# N2823W: 1981 Mooney M20J

- Status: Valid registration
- Airframe: [Mooney M20J](https://openairdocs.org/model/mooney-m20j) (registry code 5870219, 4 seats)
- Engine: [Lycoming I0360 SER A&C](https://openairdocs.org/engine/lycoming-i0360-ser-a-c) (registry code 41511)
- Data sheets: [TCDS 2A3](https://openairdocs.org/tcds/2A3) (Mooney International Corporation) (OpenAirDocs)
- Serial number: 24-1101
- Year built: 1981
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: April 27, 1981
- Certificate issued: August 4, 2021
- Expires: August 31, 2028
- Mode S code: A2D83F
- Registered owner: [Smith Scot](https://openairdocs.org/faa-owner/SMITH%20SCOT)
- Location: [Fayetteville, NC](https://openairdocs.org/faa-place/NC/Fayetteville)
- Owner type: Individual
- Owner's area on the map: 34.9585° N, 78.8968° W: Placed by OpenAirDocs at the center of ZIP code 28306, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=2823W
- Page: https://openairdocs.org/aircraft/N2823W

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): 32 in force

### Matched by airframe (Mooney M20J)

- [AD 2024-14-03](https://openairdocs.org/ad/2024-14-03): Autopilot System · Garmin GFC 500 Autopilot (STC SA01866WI). Effective Aug 20, 2024
- [AD 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023
- [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 2012-05-09](https://openairdocs.org/ad/2012-05-09): Stabilizers · Mooney M20B, M20C, M20D and 10 more. Effective Mar 20, 2012
- [AD 2006-03-08](https://openairdocs.org/ad/2006-03-08): Vacuum pumps · Aero Advantage 14-19, 14-19-2, 14-19-3 and 299 more. Effective Mar 10, 2006
- [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 2004-25-04](https://openairdocs.org/ad/2004-25-04): O & N Bladder Fuel Cell · Mooney M20B, M20C, M20D and 4 more. Effective Jan 21, 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 98-21-21 R1](https://openairdocs.org/ad/98-21-21-R1): Electric Inflatable Door Seals · Cessna 17-30, 17-30A, 17-31 and 267 more. Effective May 1, 2000
- [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 97-26-08](https://openairdocs.org/ad/97-26-08): Fuel Filler Cap Assembly · Mooney M20F, M20J and M20L. Effective Jan 20, 1998
- [AD 95-26-16 R1](https://openairdocs.org/ad/95-26-16-R1): Alternate Air Door Assembly · Mooney M20J. Effective May 16, 1996
- [AD 92-08-15](https://openairdocs.org/ad/92-08-15): Rudder Static Balance · Mooney M20J. Effective Jun 30, 1992
- [AD 88-25-11](https://openairdocs.org/ad/88-25-11): Baggage Door Mechanism · Mooney M20J and M20K. Effective Jan 5, 1989
- [AD 85-25-02](https://openairdocs.org/ad/85-25-02): Autopilot Systems · King Radio Autopilot Systems, M20J, M20K and 1 more. Effective Jan 27, 1986
- [AD 85-23-07](https://openairdocs.org/ad/85-23-07): Autopilot Systems · Aerostar PA-60-700P (Aerostar 700P), 172L, 172P and 37 more. Effective Jan 27, 1986
- [AD 85-24-03](https://openairdocs.org/ad/85-24-03): Fuel Tank Bays and Rib Station Inspection · Mooney M20B, M20C, M20D and 6 more. Effective Jan 6, 1986
- [AD 80-25-07 R1](https://openairdocs.org/ad/80-25-07-R1): Oil Coolers · American Champion 7ECA, 7GCAA, 7GCBC and 39 more. Effective Sep 24, 1981
- [AD 81-19-04](https://openairdocs.org/ad/81-19-04): Hose Assembly · Rajay Hose Assemblies, 500A, 500B and 87 more. Effective Sep 17, 1981
- [AD 80-17-03](https://openairdocs.org/ad/80-17-03): Oil Pressure Fittings · Mooney M20J. Effective Aug 18, 1980
- [AD 80-17-04](https://openairdocs.org/ad/80-17-04): Fuel Flow Transducers · Aerosonic Fuel Flow Transducers, PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601) and 9 more. Effective Aug 13, 1980
- [AD 80-13-03](https://openairdocs.org/ad/80-13-03): Fuel Pumps · Mooney M20E, M20F and M20J. Effective Jun 20, 1980
- [AD 79-06-04](https://openairdocs.org/ad/79-06-04): Elevator Control Lock · Mooney M20F and M20J. Effective Mar 26, 1979
- [AD 78-17-01](https://openairdocs.org/ad/78-17-01): Emergency Locator Transmitter · Mooney M20C, M20F and M20J. Effective Aug 21, 1978
- [AD 78-15-02](https://openairdocs.org/ad/78-15-02): MLG Side Brace Bolts · Mooney M20F and M20J. Effective Aug 1, 1978
- [AD 77-18-01](https://openairdocs.org/ad/77-18-01): Engine Oil Cooler · Mooney M20E, M20F and M20J. Effective Aug 31, 1977
- [AD 77-08-06](https://openairdocs.org/ad/77-08-06): Engine Oil · Mooney M20E, M20F and M20J. Effective Jul 8, 1977
- [AD 77-06-01](https://openairdocs.org/ad/77-06-01): Instrument Conditions · Mooney M20J. Effective Mar 18, 1977
- [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

