# N300ME: Mooney M20R

- Status: Valid registration
- Airframe: [Mooney M20R](https://openairdocs.org/model/mooney-m20r) (registry code 5870225, 2 seats)
- Data sheets: [TCDS 2A3](https://openairdocs.org/tcds/2A3) (Mooney International Corporation) (OpenAirDocs)
- Serial number: 29-0479
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Certificate issued: March 16, 2024
- Expires: March 31, 2031
- Mode S code: A3206A
- Registered owner: [Sjk Aviation LLC](https://openairdocs.org/faa-owner/SJK%20AVIATION%20LLC)
- Location: [Orland Park, IL](https://openairdocs.org/faa-place/IL/Orland%20Park)
- Owner type: LLC
- Owner's area on the map: 41.5974° N, 87.8867° W: Placed by OpenAirDocs at the center of ZIP code 60467, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=300ME
- Page: https://openairdocs.org/aircraft/N300ME

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 16 in force

### Matched by airframe (Mooney M20R)

- [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 in force)

- [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

## NTSB investigations

None matched to N300ME.

## NTSB investigations on N300ME not matched to an aircraft (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB NYC99LA050](https://openairdocs.org/ntsb/NYC99LA050), Jan 15, 1999: Douglas DC-9 (N300ME), Plainfield, PA, no damage. Probable cause: The wake turbulence from the proceeding Boeing 747.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20080530846669I](https://openairdocs.org/incident/20080530846669I), May 30, 2008: Mooney M20R (N300ME), Wurtsboro, NY, Minor damage. (-23) Short field approach with airspeed 15 to 20 knots higher than recommended. On third landing attempt aircraft porpoised and bounced prior to pilot…

## Reports on N300ME not matched to an aircraft (5)

They name N300ME, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20010427012479I](https://openairdocs.org/incident/20010427012479I), Apr 27, 2001: Doug DC915 (N300ME), Kansas City, MO. (-23)On April 27, 2001, midwest express airline (mwea), flight MEP793, a DC-9, was enroute from atl to mci and declared an emergency due to a shut down of…
- [Accident 19990115041929A](https://openairdocs.org/incident/19990115041929A), Jan 15, 1999: Doug DC915 (N300ME), Plainfield, PA. (.4)The DC-9 departed and climbed to flight level 290. About 1 hour and 35 minutes after departure, the airplane was cleared by ATC to 17,000 feet MSL. Upon…
- [Incident 19951122041909I](https://openairdocs.org/incident/19951122041909I), Nov 22, 1995: Doug DC915 (N300ME), Omaha, NE. Narrative: on November 22, 1995, N300ME, a DC-9-10, operated by midwest express airlines, inc., departed Eppley Airfield, Omaha, NE enroute to Washington DC as…
- [Incident 19930102002129I](https://openairdocs.org/incident/19930102002129I), Jan 2, 1993: Doug DC915 (N300ME), Denver, CO, Minor damage. Heard a loud bang on takeoff. Closed throttle. Returned. Landed safely. Found reverse section missing.
- [Incident 19860121008889I](https://openairdocs.org/incident/19860121008889I), Jan 21, 1986: Doug DC915 (N300ME), Milwaukee, WI. Takeoff was aborted due to engine power loss. Fuel control shaft found sheared. Right brake locked after abort.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N300ME not matched to an aircraft (189, newest 50)

