNER BULKHEAD CRACKING AT 50HRS TKS WAS INSTALLED BY AIRCRAFT FACTORY. 1ST BULKHEAD REPLACED AT 104 HRS, 2CD BULKHEAD REPLACED AT 249.5 HRS. COULD NOT DETERM
- [SDR 2005FA0000176](https://openairdocs.org/sdr/2005FA0000176), Feb 1, 2005: OIL COOLER. CRACKED. DURING ROUTINE OIL CHANGE, AN EXAMINATION OF THE OIL COOLER FLANGE AREA WHERE IT BOLTS ONTO THE ENGINE STUDS WAS FOUND TO BE CRACKED. THE CRACK WAS LOCATED BETW
- [SDR 2005FA0000203](https://openairdocs.org/sdr/2005FA0000203), Jan 20, 2005: MUFFLER. CRACKED. VERY SIMILAR TO THE CRACKS REFERENCED IN AD NR 95-12-16 BUT ITS OUTSIDE OF THE SN RANGE LISTED. (K)
- [SDR 2005FA0000950](https://openairdocs.org/sdr/2005FA0000950), Jan 15, 2005: PUMP. FAILED. THIRD FUEL PUMP FAILURE ON AIRCRAFT/ENGINE IN APPROX 90 HRS. FUEL PUMP RETURNED TO CONT FOR ANALYSIS BUT THEY WERE NOT ABLE TO LOCATE FOR TESTING/ANALYSIS. NEIT
- [SDR HJL2004F00001](https://openairdocs.org/sdr/HJL2004F00001), Sep 9, 2004: SPRING. FAILED. REPLACED (NO BACK) SPRING, INSP GEARS AND ACTUATOR IAW SB M20-282 AND SI 102000-1-901 REV 2. ON 9-3-2004, AFTER 16 HOURS, GEAR DOWN SAFETY LIGHT WOULD INDICATE 
- [SDR MPY2004F00000](https://openairdocs.org/sdr/MPY2004F00000), Jul 12, 2004: HEAT SHIELD. GOUGED. HEAT SHIELD PN 600429-503 WAS FOUND TO BE MAKING CONTACT WITH TUBULAR ENGINE MOUNT. THIS CONTACT CREATED A GOUGE APPROX .200 INCH LONG AND APPROX .045 INCH DEEP
- [SDR 2004FA0000549](https://openairdocs.org/sdr/2004FA0000549), Jul 10, 2004: HEAT SHIELD. GOUGED. HEAT SHIELD WAS FOUND TO BE MAKING CONTACT WITH TUBULAR ENGINE MOUNT. THIS CONTACT CREATED A GOUGE APPROXIMATELY .200 INCH IN LENGTH AND APPROXIMATELY .045 INCH
- [SDR 2005FA0000946](https://openairdocs.org/sdr/2005FA0000946), Apr 28, 2004: PUMP. FAILED. ENGINE FAILED ON FINAL APPROACH. WAS ABLE TO RESTART AFTER LANDING BUT HAD TO PULL THE MIXTURE CONTROL LEAN ABOUT 1INCH TO KEEP IT RUNNING. AFTER COOLDOWN, MIXT
- [SDR 2004FA0000216](https://openairdocs.org/sdr/2004FA0000216), Feb 17, 2004: ROLL PIN. SHEARED. SHEAR PINS ON LT MLG TUBE ASSEMBLY FAILED. AFT INSERT SEPARATED FROM TUBE ASSEMBLY. LT MAIN GEAR SUBSEQUENTLY REMAINED UNSAFE AND RETRACTED UPON CONTACT WITH RU
- [SDR ROSENBERG](https://openairdocs.org/sdr/ROSENBERG), Jan 23, 2004: FLUID. SOLIDIFIED. DURING ANNUAL INSPECTION IT WAS NOTED THAT THE AIRCRAFT WAS VERY HARD TO TAXI. TOOK HIGH RPM'S TO GET AIRCRAFT TO MOVE AND PULLED TO THE RIGHT. CHECKED BRAKES. 
