# N731AA: 1970 Cessna 182N

- Status: Valid registration
- Airframe: [Cessna 182N](https://openairdocs.org/model/cessna-182n) (registry code 2072730, 4 seats)
- Engine: [Continental O-470R](https://openairdocs.org/engine/continental-o-470r) (registry code 17071)
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13) (Textron Aviation Inc.), [TCDS E-273](https://openairdocs.org/tcds/E-273) (Continental Aerospace Technologies, Inc.) (OpenAirDocs)
- Serial number: 182-60331
- Year built: 1970
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: August 18, 2004
- Certificate issued: March 27, 2019
- Expires: March 31, 2029
- Mode S code: A9CEC3
- Registered owner: [Landis Lloyd B](https://openairdocs.org/faa-owner/LANDIS%20LLOYD%20B)
- Location: [Ardmore, OK](https://openairdocs.org/faa-place/OK/Ardmore)
- Owner type: Individual
- Owner's area on the map: 34.2077° N, 97.1068° W: Placed by OpenAirDocs at the center of ZIP code 73401, within about 11 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=731AA
- Page: https://openairdocs.org/aircraft/N731AA

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): 69 in force

### Matched by airframe (Cessna 182N)

- [AD 2024-14-03](https://openairdocs.org/ad/2024-14-03): Autopilot System · Garmin GFC 500 Autopilot (STC SA01866WI). Effective Aug 20, 2024
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 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 2020-18-01](https://openairdocs.org/ad/2020-18-01): Fuselage · Textron 172N, 172P, 172Q and 62 more. Effective Nov 12, 2020
- [AD 2011-10-09](https://openairdocs.org/ad/2011-10-09): Seat Rails and Roller Housing Inspections · Cessna 150A, 150B, 150C and 221 more. Effective Jun 17, 2011
- [AD 2008-26-10](https://openairdocs.org/ad/2008-26-10): Alternate static air source selector valve · Cessna 172, 172A, 172B and 179 more. Effective Jan 5, 2009
- [AD 2008-02-18](https://openairdocs.org/ad/2008-02-18): Pick-up collar support and nylon screws · BRS-172 parachute recovery system (Ballistic Recovery Systems STC SA01679CH or SA01999CH). Effective Feb 28, 2008
- [AD 2007-09-01](https://openairdocs.org/ad/2007-09-01): Ground power electrical cable, the fuel strainer cable, and the fuel line · Cessna 182H, 182J, 182K and 6 more. Effective Apr 25, 2007
- [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 2004-19-01](https://openairdocs.org/ad/2004-19-01): Upper shoulder harness adjusters · Cessna F150G, F150H, F150J and 129 more. Effective Nov 1, 2004
- [AD 2000-06-01](https://openairdocs.org/ad/2000-06-01): Fuel Strainer Assembly · Cessna 150F, 150G, 150H and 163 more. Effective May 5, 2000
- [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 98-25-02](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 98-16-04](https://openairdocs.org/ad/98-16-04): Inspect Angle Stiffener Along Lower Spar Cap · Cessna 180, 180A, 180B and 37 more. Effective Sep 21, 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 97-01-13](https://openairdocs.org/ad/97-01-13): Fuel, Oil and Hydraulic Hoses · Cessna 150, 150A, 150B and 232 more. Effective Feb 3, 1997
- [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996