### Matched by engine (Lycoming I0360 SER A&C)

None in force.

## Information bulletins (advisory) (4 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 CE-09-38](https://openairdocs.org/saib/CE-09-38): Wings: Installation of Supplemental Type Certificate (STC) Wing Tip Fairings. Issued Jul 7, 2009

## NTSB investigations

None matched to N2823W.

## FAA accident and incident reports

None matched to N2823W.

## Reports on N2823W not matched to an aircraft (3)

They name N2823W, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19860514036289I](https://openairdocs.org/incident/19860514036289I), May 14, 1986: Boeing 727247 (N2823W), Amarillo, TX. Encountered severe turbulence en route with passenger and flight attendant injury.
- [Incident 19800816066939I](https://openairdocs.org/incident/19800816066939I), Aug 16, 1980: Boeing 727 (N2823W), San Francisco, CA, Minor damage. After takeoff, flaps would not retract properly.
- [Incident 19790425025079I](https://openairdocs.org/incident/19790425025079I), Apr 25, 1979: Boeing 727 (N2823W), Denver, CO, Minor damage. Severe vibration at rotation accompanied by engine failure.a main tire had blown. Parts ingested. Flight returned.

## 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 N2823W not matched to an aircraft (81, newest 50)

They name N2823W, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DL72E954307](https://openairdocs.org/sdr/DL72E954307), Nov 8, 1995: ANTENNA. FAILED. WX RADAR SPOKES AND DISPLAYS TEST PATTERN WHILE IN NORM AND CONTOUR. REPLACED RADAR ANTENNA AND WAVE GUIDE, OPERATION NORMAL.
- [SDR DL72E953906](https://openairdocs.org/sdr/DL72E953906), Oct 3, 1995: ANGLE. CRACKED. DURING A-1 LETTER CHECK, FOUND 2 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE AT O/B STOP PAD. REPAIRED PER M/M 57-54-0.
- [SDR DL72E953905](https://openairdocs.org/sdr/DL72E953905), Oct 3, 1995: ANGLE. CRACKED. DURING A-1 LETTER CHECK, FOUND .25 INCH CRACK NR 7 L/E SLAT COVE SKIN ATTACH ANGLE AT I/B STOP PAD. REPAIRED PER M/M 57-54-0.
- [SDR DL72E951580](https://openairdocs.org/sdr/DL72E951580), Mar 22, 1995: STRINGER. CORRODED. DURING HMV, CORROSION WAS FOUND FROM STA 950F TO 1007, STR 29L AROUND FASTENER LOCATIONS ON THE UPPER SURFACE OF THE O/B SKIN ATTACH FLANGE. REPAIRED PER DL ERA
- [SDR DL72E951207](https://openairdocs.org/sdr/DL72E951207), Mar 21, 1995: STRINGER. CORRODED. AT HMV, FOUND STRINGER 25 CORRODED AT FS 1148. REMOVED DAMAGED SECTION REPAIRED PER SRM53-10-3 FIG 1.