- [SDR 2004FA0000054](https://openairdocs.org/sdr/2004FA0000054), Jan 9, 2004: CYLINDER. CRACKED. ENGINE INTAKE TUBE P/N 646207 FOR THE NR 6 CYLINDER CRACKS OUT AT ITS CYLINDER FLANGE. THIS ENGINE HAS CRACKED 3 INTAKE TUBES. THE CRACKS HAVE BEEN FOUND FROM .
- [SDR 2003FA0000780](https://openairdocs.org/sdr/2003FA0000780), Jul 17, 2003: SPRING. BROKEN. PILOT WAS UNABLE TO LOWER LANDING GEAR INVESTIGATION REVEALED THAT THE SUBJECT SPRING HAD A BROKEN TANG. RESULTING FAILURE OF LANDING GEAR ACTUATOR. MOONEY SB M
- [SDR 2003FA0000517](https://openairdocs.org/sdr/2003FA0000517), May 12, 2003: TRUSS. BROKEN. A/C RECEIVED STRUCTURAL DAMAGE DURING LANDING. (THE RECORDS SHOW A NEW 540017-509 (TRUSS ASSY, NOSE GEAR, UPPER, RETRACT) WAS INSTALLED IN A/C AT THE TIME OF RE
- [SDR 2003FA0000183](https://openairdocs.org/sdr/2003FA0000183), Feb 18, 2003: BEARING. DISINTEGRATED. DURING INSTALLATION OF AN AIR/OIL SEPARATOR, REMOVED THE AIR CONDITIONER ACCESSORY DRIVE OFF THE STARTER SHAFT TO INSTALL AN OIL RETURN FITTING FOR THE AIR/OIL 
- [SDR 2003FA0000131](https://openairdocs.org/sdr/2003FA0000131), Jan 24, 2003: DISTRIBUTOR GEAR. STRIPPED. DISTRIBUTOR GEAR, MAGNETO INOPERATIVE ON RUN-UP ON INSPECTION FOUND TEETH SHEARED IN DISTRIBUTOR GEAR-90 DEGREES.
- [SDR 2002FA0001180](https://openairdocs.org/sdr/2002FA0001180), Oct 12, 2002: CLAMP. WORN. 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 HO
- [SDR 2002FA0001250](https://openairdocs.org/sdr/2002FA0001250), Oct 9, 2002: TUBE. CRACKED. INSPECTED AIRCRAFT ENGINE DURING ROUTINE OIL CHANGE AND NOTICED FUEL STAIN ON NR 6 INTAKE TUBE. REMOVED TUBE AND FOUND TO BE CRACKED AT FLANGE PART HAD BEEN REP
- [SDR 2002FA0001156](https://openairdocs.org/sdr/2002FA0001156), Sep 30, 2002: BULKHEAD. CRACKED. 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 I
- [SDR 2002FA0000755](https://openairdocs.org/sdr/2002FA0000755), May 8, 2002: ROD END. BROKEN. ROD-END BEARING FAILED ON RIGHT RETRACT ROD.
- [SDR 2001FA0000268](https://openairdocs.org/sdr/2001FA0000268), Aug 20, 2001: THROTTLE ARM. WORN. THE PRESSED IN BUSHING AT THE END OF THE THROTTLE ARM WAS WORN THRU. THE BRONZE SECTION. (ATTACHED PHOTO)
- [SDR 2001FA0000241](https://openairdocs.org/sdr/2001FA0000241), May 22, 2001: TUBE. CRACKED. INDUCTION TUBE AT NR 6 CYLINDER IS COMPLETELY CRACKED AT FLANGED END.