- [AD 84-10-01 R1](https://openairdocs.org/ad/84-10-01-R1): Bladder Fuel Cells · Cessna 180, 180A, 180B and 103 more. Effective Jul 5, 1988
- [AD 79-10-14 R1](https://openairdocs.org/ad/79-10-14-R1): Fuel Tank Venting · Cessna 140A, 150, 150A and 172 more. Effective May 30, 1988
- [AD 86-24-07](https://openairdocs.org/ad/86-24-07): Engine Controls Installation · Cessna 150C, 150D, 150E and 142 more. Effective Jan 7, 1987
- [AD 72-03-03 R3](https://openairdocs.org/ad/72-03-03-R3): Wing Flap Actuators Jack Screw · Cessna F150F, F150G, F150H and 83 more. Effective Oct 15, 1984
- [AD 83-17-06](https://openairdocs.org/ad/83-17-06): Aileron Balance Weights · Flap actuated aileron droop system (Sierra Industries STC SA1382WE or 5 others). Effective Sep 1, 1983
- [AD 83-13-01](https://openairdocs.org/ad/83-13-01): Placard-Improper Fuel Cap Sealing · Cessna 182, 182A, 182B and 14 more. Effective Aug 1, 1983
- [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 81-15-03](https://openairdocs.org/ad/81-15-03): Engine Inlet Air Filters · Replace existing engine induction air filter (Brackett Aero Filters STC SA693CE or SA71GL). Effective Jul 20, 1981
- [AD 79-25-07](https://openairdocs.org/ad/79-25-07): Alternator Ground · Cessna 180, 180A, 180B and 95 more. Effective Dec 13, 1979
- [AD 79-08-03](https://openairdocs.org/ad/79-08-03): Electrical System · Cessna 120, 140, 140A and 152 more. Effective Jun 6, 1979
- [AD 78-01-14](https://openairdocs.org/ad/78-01-14): ELT Installation · Cessna 182, 182A, 182B and 16 more. Effective Jan 23, 1978
- [AD 77-23-11](https://openairdocs.org/ad/77-23-11): ELT Installation · Cessna 182, 182A, 182B and 16 more. Effective Nov 28, 1977
- [AD 77-04-05](https://openairdocs.org/ad/77-04-05): Carburetor Air Intake · Cessna 180, 180A, 180B and 39 more. Effective Mar 1, 1977
- [AD 77-02-09](https://openairdocs.org/ad/77-02-09): Wing Flap System · Cessna 150, 150A, 150B and 61 more. Effective Feb 3, 1977
- [AD 76-04-03](https://openairdocs.org/ad/76-04-03): ARC PA-500A Actuators · Cessna 172L, 172M, 177B and 43 more. Effective Feb 26, 1976
- [AD 75-16-01](https://openairdocs.org/ad/75-16-01): Wing Fuel Tanks · Cessna 180, 180A, 180B and 68 more. Effective Jul 30, 1975
- [AD 75-05-02](https://openairdocs.org/ad/75-05-02): Engine Oil · Beryl D Shannon Aviation Specialties Engine Crankcase… (D'Shannon Products STC SA2653WE). Effective Feb 21, 1975
- [AD 72-07-09](https://openairdocs.org/ad/72-07-09): Cracks And Loose Bolts In Fin & Rudder · Cessna 182, 182A, 182B and 74 more. Effective Oct 17, 1974
- [AD 74-08-01](https://openairdocs.org/ad/74-08-01): Autopilot Servo Actuators · Aircraft Radio Autopilot Servo Actuators, 172L, 172M and 29 more. Effective Apr 9, 1974
- [AD 73-23-07](https://openairdocs.org/ad/73-23-07): Defective Spar Attachment Fittings · Cessna 150, 150A, 150B and 68 more. Effective Nov 19, 1973
- [AD 73-17-01](https://openairdocs.org/ad/73-17-01): Fuel Transfer Pump Placard · Cessna 170, 170A, 170B and 53 more. Effective Aug 16, 1973
- [AD 71-22-02](https://openairdocs.org/ad/71-22-02): Cracks In Nose Gear Fork · Cessna 150, 150A, 150B and 52 more. Effective Nov 9, 1971