- [SDR DL72E951193](https://openairdocs.org/sdr/DL72E951193), Mar 17, 1995: ANGLE. CORRODED. DURING HMV, THE FLOOR SUPPORT ANGLES AT STA 1166 WERE FOUND TO BE CORRODED. THESE WERE REPAIRED PER SRM 53-10-3 FIG 10.
- [SDR DL72E951192](https://openairdocs.org/sdr/DL72E951192), Mar 17, 1995: ANGLES. CORRODED. AT HMV THE FLOOR SUPPORT ANGLES AT STA 1166 WERE FOUND TO BE CORRODED. THE ANGLES WERE REPAIRED PER SRM 53-10-5 FIG 10.
- [SDR DL72E951174](https://openairdocs.org/sdr/DL72E951174), Mar 17, 1995: FRAME. CRACKED. AT HMV, FOUND FUSELAGE FS 580 FRAME CRACKED AT STR 25L. CRACK IS IN DOUBLER ON TOP OF FRAME UPPER FLANGE. REPAIRED PER SRM 53-10-4 PG 106.
- [SDR DL72E951103](https://openairdocs.org/sdr/DL72E951103), Mar 15, 1995: FLAP. WORN. AT HMV SHOP INSPECTION NR 4 FOREFLAP WAS FOUND WITH WEAR DAMAGE TO L/E SKIN AT 54 INCHES FROM THE O/B END OF FLAP. REPAIRED PER SRM 57-50-4.
- [SDR DL72E951129](https://openairdocs.org/sdr/DL72E951129), Mar 14, 1995: SEAT TRACK. DAMAGED. SEAT TRACK RT I/B HAS TOOLING DAMAGE ON O/B FLANGE STA 800. REPAIRED PER SRM 53-10-5 PG27. FOUND AT HMV.
- [SDR DL72E951206](https://openairdocs.org/sdr/DL72E951206), Mar 11, 1995: STRINGER. CORRODED. STRINGER 27R CORRODED INSIDE STRINGER STA 740 AFT OF SPLICE STRINGER SLICE PER SRM 53-10-3 PG 3. FOUND AT HMV.
- [SDR DL72E951205](https://openairdocs.org/sdr/DL72E951205), Mar 11, 1995: SUPPORT. CORRODED. AT HMV, FOUND LOWER FUSELAGE SKIN SUPPORT ANGLE AT FS 720 WITH CORROSION DAMAGE. REPLACED ANGLE PER MM 53-11-10 PG 858 TO 859.
- [SDR DL72E951131](https://openairdocs.org/sdr/DL72E951131), Mar 11, 1995: SEAT TRACKS. CORRODED. RT I/B AND RT O/B SEAT TRACKS CORRODED STA 1010-1050. REPAIRED PER MM 53-20-11 FIG 804. FOUND AT HMV.
- [SDR DL72E951130](https://openairdocs.org/sdr/DL72E951130), Mar 11, 1995: STRINGER. CORRODED. FWD B/B CORROSION ON STR 28L AT STA 700. REPAIRED PER SRM 53-10-3 FIG 1. FOUND AT HMV.
- [SDR DL72E951204](https://openairdocs.org/sdr/DL72E951204), Mar 10, 1995: STRINGER. CORRODED. AT HMV, FOUND STRINER 27R, CORRODED AT FS 740. REPAIRED PER SRM 53-10-3 FIG. 1.
- [SDR DL72E950994](https://openairdocs.org/sdr/DL72E950994), Mar 10, 1995: FLAP. WORN. LEADING EDGE WORN 52 INCHES FROM I/B END OF RT WING NR 3 AFT FLAP. REPAIRED PER SRM 575004 FIG 9.
- [SDR DL72E951173](https://openairdocs.org/sdr/DL72E951173), Mar 9, 1995: TEE. CORRODED. AT HMV, FOUND LOWER FUSELAGE STRUCTURE TEE ANGLE CORRODED AT FORWARD HINGE AREA OF PANEL 3448 AT FS 742. REPAIRED PER MM 53-30-1 FIG 804.