They name N300ME, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR MWEA030210](https://openairdocs.org/sdr/MWEA030210), May 13, 2003: PRESSURE SWITCH. INOPERATIVE. COULD NOT GET ELEVATOR POWER ON LIGHT TO COME ON. REMOVED AND REPLACED ELEVATOR PRESSURE SWITCH, AND REPAIRED BROKEN WIRES.
- [SDR MWEA030178](https://openairdocs.org/sdr/MWEA030178), Apr 16, 2003: PRESSURE SWITCH. OUT OF ADJUST. ELEVATOR POWER ON ANNUNCIATOR DOES NOT ILLUMINATE WITH M-FUNCTION. INSPECTED SWITCH & PERFORMED ADJUSTMENT TEST OF ELEVATOR POWER CONTROL PRESSURE SWITCH NO DEF
- [SDR MWEA030172](https://openairdocs.org/sdr/MWEA030172), Apr 15, 2003: DOUBLER. DENTED. LEFT FLAP FOUND DENT 1 X .068 INCH DEEP AT STATION XRS 320. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA030175](https://openairdocs.org/sdr/MWEA030175), Apr 14, 2003: SWITCH. OUT OF ADJUST. ELEVATOR POWER ON ANNUNCIATOR DOES NOT ILLUMINATE ON ELEVATOR POWER CHECK. INSPECTED SWITCH AND PERFORMED ADJUSTMENT TEST. NO DEFECTS NOTED, TEST GOOD.
- [SDR MWEA030170](https://openairdocs.org/sdr/MWEA030170), Apr 14, 2003: PANEL. DENTED. RIGHT CENTER SPOILER PANEL HAS DENT 1.5 X .033 INCH DEEP AND DELAMINATED. ROUT OUT DAMAGE BONDED EXISTING DOUBLER.
- [SDR MWEA030167](https://openairdocs.org/sdr/MWEA030167), Apr 14, 2003: PANEL. DENTED. RIGHT CENTER SPOILER PANEL HAS A DENT 2.5 X .052 INCH DEEP AND DELAMINATED. ROUT OUT DAMAGE AND BOND EXISTING DOUBLER.
- [SDR MWEA030173](https://openairdocs.org/sdr/MWEA030173), Apr 14, 2003: STRUCTURE. DENTED. LEFT AILERON TAB HAS A DENT LOCATED AFT OF THE THIRD HINGE OUTBOARD TRAILING EDGE DENT 2 X .080 INCH DEEP. REPAIRED AND BALANCED AILERON CONTROL TAB.
- [SDR MWEA030171](https://openairdocs.org/sdr/MWEA030171), Apr 14, 2003: SKIN. DENTED. RIGHT CENTER SPOILER PANEL HAS DENT 1.75 X .037 INCH DEEP AND DELAMINATED. ROUT OUT DAMAGE AND BOND DOUBLER.
- [SDR MWEA030169](https://openairdocs.org/sdr/MWEA030169), Apr 14, 2003: SKIN. DENTED. LEFT WING INBOARD FLIGHT SPOILER HAS DENT 2.375 X .059 INCH DEEP. CUT OUT DAMAGE, HOT BOND DOUBLER.
- [SDR MWEA030168](https://openairdocs.org/sdr/MWEA030168), Apr 14, 2003: SKIN. DENTED. LEFT WING GROUND SPOILER HAS A DENT 2 X .058 INCH DEEP. CUT OUT DAMAGE, HOT BOND ON REPAIR DOUBLER.
- [SDR MWEA020768](https://openairdocs.org/sdr/MWEA020768), Dec 31, 2002: DOUBLER. PUNCTURED. THERE IS A PUNCTURE IN THE SUBFLOORING JUST AFT OF STATION 160 AT RIGHT SIDE OF CENTERLINE OF FUSELAGE. -- REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLE
- [SDR MWEA020767](https://openairdocs.org/sdr/MWEA020767), Dec 27, 2002: DOUBLER. CRACKED. FORWARD FACE OF THE AFT PRESSURE BULKHEAD AT THE SEVEN O'CLOCK POSTION DOOR JAMB PIN HOLDER IS CRACKED. -- FABRICATED AND INSTALLED FINGER DOUBLER AND DOUBLER.
- [SDR MWEA020766](https://openairdocs.org/sdr/MWEA020766), Dec 27, 2002: DOUBLER. CRACKED. FORWARD FACE OF THE AFT PRESSURE BULKHEAD AT THE FIVE O'CLOCK POSITION PLUG DOOR JAMB PIN HOLDER IS CRACKED. -- FABRICATED AND INSTALLED FINGER DOUBLER AND REPA