### Matched by engine (Continental O-470R)

- [AD 2023-17-04](https://openairdocs.org/ad/2023-17-04): Reciprocating Engine Oil System · F & M Enterprises' Model C6LC, C6LC-S or C6LC-L oil filter… (Stratus Tool Technologies STC SE09356SC or 2 others). Effective Oct 26, 2023
- [AD 2023-05-16](https://openairdocs.org/ad/2023-05-16): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 147 more. Effective Mar 15, 2023
- [AD 2023-02-12](https://openairdocs.org/ad/2023-02-12): Engine Air Intake System · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 127 more. Effective Feb 17, 2023
- [AD 2022-16-03](https://openairdocs.org/ad/2022-16-03): Engine (RECIPROCATING) · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-F and 236 more. Effective Aug 15, 2022
- [AD 2010-11-04](https://openairdocs.org/ad/2010-11-04): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 190 more. Effective Jun 16, 2010
- [AD 2010-07-08](https://openairdocs.org/ad/2010-07-08): Turbochargers · Kelly Aerospace Energy Systems HIO-360-E1AD, HIO-360-E1BD, HIO-360-F1AD and 137 more. Effective Apr 19, 2010
- [AD 2009-19-07](https://openairdocs.org/ad/2009-19-07): EQ3 cylinders · Continental Motors IO-470-C, IO-470-D, IO-470-E and 72 more. Effective Oct 7, 2009
- [AD 2007-04-19 R1](https://openairdocs.org/ad/2007-04-19-R1): SAP cylinder assemblies · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 314 more. Effective May 7, 2007
- [AD 2000-23-21](https://openairdocs.org/ad/2000-23-21): Crankshaft · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 164 more. Effective Dec 12, 2000
- [AD 99-19-01](https://openairdocs.org/ad/99-19-01): No. 2 and No. 5 Crankshaft Inspections · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 127 more. Effective Sep 30, 1999
- [AD 98-17-11](https://openairdocs.org/ad/98-17-11): Crankshafts · Continental Motors A-65-3, A-65-8, A75-8 and 90 more. Effective Oct 19, 1998
- [AD 97-21-02](https://openairdocs.org/ad/97-21-02): Cylinders · Continental Motors E165-2, E165-3, E165-4 and 61 more. Effective Oct 27, 1997
- [AD 96-12-04](https://openairdocs.org/ad/96-12-04): Pistons · Superior Air Parts Pistons, O-470-K, O-470-L and 1 more. Effective Aug 12, 1996
- [AD 95-21-15](https://openairdocs.org/ad/95-21-15): Aviation Gasoline · Continental Motors A-65-8, C85-12F, C85-12FJ and 77 more. Effective Nov 28, 1995
- [AD 93-08-17](https://openairdocs.org/ad/93-08-17): Oil Pick-Up Tube · Continental Motors IO-470-A, IO-470-C, IO-470-D and 104 more. Effective Aug 23, 1993
- [AD 93-10-02](https://openairdocs.org/ad/93-10-02): Missing Cylinder Valve Retainer Key · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 180 more. Effective Aug 12, 1993
- [AD 91-19-03](https://openairdocs.org/ad/91-19-03): Oil Filter · Continental Motors 6-285-A, 6-285-B, 6-285-BA and 169 more. Effective Sep 29, 1991
- [AD 89-04-02](https://openairdocs.org/ad/89-04-02): Carburetors · Continental Motors O-470-11, O-470-11-CI, O-470-11B and 175 more. Effective Mar 8, 1989
- [AD 88-03-06](https://openairdocs.org/ad/88-03-06): Oil Filter · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 155 more. Effective Apr 15, 1988
- [AD 85-08-02](https://openairdocs.org/ad/85-08-02): Cylinder Assemblies · Continental Motors IO-470-C, O-470-G, O-470-K and 4 more. Effective Apr 15, 1985
- [AD 81-16-05](https://openairdocs.org/ad/81-16-05): Magnetos · Lycoming Engines AEIO-320-E1B, AEIO-320-E2B, AEIO-360-B1G6 and 234 more. Effective Aug 6, 1981
- [AD 79-05-09](https://openairdocs.org/ad/79-05-09): Oil Pump Assembly Or Oil Pressure Relief Valve Screw And/Or Plunger · Teledyne Continental Motors 6-285-CA, GTSIO-520-C, GTSIO-520-D and 60 more. Effective Mar 12, 1979
- [AD 73-13-04](https://openairdocs.org/ad/73-13-04): Carburetor Bowl Drain Plug · Continental Motors O-470-J, O-470-K, O-470-L and 1 more. Effective Jun 20, 1973
- [AD 63-15-01](https://openairdocs.org/ad/63-15-01): Exhaust Valves · Continental Motors E165-2, E165-3, E165-4 and 41 more. Effective Dec 31, 1969
- [AD 69-24-03](https://openairdocs.org/ad/69-24-03): Carburetors · Continental Motors A-65-1, A-65-12, A-65-12F and 321 more. Effective Nov 29, 1969
- [AD 67-01-04](https://openairdocs.org/ad/67-01-04): Oil Filters · Full flow oil filter (Superior Flow STC SA401SW or 2 others). Effective Jan 2, 1967
- [AD 63-22-03](https://openairdocs.org/ad/63-22-03): Carburetors · Continental Motors GO-300-A, GO-300-B, GO-300-C and 143 more. Effective Dec 2, 1963
- [AD 98-01-08](https://openairdocs.org/ad/98-01-08): Exhaust Roller Rocker Arm · Roller rocker arm P/N PE 92I intake and PE92E exhaust (Performance Engineering STC SE8594SW)
- [AD 56-06-01](https://openairdocs.org/ad/56-06-01): Piston Pin Assembly · Continental Motors E165-2, E165-3, E165-4 and 41 more