- [SDR DL72E951014](https://openairdocs.org/sdr/DL72E951014), Mar 9, 1995: LIGHT BOX. CRACKED. DURING HMV FOUND L/W L/E LIGHT BOX, STR 15L IS CRACKED ON FWD AND AFT SIDES OF LIGHT BOX, REPAIRED PER SRM 53-10-1 FIG 1.
- [SDR DL72E950914](https://openairdocs.org/sdr/DL72E950914), Mar 5, 1995: BONDNG WIRE HOLE. ELONGATED. DURING HMV, FOUND 727 O/B AILERON BONDING WIRE ATTACH HOLE ELONGATED. REPAIRED PER SRM 57-50-5.
- [SDR DL72E950913](https://openairdocs.org/sdr/DL72E950913), Mar 5, 1995: SKIN. PUNCTURE. DURING HMV, FOUND HOLE PUNCTURED IN LOWER SKIN, I/B END 727 O/B AILERON. REPAIRED PER SRM 57-50-5.
- [SDR DL72E951219](https://openairdocs.org/sdr/DL72E951219), Mar 4, 1995: STRINGER. CRACKED. DURING HMV, FOUND STRINGER CRACKED NR 29L CRACKED IN LOWER RADIUS FROM FS 990 - 1000. REPAIRED PER ERA 301274-14 REV B. FOUND AT HMV.
- [SDR DL72E951158](https://openairdocs.org/sdr/DL72E951158), Mar 3, 1995: FLOOR. CORRODED. STA 1167 FLOOR AT LBL 44 TO LBL 49 CORRODED. FOUND AT HMV. REPAIRED PER SRM 53-10-8 FIG 10.
- [SDR DL72E951110](https://openairdocs.org/sdr/DL72E951110), Mar 2, 1995: STRINGER. CRACKED. DURING HMV INSPECTION PER EO 4-59253-3AD, FOUR DIFFERENT VERTICAL STABILIZER STRINGERS WERE FOUND CRACKED. THE CRACK LOCATIONS ARE STR8L AT STA 180.6, STR 9L AT
- [SDR DL72E951176](https://openairdocs.org/sdr/DL72E951176), Mar 1, 1995: STRINGER. CORRODED. AT HMV, STRINGER 22L WAS FOUND CORRODED AT FS 1154 ON IB FLANGE AND A SPLICE BELOW LAV DUMP CHUTE. DAMAGED AREA WAS REMOVED AND NEW SECTION WAS MFG PER SRM 53-1
- [SDR DL72E951171](https://openairdocs.org/sdr/DL72E951171), Mar 1, 1995: ANGLE. CORROSION. ANGLE CORRODED FLOOR SUPPORT ANGLES CORRODED FROM FS 312 TO FS 344 LBL28. REPLACED SUPPORT AT FS 312 TO 328 AND CLEANED CORROSION PER SRM 51-10-6.
- [SDR DL72E951166](https://openairdocs.org/sdr/DL72E951166), Mar 1, 1995: BEAM. CORROSION. CORROSION FLOOR BEAM STA 1110, TOP OF BEAM ALL THE WAY ACROSS. REPAIRED AT RBL 18 TO RBL 33 PER SRM 53-10-8.
- [SDR DL72E951164](https://openairdocs.org/sdr/DL72E951164), Mar 1, 1995: SUPPORT. CORROSION. FLOOR SUPPORTS STA 1130 TO 1148 RBL12 AND SMALL CONNECTING STUB SUPPORT WERE FOUND CORRODED. CLEANED CORROSION PER SRM 51-10-6, WITHIN LIMITS 53-20-11 FIG 804, 
- [SDR DL72E951156](https://openairdocs.org/sdr/DL72E951156), Mar 1, 1995: CHORD. CORRODED. CHORD CORRDED, CORROSION ON CHORD OB OF RT KEEL BEAM EXTENSION FS950, FOUND AT HMV. REPAIRED PER SRM 53-10-9 FIG 11.