- [SDR MWEA020765](https://openairdocs.org/sdr/MWEA020765), Dec 27, 2002: NUT PLATE. CORRODED. PRESSURE SLANT PANEL CORRODED AROUND LOWER NUT PLATES ON LEFT SIDE FROM APPROXIMATELY 22 INCHES TO 44 INCHES FROM CENTERLINE. -- FABRICATED AND INSTALLED NEW SL
- [SDR MWEA020751](https://openairdocs.org/sdr/MWEA020751), Dec 26, 2002: STIFFENER. CRACKED. STIFFENER AT AFT PRESSURE BULKHEAD AFT SIDE RADIAL 20 RIGHT. -- FABRICATED AND INSTALLED STIFFENER.
- [SDR MWEA020750](https://openairdocs.org/sdr/MWEA020750), Dec 26, 2002: DOUBLER. CRACKED. FORWARD CARGO DOOR OUTER PAN RADIUS IS CRACKED INBOARD OF LOWER FORWARD DOOR STOP PAD. -- FABRICATED, DRILLED AND INSTALLED DOUBLER.
- [SDR MWEA020749](https://openairdocs.org/sdr/MWEA020749), Dec 26, 2002: STIFFENER. CRACKED. STIFFENER AT AFT PRESSURE BULKHEAD AFT SIDE RADIAL 20 LEFT IS CRACKED. -- FABRICATED AND INSTALLED STIFFENER.
- [SDR MWEA020746](https://openairdocs.org/sdr/MWEA020746), Dec 20, 2002: STIFFENER. CORRODED. SIX EACH STIFFENERS CORRODED ON LEFT PRESSURE PANEL. -- FABRICATED AND INSTALLED STIFFENERS.
- [SDR MWEA020739](https://openairdocs.org/sdr/MWEA020739), Dec 18, 2002: INTERCOSTAL. CRACKED. FORWARD CARGO DOOR, INTERCOSTAL IS CRACKED BETWEEN BEAM #5 AND UPPER DOOR PAN. -- LOCATED AND DRILLED AND INSTALLED NEW INTERCOSTAL.
- [SDR MWEA020731](https://openairdocs.org/sdr/MWEA020731), Dec 16, 2002: DOUBLER. CORRODED. EXISTING REPAIR ON SUBFLOOR AT STATION 165 APPROXIMATELY 10 INCHES RIGHT SIDE FROM CENTERLINE HAS SEVERAL FASTENERS PULLING THROUGH FLOOR WEB.
- [SDR MWEA020730](https://openairdocs.org/sdr/MWEA020730), Dec 16, 2002: DOUBLER. CORRODED. CORROSION IN SUBFLOOR AT APPROXIMATELY STATION 170 ABOUT 20 INCHES RIGHT OF FUSELAGE CENTERLINE. -- REMOVED CORROSION FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA020729](https://openairdocs.org/sdr/MWEA020729), Dec 16, 2002: DOUBLER. CORRODED. CORROSION THROUGH SUBFLOORING JUST AFT OF STATION 160 AT LEFT SIDE OF FUSELAGE CENTERLINE.. -- REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA011469](https://openairdocs.org/sdr/MWEA011469), Dec 4, 2001: ANGLE. CRACKED. RIGHT WING - FORWARD LOWER WING TO FUSELAGE ATTACH ANGLE UPPER FLANGE IS CRACKED BETWEEN LONGERON 22 AND 23 RIGHT -- REMOVED CRACKED ANGLE. LOCATED AND INSTALLE
- [SDR MWEA011468](https://openairdocs.org/sdr/MWEA011468), Dec 4, 2001: CHANNEL. CORRODED. FLOOR SUPPORT CHANNEL CORRODED ON UNDER SIDE AT 3 MOST INBOARD FASTENER HOLES AND INBOARD END AT STATION 200 AND OUTBOARD OF SEAT TRACK, #4 -- REMOVED, FABRICAT
- [SDR MWEA011467](https://openairdocs.org/sdr/MWEA011467), Dec 3, 2001: AILERON. DAMAGED. REMOVED STATIC WICK AND DOUBLER TO FACILITATE OTHER MAINTENANCE FROM THE LEFT HAND AILERON AT APPROXIMATELY STATION XA471. FABRICATED AND INSTALLED DOUBLER REPA
- [SDR MWEA011466](https://openairdocs.org/sdr/MWEA011466), Dec 3, 2001: SKIN. CORRODED. LEFT HAND AILERON HAS CORROSION ALONG LOWER SKIN AT TRAILING EDGE AT APPROXIMATELY STATION XA471. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR.