### Historical (superseded or no longer in force)

- [AD 87-20-03 R2](https://openairdocs.org/ad/87-20-03-R2) (historical): Seat Tracks · Cessna 150A, 150B, 150C and 212 more. Effective Sep 24, 1990
- [AD 86-26-04](https://openairdocs.org/ad/86-26-04) (historical): Shoulder Harness Adjuster · Cessna Aircraft Company, The 120, 140, 140A and 134 more. Effective Jan 6, 1987
- [AD 2023-04-08](https://openairdocs.org/ad/2023-04-08) (historical): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 141 more. Effective Feb 23, 2023
- [AD 2022-04-04](https://openairdocs.org/ad/2022-04-04) (historical): Reciprocating Engine Oil System · F & M Enterprises' Model C6LC, C6LC-S or C6LC-L oil filter… (Stratus Tool Technologies STC SE09356SC or 2 others). Effective Mar 29, 2022
- [AD 2009-24-52](https://openairdocs.org/ad/2009-24-52) (historical): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 192 more
- [AD 2009-24-51](https://openairdocs.org/ad/2009-24-51) (historical): Hydraulic lifters · Teledyne Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 156 more
- [AD 2000-08-51](https://openairdocs.org/ad/2000-08-51) (historical): Crankshaft · Teledyne Continental Motors IO-360-A, IO-360-AB, IO-360-B and 158 more
- [AD 94-14-12](https://openairdocs.org/ad/94-14-12) (historical): Octane Aviation Gasoline · Teledyne Continental Motors A-65-8, C85-12, E185-11 and 68 more
- [AD 99-09-17](https://openairdocs.org/ad/99-09-17) (historical): Crankshaft · Teledyne Continental Motors IO-470-A, IO-470-C, IO-470-D and 114 more
- [AD 97-15-01](https://openairdocs.org/ad/97-15-01) (historical): Pistons · Teledyne Continental Motors E165-2, E165-3, E165-4 and 61 more