- [SDR DL72E951133](https://openairdocs.org/sdr/DL72E951133), Mar 1, 1995: SUPPORT. WORN. SUPPORT WORN AC DISTRIBUTION BAY BULKHEAD SUPPORT WORN AT UPPER ATTACH POINT, FS 720D ABOVE STR26L. REPAIRED PER SRM 53-10-9 FIG 8. FOUND AT HMV.
- [SDR DL72E951132](https://openairdocs.org/sdr/DL72E951132), Mar 1, 1995: BEAM. WORN. BEAM WORN C1 AFT BULKHEAD WALL SUPPORT BEAM AT STA 720D, BELOW RT I/B SEAT TRACK IS WORN AT WASHERS. REPAIRED PER SRM 53-10-9 FIG 8. FOUND AT HMV.
- [SDR DL72E951128](https://openairdocs.org/sdr/DL72E951128), Mar 1, 1995: FLOOR BEAM. CORRODED. FLOOR BEAM CORRODED AT FS 400 FROM LBL 12 TO RBL 12. SPLICED IN NEW SECTION OF BEAM PER SRM 53-10-8 FIG 3. FOUND AT HMV.
- [SDR DL72E951127](https://openairdocs.org/sdr/DL72E951127), Mar 1, 1995: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED AT STA 418 RBL 12 INCHES TO Z ANGLE AT AFT SIDE OF FWD SVC DOOR. REPAIRED PER MM 53-20-11 FIG 804. FOUND AT HMV.
- [SDR DL72E951126](https://openairdocs.org/sdr/DL72E951126), Mar 1, 1995: FLOOR BEAM. CORRODED. FLOOR BEAM CORRODED AT STA 42O, RBL 56 INCHES. O/B SEATTRACK RIGHT SIDE CORRODED SAME LOC AS ITEM 1. REPAIRED PER SRM 53-10-8 FIG 1. FOUND AT HMV.
- [SDR DL72E951070](https://openairdocs.org/sdr/DL72E951070), Mar 1, 1995: FLOOR BEAM. CORRODED. AT HMV, FOUND FS 380 CABIN FLOOR BEAM CORRODED AT RBL 60. REPAIRED PER SRM 53-10-8 FIG 1.
- [SDR DL72E951068](https://openairdocs.org/sdr/DL72E951068), Mar 1, 1995: SEAT TRACK. CORRODED. SEAT TRACK CORRODED STA 420 TO 380. REPLACED SECTION OF TRACK PER MM 53-20-11.
- [SDR DL72E951067](https://openairdocs.org/sdr/DL72E951067), Mar 1, 1995: SEAT TRACK. CORRODED. AT HMV, FOUND SEAT TRACK CORRODED AT FS 420 - 380 AT RBL 24 SPLICED IN SECTION FROM 400 TO 344 PER MM 53-20-11 FIG 802. SPLICED SEAT TRACK SECTION FROM 400-440 
- [SDR DL72E951013](https://openairdocs.org/sdr/DL72E951013), Mar 1, 1995: SEAT TRACK. WORN. DURING HMV FOUND LT SEAT TRACKS WORN AT SEVERAL SEAT LOCATIONS BETWEEN 950F AND 1138, REPAIRED BY REMOVING CORROSION PER SRM 51-10-6, TREATED AND PAINTED STA 95
- [SDR DL72E950917](https://openairdocs.org/sdr/DL72E950917), Mar 1, 1995: SKIN. CRACKED. AT HMV, FOUND FUSELAGE SKIN CRACKED AT FS 1052 OUTBOARD OF STRINGER 28L. REPAIRED PER SRM 53-30-3.
- [SDR DL72E951191](https://openairdocs.org/sdr/DL72E951191), Feb 28, 1995: WEB. CRACKED. AT HMV THE WEB INSIDE VERT STAB HAD 2 CRACKS IN RT LOWER CORNER AT STA 1303. STOP DRILLED CRACK AND REPAIRED PER SRM 53-10-4.