- [SDR 20010605CW018](https://openairdocs.org/sdr/20010605CW018), May 4, 2001: TRANSMITTER. FAILED. DURING ANNUAL INSPECTION, PERFORMED ELT INSPECTION IAW FAR 91.207D, AND FOUND THAT ELT DOES NOT TRANSMIT A SIGNAL EVEN THOUGH RED TRANSMIT LIGHT ON UNIT LIGHTS 
- [SDR 20010524CW001](https://openairdocs.org/sdr/20010524CW001), Apr 27, 2001: THROTTLE ARM. WORN. WHILE WARMING THE ENGINE FOR OIL CHANGE, NOTED THAT THERE WAS AN EXCESSIVE AMOUNT OF FREE PLAY IN THE THROTTLE LINKAGE. AFTER RUNNING THE ENGINE UP TO 1500 RPM,
- [SDR 20010322CW013](https://openairdocs.org/sdr/20010322CW013), Feb 2, 2001: CONNECTOR. SHORTED. DURING ANNUAL INSPECTION TAIL STROBE LIGHT WAS INOPERATIVE, ELECTRICAL ARCING ACROSS PINS IN CONNECTOR. CONNECTOR WAS LOCATED AT THE PIVOT POINT OF THE TAIL. (T
- [SDR 20000523SH025](https://openairdocs.org/sdr/20000523SH025), May 23, 2000: PLACARD. INCORRECT. THE OPERATION LIMITATIONS PLACARD DOES NOT MATCH THE TYPE CERTIFICATE DATA SHEET. THE MANEUVERING SPEED IS DIFFERENT. (X)
- [SDR 99ZZZX3826](https://openairdocs.org/sdr/99ZZZX3826), Sep 1, 1999: FUEL CELL. LEAKING. FUEL LEAK UNDER FOWARD AND AFT WING WALK. TWO INBOARD SCREWS.
- [SDR 99ZZZX3825](https://openairdocs.org/sdr/99ZZZX3825), Sep 1, 1999: FUEL CELL. LEAKING. FUEL LEAK UNDER FORWARD WING WALK TWO INBOARD SCREWS.
- [SDR 99ZZZX3811](https://openairdocs.org/sdr/99ZZZX3811), Sep 1, 1999: FUEL CELL. LEAKING. FUEL LEAK AT RIGHT WING INBOARD WING ATTACH POINT. ALSO, LEAKING AT FORWARD WING WALK AT INBOARD SCREWS.
- [SDR 99ZZZX3474](https://openairdocs.org/sdr/99ZZZX3474), Aug 17, 1999: INJECTOR. FAILED. NEW AIRCRAFT AND NEW ENGINE. ENGINE RAN ROUGH ON TAKEOFF, TOP COWL REMOVED AND COLD CYLINDER ESTABLISHED. UPON REMOVAL OF FUEL MANIFOLD, WRENCH WAS APPLIED TO I
- [SDR 99ZZZX3473](https://openairdocs.org/sdr/99ZZZX3473), Aug 17, 1999: CRANKSHAFT. FAILED. ENGINE SHOOK VIOLENTLY. MIXTURE CONTROL WAS PULLED BACK TO CUT-OFF IMMEDIATELY. THE ENGINE SEIZED UP. A SAFE LANDING WAS MADE. TEAR-DOWN INSPECTION REVEALED THE
- [SDR 99ZZZX2424](https://openairdocs.org/sdr/99ZZZX2424), May 6, 1999: LINK. CRACKED. PROPELLER LINK CRACKED.
- [SDR 20000714SH028](https://openairdocs.org/sdr/20000714SH028), Mar 23, 1999: ROD END. LOOSE. DURING ROUTINE ANNUAL INSP, FOUND EXCESSIVE PLAY AT ROLL PINS USED TO HOLD ROD ENDS IN PLACE FOR GEAR DOWN RETRACT/EXTENSION ROD ASSY AT LEAST .1250 INCH PLAY N
- [SDR 98ZZZX764](https://openairdocs.org/sdr/98ZZZX764), Feb 2, 1998: OIL COOLER. CRACKED. OIL COOLER INSPECTION FOUND A CRACK FORMED AT THE BASE OF THE FRONT INBOARD STIFFENER, IN WELD AREA. CRACK HAD PENETRATED THE WELD. SUSPECT CAUSE, BAD WELD.