## Information bulletins (advisory) (17 in force)

- [SAIB AIR-21-16](https://openairdocs.org/saib/AIR-21-16): FLIGHT COMPARTMENT EQUIPMENT, Cessna Seat Back Attachment Bolt Inspection. Issued Aug 26, 2021
- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-18-23](https://openairdocs.org/saib/CE-18-23): Passenger Compartment Equipment - Installation of F. Atlee Dodge Aircraft Services LLC. Folding Jump Seats. Issued Jul 19, 2018
- [SAIB CE-17-25](https://openairdocs.org/saib/CE-17-25): ELEVATOR TORQUE TUBE  Inspections for cracks and corrosion in elevator torque tubes. Issued Aug 25, 2017
- [SAIB CE-12-41](https://openairdocs.org/saib/CE-12-41): Flight Controls  Loose Glide Screw. Issued Aug 9, 2012
- [SAIB CE-12-14](https://openairdocs.org/saib/CE-12-14): Three Alternative Methods of Compliance for AD 2011-10-09. Issued Jan 25, 2012
- [SAIB CE-10-40R1](https://openairdocs.org/saib/CE-10-40R1): Aircraft Fuel System; water contamination of fuel tank systems on Cessna single engine airplanes. Issued Jul 30, 2010
- [SAIB CE-09-42](https://openairdocs.org/saib/CE-09-42): Lights - Landing Light, Beacon Light and Taxi Light Switch Applications. Issued Jul 24, 2009
- [SAIB CE-09-10](https://openairdocs.org/saib/CE-09-10): Availability of Secondary Seat Stops for Pilot and Copilot Seats. Issued Feb 5, 2009
- [SAIB CE-09-01](https://openairdocs.org/saib/CE-09-01): Equipment - Emergency. Issued Oct 21, 2008
- [SAIB CE-08-02](https://openairdocs.org/saib/CE-08-02): Flight Controls. Issued Nov 2, 2007
- [SAIB CE-01-41R2](https://openairdocs.org/saib/CE-01-41R2): Flight Controls. Issued Oct 1, 2007
- [SAIB CE-04-11](https://openairdocs.org/saib/CE-04-11): . Issued Oct 28, 2003
- [SAIB NE-16-13](https://openairdocs.org/saib/NE-16-13): Powerplant - Prohibited use of sealant. Issued Mar 8, 2016
- [SAIB NE-13-04](https://openairdocs.org/saib/NE-13-04): Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing Inspection. Issued Oct 31, 2012
- [SAIB NE-10-09](https://openairdocs.org/saib/NE-10-09): Reciprocating Engine Power Section: Hydraulic Valve Lifters. Issued Nov 20, 2009
- [SAIB NE-09-08](https://openairdocs.org/saib/NE-09-08): Reciprocating Engine Cylinder Section. Issued Jan 30, 2009
- [SAIB CE-01-41R1](https://openairdocs.org/saib/CE-01-41R1) (historical): Cracks in plastic or non-metallic control wheels. Issued Jan 10, 2007

## NTSB investigations

None matched to N731AA.

## 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 20050608016729I](https://openairdocs.org/incident/20050608016729I), Jun 8, 2005: Cessna 182N (N731AA), Jacksonville, FL, Minor damage. (-23) The pilot failed to take tow bar off prior to engine start up. Props made contact with the tow bar. Pilot did not provide information for sections 13 and…

## Reports on N731AA not matched to an aircraft (3)

They name N731AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19940117003239I](https://openairdocs.org/incident/19940117003239I), Jan 17, 1994: Boeing 727227 (N731AA), Raleigh-Durham, NC. Narrative: at approximately 1045, flight 1161, N731AA, departed rdu for cun. Immediately after takeoff, flight attendant reported hearing a loud swooshing…
- [Incident 19820917053889I](https://openairdocs.org/incident/19820917053889I), Sep 17, 1982: Boeing 727227 (N731AA), New Orleans, LA. When flight attendant opened lavatory door a male passenger tumbled out. Passenger dead on arrival at airport.
- [Incident 19820216011739I](https://openairdocs.org/incident/19820216011739I), Feb 16, 1982: Boeing 727227 (N731AA), Miami, FL. Unable to retract nose gear. Returned and made an overweight landing. Nose gear safety pin not removed.