- [SDR DL72E951190](https://openairdocs.org/sdr/DL72E951190), Feb 28, 1995: WEB. CRACKED. AT HMV THE WEB INSIDE VERT STAB JUST ABOVE S-DUCT WAS CRACKED AT THE LT LOWER CORNER. STOP DRILLED THE CRACK AND FABRICATED REPAIR PER SRM 53-10-4. INSTALLED RE
- [SDR DL72E951155](https://openairdocs.org/sdr/DL72E951155), Feb 28, 1995: SKIN. CRACKED. SKIN BULGED AND CRACKED STA 1125 STR 27 RT. FOUND AT HMV. REPAIRED PER SRM 53-30-3 FIG.
- [SDR DL72E951122](https://openairdocs.org/sdr/DL72E951122), Feb 28, 1995: SKIN. STOP DRILLED. DURING HMV, FOUND VERTICAL STABILIZER EXTERIOR SKIN HAS A STOP DRILL ON RT SIDE 20 INCHES FWD OF REAR SPAR AT FUSELAGE, REPAIRED PER FABRICATING DOUBLER PER MM 
- [SDR DL72E951066](https://openairdocs.org/sdr/DL72E951066), Feb 28, 1995: DOUBLER. REQ REPLACEMENT. AT HMV FOUND TIME LIMITED REPAIR AT FS1060 BETWEEN STR 21 AND 22L. INSTALLED PERMANENT REPAIR PER SRM 53-30-3 FIG 1.
- [SDR DL72E951065](https://openairdocs.org/sdr/DL72E951065), Feb 28, 1995: STRINGER. CORROSION. AFT B/B CORROSION ON O/B SIDE OF STR 28L FS 1050-1070 NEAR JUNCTURE WITH FUS SKIN. FOUND AND REPAIRED AT HMV. REPAIRED PER SRM 53-10-3.
- [SDR DL72E950932](https://openairdocs.org/sdr/DL72E950932), Feb 28, 1995: SUPPORT. WORN. THE NR 2 FWD COWL MATING SUPPORT RING FOUND WORN AT HMV. INSTALLED SPLICES AND REPAIR ANGLE PER MM 53-11-0.
- [SDR DL72E950916](https://openairdocs.org/sdr/DL72E950916), Feb 28, 1995: SKIN. DAMAGED. DURING HMV, FOUND L/W OB AILERON HOLE NEXT TO WT AND BALANCE PLACARD ON I/B UNDERSIDE. REPAIRED PER SRM 57-50-5.
- [SDR DL72E950915](https://openairdocs.org/sdr/DL72E950915), Feb 28, 1995: BONDNG WIRE HOLE. ELONGATED. DURING HMV, FOUND O/B LT WG AILERON BONDING WIRE ATTACH HOLE IS ELONGATED AT O/B TAB CUTOUT AREA. RPAIRED PER SRM 57-50-5 FIG 3.
- [SDR DL72E950903](https://openairdocs.org/sdr/DL72E950903), Feb 28, 1995: FRAME. CRACKED. DURING HMV, FOUND FS 804.95 FRAME CRACKED, RT SIDE JUST BELOW WINDOW FRAME. REPAIRED PER SRM 53-10-4 FIG 22.
- [SDR DL72E950902](https://openairdocs.org/sdr/DL72E950902), Feb 28, 1995: UPLOCK SUPPORT. DAMAGED. AT HMV, LEFT MLG UPLOCK SUPPORT FRAME AT FS 913 WAS FOUND WITH TIME LIMITED REPAIR. INSTALLED PERMANENT REPAIR PER MM 53-11-0 PG 815.
- [SDR DL72E951212](https://openairdocs.org/sdr/DL72E951212), Feb 27, 1995: FRAME. CORRODED. AFT BB FRAME CORRODED, STA 1130 BETWEEN STR 28R AND 29R. REPAIRED PER 53-11-0 PAGE 825. FOUND AT HMV.