- [SDR MWEA011463](https://openairdocs.org/sdr/MWEA011463), Nov 30, 2001: SKIN. CRACKED. EXTERIOR SKIN IS CRACKED AT STATION 818, LONGERON 19 RIGHT, BETWEEN EXISTING DOUBLER AND SKIN BUTT SPLICE -- REMOVED, STOP DRILLED AND INSTALLED REPAIR.
- [SDR MWEA011464](https://openairdocs.org/sdr/MWEA011464), Nov 30, 2001: SKIN. CRACKED. EXTERIOR SKIN IS CRACKED AT STATION 815 LONGERON 17 RIGHT -- CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR.
- [SDR MWEA011461](https://openairdocs.org/sdr/MWEA011461), Nov 28, 2001: BEAM. CRACKED. GALLEY SERVICE DOOR BEAM #1 HAS A CRACK ON AFT END -- STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA011447](https://openairdocs.org/sdr/MWEA011447), Nov 26, 2001: FRAME. MISDRILLED. FRAME (FORMER) AT FUSELAGE STATION 377.5 AND BETWEEN LONGERON 30 AND LONGERON 28 RIGHT MISDRILLED -- REMOVED INTERCOSTAL. FABRICATED AND INSTALLED STACKED ANGLE
- [SDR MWEA011458](https://openairdocs.org/sdr/MWEA011458), Nov 26, 2001: INTERCOSTAL. ELONGATED. INTERCOSTAL FROM STATION 370-377.5, LONGERON 29 RIGHT HAS DOUBLE-DRILLED HOLE AT STATION 377.5 -- REMOVED, FABRICATED AND INSTALLED "T" FITTING AND INTERCOSTAL.
- [SDR MWEA011457](https://openairdocs.org/sdr/MWEA011457), Nov 26, 2001: SKIN. CORRODED. SKIN CORRODED AT SHEAR TIE BETWEEN LONGERON 30 AND LONGERON 29 RIGHT AT FUSELAGE STATION 370 -- FABRICATED AND INSTALLED REPAIR DOUBLERS: INTERNAL FINGER DOUBLE
- [SDR MWEA011456](https://openairdocs.org/sdr/MWEA011456), Nov 26, 2001: BEAM. CRACKED. MAIN CABIN DOOR BEAM NUMBER 7 HAS A CRACK ON AFT END -- STOP DRILLED CRACK. DRILLED UP NEW -53 DOUBLER. INSTALLED DOUBLER, FITTING AND DOOR STOP.
- [SDR MWEA011455](https://openairdocs.org/sdr/MWEA011455), Nov 20, 2001: STIFFENER. CRACKED. LEFT HAND INBOARD FLAP STIFFENER P/N 9958001-39 IS CRACKED. REMOVED, FABRICATED AND INSTALLED NEW STIFFENER.
- [SDR MWEA011454](https://openairdocs.org/sdr/MWEA011454), Nov 20, 2001: FORMER. ELONGATED. PASSENGER DOOR INTERCOSTAL (FORMER) HAS ELONGATED ON END NEAR HOOK ACTUATOR CRANK -- LOCATED AND DRILLED HOLES IN NEW FORMER. INSTALLED INTERCOSTAL.
- [SDR MWEA011448](https://openairdocs.org/sdr/MWEA011448), Nov 20, 2001: STIFFENER. CRACKED. POSSIBLE CRACK INDICATION ON AFT PRESSURE BULKHEAD TEE JUST ABOVE LONGERON 18 RIGHT REQUIRES CHEMICAL REMOVAL OF PRIMES FOR FURTHER EVALUATION. REMOVED, FIT, DR
- [SDR MWEA011446](https://openairdocs.org/sdr/MWEA011446), Nov 20, 2001: WEB. MISDRILLED. FORWARD CARGO DOOR JAMB WEB (GUSSET) MISDRILLED 2 PLACES AT FUSELAGE STATION 377.5 AND LONGERON 29 RIGHT -- REMOVED, FABRICATED AND INSTALLED WEB REPAIR.
- [SDR MWEA011445](https://openairdocs.org/sdr/MWEA011445), Nov 20, 2001: LONGERON. CORRODED. MODERATE CORROSION IN LONGERON CHANNEL 29 LEFT FROM 313 TO 332 -- FABRICATED AND INSTALLED REPAIR FITTING ON LONGERON 29 LEFT AT STATION 313-332.
- [SDR MWEA011443](https://openairdocs.org/sdr/MWEA011443), Nov 20, 2001: SHEAR TIE. CORRODED. SHEAR TIE AT FUSELAGE STATION 377.5, BETWEEN LONGERON 29 RIGHT AND LONGERON 29 LEFT IS CORRODED -- REMOVED, FABRICATED AND INSTALLED SHEAR TIE.