## 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 N731AA not matched to an aircraft (63, newest 50)

They name N731AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR AALA20011783](https://openairdocs.org/sdr/AALA20011783), Sep 17, 2001: LIGHT. INOPERATIVE. DTW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NOMAL OPERA
- [SDR AALA20011596](https://openairdocs.org/sdr/AALA20011596), Aug 5, 2001: WIRE. BROKEN. RDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT SEAT 16 THROUGH 18 INOPERATIVE. REPAIRED BROKEN WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION
- [SDR AALA20011411](https://openairdocs.org/sdr/AALA20011411), Jul 9, 2001: TRUNNION. CORRODED. TUL - FOUND CORROSION IN NOSE GEAR TRUNNION FITTINGS. CORROSION REMOVED, NOSE GEAR TRUNNION FITTINGS WERE REBORED AND REBUSHED PER ESO 11697 DATED 7/6/2001. (M)
- [SDR AALA20011410](https://openairdocs.org/sdr/AALA20011410), Jul 6, 2001: BEAM. CORRODED. TUL - FOUND LEFT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM CORRODED SS136 TO SS142. REMOVED CORROSION, INSTALLED DOUBLER REPAIR PER ESO 11697 DATED 7-6-01.
- [SDR AALA20011412](https://openairdocs.org/sdr/AALA20011412), Jul 5, 2001: STRINGER. TUL - FOUND RIVETS HEADS POPPED AND SKIN BULGED AT STRINGER 21R JUST AFT OF STRINGER 440. REMOVED CORRODED SECTION OF STRINGER 21R AND INSTALLED STRINGER SPLICE
- [SDR AALA20010498](https://openairdocs.org/sdr/AALA20010498), Mar 15, 2001: LIGHT. DEFECTIVE. DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT RIGHT OVERWING EXIT SIGN DIM. REPLACED EMERGENCY EXIT LIGHT AT RIGHT OVERWING EXIT SIGN. SYSTEM GROU
- [SDR AALA20001188](https://openairdocs.org/sdr/AALA20001188), Jul 14, 2000: SPAR. CORRODED. TUL - FORWARD LOWER SPAR CORD HAS INTERGRANULAR CORROSION BELOW NR 3 LEADING EDGE FLAP ACTUATOR SUPPORT STRUCTURE. INSTALLED REPAIR PER ESO 11697 DATED 7-7-00. 
- [SDR AALA20001187](https://openairdocs.org/sdr/AALA20001187), Jul 14, 2000: SKIN. BULGED. TUL - BULGE IN BELLY SKIN STA 708 - STR 27L. INSTALLED REPAIR STA 700 - STA 720 PER ESO 11697 DATED 7-14-00. (X)
- [SDR AALA20001186](https://openairdocs.org/sdr/AALA20001186), Jul 13, 2000: STRINGER. DAMAGED. TUL - STR 28L HAS TOOLING DAMAGE 4 INCHES FORWARD STA 950B. CUT OUT DAMAGED AREA, INSTALLED 'U' CHANNEL REPAIR PER SRM 53-10-3 FIG 2 SHEET 3. (X)
- [SDR AALA20001185](https://openairdocs.org/sdr/AALA20001185), Jul 12, 2000: FRAME. GOUGED. TUL - BELT FRAME STA 950C HAS DEEP GOUGE AND SEVERAL DENTS IN FRAME RADIUS BETWEEN STR 25R AND STR 27R. INSTALLED DOUBLER PER SRM 53-10-4. (X)