All 81: https://openairdocs.org/aircraft/N2823W/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (376, 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 M20J)

- [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 SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation
- [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 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 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 SA02871AT](https://openairdocs.org/stc/SA02871AT): Install Powerflow Systems, Inc., tuned exhaust system to enhance engine performance. Power Flow Systems 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 SA5788SW](https://openairdocs.org/stc/SA5788SW): Installation of ALCOR fuel flow/totalizer system 24606. Alcor LLC
- [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 SA1798GL](https://openairdocs.org/stc/SA1798GL): Installation of multi-sensor long range navigation system. M20J S/N 24-0326. Acron Aviation Inc
- [STC SA11888CH](https://openairdocs.org/stc/SA11888CH): Installation of Hartzell Propeller Model 2C1-R419A1/75C(S)08, 2 blade composite propeller. Hartzell Propeller LLC
- [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 SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels 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 SA02349LA](https://openairdocs.org/stc/SA02349LA): Installation of Lake Aero Styling and Repair Nose Gear Truss. LASAR Inc
- [STC SA3252NM](https://openairdocs.org/stc/SA3252NM): Installation of fiberglass belly fairing. LASAR Inc
- [STC SA3540NM](https://openairdocs.org/stc/SA3540NM): Installation of modified nose gear bushings. LASAR Inc
- [STC SA4443NM](https://openairdocs.org/stc/SA4443NM): Installation of gap seals and speed fairings involving 10 kits. 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 SA3555WE](https://openairdocs.org/stc/SA3555WE): Installation of Roto-Master (Rajay) turbocharged Lycoming IO-360-A3B6D and/or IO-360-A1D6D engines. TALCO Aviation
- [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 SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation
- [STC SA04586CH](https://openairdocs.org/stc/SA04586CH): Installation of Electroair Back Up Battery Panel System Control. Electroair Aquisition Corp
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc
- [STC SA02041AT](https://openairdocs.org/stc/SA02041AT): Installation of a new technology landing light. Whelen Aerospace Technologies
- [STC SA02232AT](https://openairdocs.org/stc/SA02232AT): Installation of composite nose cowl, nose landing gear doors, and induction air system. Whelen Aerospace Technologies
- [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 SA1938SW](https://openairdocs.org/stc/SA1938SW): Brittain LSA-6 lateral stability augmentation system (positive control). Brittain Industries Inc
- [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc
- [STC SA04195NY](https://openairdocs.org/stc/SA04195NY): Installation of the KFC 230 Aerocruze Automatic Flight Control System (FCS) upgraded from KFC 200 FCS. Honeywell International Inc. (Bendix King)
- [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King)

All 376: https://openairdocs.org/aircraft/N2823W/stcs.md

## Related

- Other Mooney M20J aircraft: https://openairdocs.org/model/mooney-m20j/aircraft.md
- The Lycoming I0360 SER A&C engine: https://openairdocs.org/engine/lycoming-i0360-ser-a-c.md

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