- [SDR MWEA011442](https://openairdocs.org/sdr/MWEA011442), Nov 20, 2001: SHEAR TIE. CORRODED. SHEAR TIE AT FUSELAGE STATION 370 BETWEEN LONGERON 30 AND LONGERPM 29 RIGHT IS CORRODED -- REMOVED, FABRICATED AND INSTALLED SHEAR TIE.
- [SDR MWEA011453](https://openairdocs.org/sdr/MWEA011453), Nov 20, 2001: FITTING. CRACKED. LEFT HAND INBOARD FLAP FITTING IS CRACKED AND BENT. REMOVED, LOCATED, DRILLED AND INSTALLED LEFT HAND INBOARD FLAP FITTING.
- [SDR MWEA011451](https://openairdocs.org/sdr/MWEA011451), Nov 20, 2001: BEAM. CRACKED. MAIN CABIN DOOR BEAM NUMBER 5 IS CRACKED ON FORWARD END -- LOCATED, DRILLED AND INSTALLED NEW DOOR BEAM.
- [SDR MWEA011449](https://openairdocs.org/sdr/MWEA011449), Nov 20, 2001: BEAM. CRACKED. MAIN CABIN DOOR BEAM NUMBER 8 HAS A CRACK ON FORWARD END -- REMOVED, DRILLED AND INSTALLED NEW BEAM.
- [SDR MWEA011444](https://openairdocs.org/sdr/MWEA011444), Nov 20, 2001: PAN. CORRODED. FORWARD CARGO DOOR JAMB ENTIRE BOTTOM PAN FACE HAS LIGHT TO MODERATE CORROSION -- REMOVED LOWER SECTION OF CARGO DOOR PAN. TRIMMED, LOCATED, DRILLED AND INSTALL
- [SDR MWEA011441](https://openairdocs.org/sdr/MWEA011441), Nov 20, 2001: SEAT TRACK. CORRODED. SEAT TRACK 4 BETWEEN STATION 200 AND 218 IS CORRODED AT FORWARD END AND AROUND FASTENER HOLES ON UPPER SURFACE AND LOWER SURFACE REMOVED, FABRICATED AND INSTALL
- [SDR MWEA011452](https://openairdocs.org/sdr/MWEA011452), Nov 20, 2001: LONGERON. CRACKED. FUSELAGE STATION 925 CRACKED AT LONGERON 16 LEFT -- STOP DRILLED CRACK. DRILLED ANGLES AND FRAME AND INSTALLED REPAIR ANGLES.
- [SDR MWEA011439](https://openairdocs.org/sdr/MWEA011439), Nov 15, 2001: SUPPORT FITTING. CRACKED. AREA OVER CENTER WING LATERAL FLOOR SUPPORT BEAM ATTACH ANGLE IS CRACKED AT STATION 566 XCW 40 LEFT -- REMOVED FLOOR SUPPORT FITTING AND INSTALLED REPAIR ANGLE.
- [SDR MWEA011438](https://openairdocs.org/sdr/MWEA011438), Nov 15, 2001: LONGERON. CRACKED. LEFT LAV HAS A CRACKED LONGERON AT FUSELAGE STATION 786 AND LONGERON 17 LEFT -- INSTALLED LONGERON REPAIR SPLICE SECTION.
- [SDR MWEA011437](https://openairdocs.org/sdr/MWEA011437), Nov 15, 2001: LONGERON. CRACKED. RIGHT LAV HAS A CRACKED LONGERON AT FUSELAGE STATION 786 LONGERON 17 LEFT -- REMOVED DAMAGED SECTION OF LONGERON AND INSTALLED LONGERON REPAIR SPLICE.
- [SDR MWEA011435](https://openairdocs.org/sdr/MWEA011435), Nov 15, 2001: INTERCOSTAL. CRACKED. INTERCOSTAL BETWEEN FUSELAGE STATION 880 & 859 CRACKED AT RADIUS NEXT TO 859 ABOVE LONGERON 16 RIGHT -- INSTALLED REPAIR ANGLES.

All 189: https://openairdocs.org/aircraft/N300ME/unmatched-reports.md

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

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Mooney M20R)

- [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/aircraft/N300ME/stcs.md

## Related

- Other Mooney M20R aircraft: https://openairdocs.org/model/mooney-m20r/aircraft.md

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