- [SDR AALA20001197](https://openairdocs.org/sdr/AALA20001197), Jul 11, 2000: FRAME. DENTED. TUL - DENT IN PREVIOUS REPAIR ON BELT FRAME STA 950F BETWEEN STR 25L AND STR 26L. REPLACED REPAIR SECTION PER SRM 51-40-3. SIZE OF REPAIR 24 INCHES LONG. FASTEN
- [SDR AALA20001196](https://openairdocs.org/sdr/AALA20001196), Jul 11, 2000: FRAME. DENTED. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-40-3, FIG 1. MATERIAL 7075T6 .050 INCH FASTENERS MS2047006 WITH 5 ROWS PAST DAMAGE USING EXISTING FASTENER
- [SDR AALA20001198](https://openairdocs.org/sdr/AALA20001198), Jul 10, 2000: FRAME. CRACKED. TUL - CRACK IN WEB FORWARD CARGO DOOR FRAME AT RIVET HOLE BETWEEN LOWER FORWARD DOOR STOP. INSTALLED DOUBLER PER SRM 51-40-2, FIG 1 WITH MATERIAL 17.7 MT1050 KS
- [SDR AALA20000558](https://openairdocs.org/sdr/AALA20000558), Mar 27, 2000: CYLINDER. DEFECTIVE. DFW - FLT 463 - DURING CLIMB, GEAR DOOR DISAGREEMENT LIGHT ILLUMINATED. NOSE GEAR DOOR LIGHT ON FLIGHT ENGINEERS PANEL ILLUMINATED. GEAR SELECTOR MOVED TO UP PO
- [SDR AALA20000401](https://openairdocs.org/sdr/AALA20000401), Mar 5, 2000: WIRE. BROKEN. MIA - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT, CEILING AND ESCAPE FLOOR PATH LIGHTS INOPERATIVE. REPAIRED WIRE JUMPER. SYSTEM GROUND CHECK NORMAL OPERATION.
- [SDR AALA991263](https://openairdocs.org/sdr/AALA991263), Aug 23, 1999: SKIN. DENTED. TUL - FOUND DENT IN SKIN BS 245, STRINGER 16R AND 17R. INSTALLED DOUBLER PER SRM 53-30-3. (M)
- [SDR AALA991260](https://openairdocs.org/sdr/AALA991260), Aug 23, 1999: ANGLE. CORRODED. TUL - FOUND CORROSION ON RIGHT SKATE ANGLE STATION 310-320. FABRICATED AND INSTALLED REPAIR PER ESO 11697, DATED 8/23/99. (M)
- [SDR AALA991262](https://openairdocs.org/sdr/AALA991262), Aug 21, 1999: SKIN. CORRODED. TUL - FOUND CENTER TANK LOWER SKIN HAS 4 AREAS OF CORROSION ABOVE LEFT PRIMARY HEAT EXCHANGER STATION 833-837. INSTALLED DOUBLER AND TRIPLER REPAIR PER ESO 1169
- [SDR AALA991261](https://openairdocs.org/sdr/AALA991261), Aug 17, 1999: SKIN. CORRODED. TUL - FOUND SKIN LAP CORROSION STRINGER 19R, 17 INCH LENGTH BULGED AND CRACKED. CUT OUT CORRODED AREA OF THE SKIN LAP AND INSTALLED DOUBLER PER 53-30-3 FIG 5 P2
- [SDR AALA991111](https://openairdocs.org/sdr/AALA991111), Jul 29, 1999: WIRE. BROKEN. MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIPS IN CABIN MID SECTION INOPERATIVE. REPLACED WIRING TO EMERGENCY EXIT FLOOR PATH LIG
- [SDR AALA982224](https://openairdocs.org/sdr/AALA982224), Dec 1, 1998: FILLER. MISINSTALLED. TUL - STRINGER 25R FILLER AFT STATION 440 HAS MATERIAL WITH LESS THICKNESS THAN ORIGINAL STRINGER MATERIAL. REMOVED FILLER STATION 440, STRINGER 25R. INSTALLED 