- [SDR 98ZZZX1860](https://openairdocs.org/sdr/98ZZZX1860), Dec 2, 1997: FUEL PUMP. FAILED. WHILE UTILIZING THE ELECTRIC FUEL PUMP TO TRANSFER FUEL, THE PUMP FAILED IN ABOUT 15 MINUTES. THIS IS THE SECOND TIME IN A MONTH THIS MODEL WELDON PUMP FAILED I
- [SDR 97ZZZX1160](https://openairdocs.org/sdr/97ZZZX1160), Feb 14, 1997: HUB. FAILED. ALTERNATOR FAILURE IN-FLIGHT. INVESTIGATION REVEALED ALT DRIVE HUB HAD FAILED.
- [SDR 96ZZZX196](https://openairdocs.org/sdr/96ZZZX196), Dec 12, 1995: SUPPORT BRACKET. BROKEN. DURING ANNUAL INSPECTION, NOTED THE BAFFLE SUPPORT BRACKET UNDER THE FRONT CENTER SECTION OF ENGINE WAS BROKEN. OBTAINED NEW BRACKET AND INSTALLED. SUBMITTER ST

All 52: https://openairdocs.org/model/mooney-international-m20r/reports.md

## STCs that may be installed (OpenAirDocs) (219, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA01134DE](https://openairdocs.org/stc/SA01134DE): Installation of EarthX ETX680-24-TSO Lithium Battery. EarthX Inc
- [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Airwolf Filter Corporation
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA01866WI](https://openairdocs.org/stc/SA01866WI): Installation of Garmin GFC 500 Autopilot with Electronic Stability and Protection. Garmin International Inc
- [STC SA01005DE](https://openairdocs.org/stc/SA01005DE): Installation of a EarthX ETX900-TSO Lithium battery. EarthX Inc
- [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector. Alcor LLC
- [STC SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC. Lists M20 Series
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA1913SO](https://openairdocs.org/stc/SA1913SO): Installation of auxiliary fuel cells. KMAX Aero LLC
- [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics
- [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC
- [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA3540NM](https://openairdocs.org/stc/SA3540NM): Installation of modified nose gear bushings. LASAR Inc
- [STC ST01554LA](https://openairdocs.org/stc/ST01554LA): Installation of a Nose Landing Gear Steering Horn Assembly. LASAR Inc
- [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA04400NY](https://openairdocs.org/stc/SA04400NY): Installation of the Integrated Back-up Battery System (IBBS). TCW Technologies LLC
- [STC SA04192NY](https://openairdocs.org/stc/SA04192NY): KFD 900 Primary Flight Display System Additional Functions. Honeywell International Inc
- [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine
- [STC SA04586CH](https://openairdocs.org/stc/SA04586CH): Installation of Electroair Back Up Battery Panel System Control. Electroair Aquisition Corp
- [STC SA03165CH](https://openairdocs.org/stc/SA03165CH): Installation of MT Propeller model MTV-14-D/(188-193)-30( ) in Mooney aircraft models M20R, M20S and M20TN. McFarlane Aviation LLC
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc
- [STC SA04231CH](https://openairdocs.org/stc/SA04231CH): Installation and activation of a TruTrak Vizion autopilot system. Honeywell International Inc
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc
- [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King)
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA04181NY](https://openairdocs.org/stc/SA04181NY): Installation of the KFC 230 Aerocruze Automatic Flight Control System. Honeywell International Inc
- [STC SA02426AK](https://openairdocs.org/stc/SA02426AK): Approval of the FreeFlight FDL-978-TX ADS-B system installed. FreeFlight Systems
- [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA00824WI-D](https://openairdocs.org/stc/SA00824WI-D): Installation of Bendix/King KMD 150 MDF Multi-Function Display. Honeywell International Inc
- [STC SA00933WI-D](https://openairdocs.org/stc/SA00933WI-D): Installation of Bendix/King KMD 550 Multi-Function Display (MFD) system and optional Bendix/King KGP 560 General Aviation Enhanced ground proximity warning system (GA-EGPWS) and optional BF Goodrich WX 500 Stormscope. Honeywell International Inc
- [STC SA00934WI-D](https://openairdocs.org/stc/SA00934WI-D): Installation of Bendix/King KLN 94 GPS (Global Positioning System) Navigation Receiver for IFR enroute and non-precision approach operations. Honeywell International Inc
- [STC SA00771WI-D](https://openairdocs.org/stc/SA00771WI-D): Installation of Bendix/King KFC 225 automatic flight control system. Honeywell International Inc

All 219: https://openairdocs.org/model/mooney-international-m20r/stcs.md

## PMA parts (OpenAirDocs) (413, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [530021-000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198506145620260909151446.0001): Damper. Hutchinson Aerospace & Industry Inc. · PMA PQ0524NM · Replaces 96600-1 · May 19, 2026
- [LA148-720095-004](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197421754720251205185453.0001): 0.500 Removable Stud Assembly. LASAR Inc. · PMA PQ1208NM · Modification part · Nov 17, 2025
- [LA148-720095-005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185672508220251205185453.0001): Rod End Assembly. LASAR Inc. · PMA PQ1208NM · Modification part · Nov 17, 2025
- [LA148-720095-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169009974220251205185452.0001): Steering Horn Assembly. LASAR Inc. · PMA PQ1208NM · Modification part · Nov 17, 2025
- [LA148-720095-017](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113481946520251205185453.0001): “T” Shaft Assembly. LASAR Inc. · PMA PQ1208NM · Modification part · Nov 17, 2025
- [LA148-720020-501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111817357220251205185454.0001): Collar. LASAR Inc. · PMA PQ1208NM · Modification part · Nov 17, 2025
- [L025-914007-005-005AB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189952853820250508133423.0001): Oversize Bushing, NLG & MLG Shock Link. LASAR Inc. · PMA PQ1208NM · Modification part · Apr 10, 2025
- [L025-914007-004-005AB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165963182320250508133422.0001): Oversize Bushing, NLG Pivot. LASAR Inc. · PMA PQ1208NM · Modification part · Apr 10, 2025
- [L025-914020-021-005AB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162748189020250508133424.0001): Oversize Bushing, MLG Retraction Link. LASAR Inc. · PMA PQ1208NM · Modification part · Apr 10, 2025
- [L025-914007-003-005AB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154729916620250508133422.0001): Oversize Bushing, NLG & MLG Lower Leg. LASAR Inc. · PMA PQ1208NM · Modification part · Apr 10, 2025
- [L025-914020-145-005AB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152725293720250508133424.0001): Oversize Bushing, MLG Retraction Link. LASAR Inc. · PMA PQ1208NM · Modification part · Apr 10, 2025
- [L025-914020-143-005AB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151677647820250508133424.0001): Oversize Bushing, MLG Retraction Truss. LASAR Inc. · PMA PQ1208NM · Modification part · Apr 10, 2025
- [L025-914007-002-005AB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149983996120250508133422.0001): Oversize Bushing, NLG Pivot Truss. LASAR Inc. · PMA PQ1208NM · Modification part · Apr 10, 2025
- [L025-914020-017-005AB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148274148220250508133423.0001): Oversize Bushing, NLG & MLG Retraction Link. LASAR Inc. · PMA PQ1208NM · Modification part · Apr 10, 2025
- [L025-914020-019-005AB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114096748120250508133424.0001): Oversize Bushing, NLG & MLG Lower Leg. LASAR Inc. · PMA PQ1208NM · Modification part · Apr 10, 2025
- [L025-914007-013-005AB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103408223820250508133423.0001): Oversize Bushing, NLG Retraction Truss. LASAR Inc. · PMA PQ1208NM · Modification part · Apr 10, 2025
- [LSM-200-700-11](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169289122020250417183925.0001): Hub Cap Assy. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · Dec 10, 2024
- [8850-4CJ](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158105069320240625133918.0001): MOTOR (24 VDC). McFarlane Aviation Inc. · PMA PQ3732CE · Replaces 8850-4 · Mar 14, 2024
- [110SS](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169832363120240221142904.0001): Drain Valve Assembly. Saf-Air Products Inc · PMA PQ2036CE · Replaces CAV-110 · Jan 30, 2024
- [110HS](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107207908920240221142907.0001): Drain Valve Assembly. Saf-Air Products Inc · PMA PQ2036CE · Replaces CAV-110H-4 · Jan 30, 2024
- [MDL103216-000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148124030220240221143426.0001): SkyView HDX Instrumentation. Dynon Avionics, Inc. · PMA PQ05359NM · Modification part · Jan 26, 2024
- [FS2-20](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129725693320250925194345.0001): Alternator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces BC410-1 · Dec 6, 2023
- [UAV-1004236-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104337454220230707211342.0001): AV-30-C. uAvionix Corporation · PMA PQ05445NM · Modification part · Jun 28, 2023
- [EA-26000-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189329754620230105195519.0001): EA-26000 Series EIS Back-up Battery System Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jan 3, 2023
- [EA-26000-24](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139497566720230105195539.0001): EA-26000 Series EIS Back-up Battery System Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jan 3, 2023
- [4110-200-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130019255720230621172220.0001): Cylinder. Aerox Aviation Oxygen Systems · PMA PQ4373CE · Replaces 21507-031270152-3176700-77 · Dec 1, 2022
- [4110-200-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102141098620230621172221.0001): Cylinder. Aerox Aviation Oxygen Systems · PMA PQ4373CE · Replaces 21507-041270152-4176700-115 · Dec 1, 2022
- [8000-177](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152582727220240229155223.0001): PMA Link Sensor. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8000-177 · Nov 18, 2022
- [8000-175](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135545732520240229155222.0001): VizionPMA Flat. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8000-175 · Nov 18, 2022
- [8100-064](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122380228320240229155224.0001): 60 in-lb. PMA Servo 12V. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8100-064 · Nov 18, 2022
- [AAG5-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182309264920220811111803.0001): G5 Adapter Plate. Affordable Aviation LLC · PMA PQ05456NM · Replaces Garmin 115-02733-00 · Aug 2, 2022
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118349605520220706160152.0001): Whelen Aerospace Technologies · PMA PQ1372CE · Jun 21, 2022
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185927358020220720120314.0001): C J Aviation, Inc. · PMA PQ1607CE · Jun 17, 2022
- [EA-22000T](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136217125220220525194511.0001): Controller Wire Harness- Twin (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-22000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131569650020220525194358.0001): Controller Wire Harness (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-21000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107789028420220525194236.0001): Six-Cylinder Ignition Controller. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [89000020-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186647569520240229155257.0001): Final Assembly KSD 100 Primary Flight Display (PFD). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000023-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182434160220240229155303.0001): Final Assembly KG 71 Air Data Attitude and Heading Reference System (ADHRS). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000026-003](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177094890620240229155313.0001): Final Assembly KCP 100 Control Panel(Landscape). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000026-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118953589220240229155308.0001): Final Assembly KCP 100 Control Panel. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [EA-23000-A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID652785049020210923143725.0001): EA-23000 Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jul 28, 2021
- [EA-23000-A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID405491937720210923143826.0001): EA-23000 Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jul 28, 2021
- [700-00190-100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID364727301920210921142557.0001): SkyTrax 100B/200 ADS-B Receiver. Avidyne Corporation · PMA PQ4035CE · Replaces ModificationPart · Jul 28, 2021
- [MC660226-023](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID775499530202107231445280.0001): Control, RPM. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 660226-023 · Apr 9, 2021
- [MC660226-005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID708026138120210723144523.0001): Control, Mixture. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 660226-005, 660226-5 · Apr 9, 2021
- [MC660226-025](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID432612317120210723144528.0001): Control, Mixture. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 660226-025 · Apr 9, 2021
- [MCVA660226-027](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID319247314820210723144533.0001): Control, Throttle. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 660226-027 · Apr 9, 2021
- [MC660226-027](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164830861820210723144529.0001): Control, Throttle. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 660226-027 · Apr 9, 2021
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID881714192720210702175232.0001): Aspen Avionics · PMA PQ03868SW · Jan 20, 2021
- [1049-4000-03-001C](https://drs.faa.gov/browse/excelExternalWindow/FB6A4D62429A217F86258633006145AB.0001): Roll Steering Converter. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020

All of them: https://openairdocs.org/model/mooney-international-m20r/pma.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Mooney M20R](https://openairdocs.org/model/mooney-m20r): 399 registered aircraft, registry code 5870225

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.