- [SDR AALA982140](https://openairdocs.org/sdr/AALA982140), Dec 1, 1998: SKIN. CRACKED. TUL - FOUND FUSELAGE SKIN BULGED AND CRACKED AT STRINGER 25R AND BELOW, BETWEEN STATION 444 AND 459. CUT OUT DAMAGED AREA SKIN STATION 440-463, STRINGER 25R TO 
- [SDR AALA981536](https://openairdocs.org/sdr/AALA981536), Aug 14, 1998: FRAME. CORRODED. TUL - FOUND CORROSION ON BELLFRAME STATION 1050 BETWEEN STATION 26L AND 28L. REMOVED CORROSION AND TREATED PER SRM 51-20-0 AND REPAIRED PER SRM 51-40-3. (M)
- [SDR AALA981520](https://openairdocs.org/sdr/AALA981520), Aug 12, 1998: FLOORBEAM. DAMAGED. TUL - FOUND FLOORBEAM UPPER CAP STATION 360 RBL 10 TO RBL 14. REPAIRED PER AARD 53-10-07-07 FIG 2. (M)
- [SDR AALA981519](https://openairdocs.org/sdr/AALA981519), Aug 11, 1998: FLOORBEAM. CORRODED. TUL - FOUND FLOORBEAM UPPER CAP CORRODED AND CRACKED, STATION 344 RBL 10 TO RBL 22. REMOVED CORRODED SECTION OF FLOORBEAM UPPER CAP STATION 344 RBL 10 TO RBL 58
- [SDR AALA981514](https://openairdocs.org/sdr/AALA981514), Aug 11, 1998: FRAME. GOUGED. TUL - DEEP GROOVE AND SMALL NICKS ON BELLFRAME AT STATION 1110 STRINGER 26R TO STRINGER 27R. INSTALLED DOUBLER ON BELLFRAME PER SRM 53-10-4. (M)
- [SDR AALA981513](https://openairdocs.org/sdr/AALA981513), Aug 11, 1998: FRAME. DENTED. TUL - BELLFRAME IS DENTED AT STATION 580 ABOVE STRINGER 24L. INSTALLED DOUBLER PER SRM 53-10-4. (M)
- [SDR AALA981512](https://openairdocs.org/sdr/AALA981512), Aug 11, 1998: SPAR. CORRODED. TUL - FOUND CORROSION ON TOP AND BOTTOM OF LE SPAR LOWR CHORD ANGLE AT WING LE STATION 392, BELOW FUEL VALVE. INSTALLED STRIP DOUBLER ON UPPER SIDE OF BLENDED A
- [SDR AALA981511](https://openairdocs.org/sdr/AALA981511), Aug 11, 1998: SKIN. CORRODED. TUL - AFT HEAT EXCHANGER PLENUM CORRODED RT SIDE. INSTALLED DOUBLER REPAIR IAW ESO 11697, DATED 7-14-98. (M)
- [SDR AALA981510](https://openairdocs.org/sdr/AALA981510), Aug 11, 1998: SKIN. DAMAGED. TUL - LIGHTING STRIKE BLEND OUT IS BEYOND LIMITS. INSTALLED DOUBLER REPAIR PER AARD 53-30-3, PAGE 1, 5, 7, 8 OF SRM 53-30-3. (M)
- [SDR AALA981509](https://openairdocs.org/sdr/AALA981509), Aug 11, 1998: SPAR. CRACKED. TUL - CHORD ANGLE CRACKED 3 INCHES FORWARD OF NR 7 SPOILER CASTING. CUT OUT DAMAGED SECTION OF LOWER CHORD ANGLE AND SPLICED IN NEW SECTION PER SRM 51-40-4. (M)
- [SDR AALA981508](https://openairdocs.org/sdr/AALA981508), Aug 11, 1998: SKIN. CORRODED. TUL - FOUND CORROSION UNDER INBOARD WALL ATTACH CHANNEL STATION 1130-1136 RBL 19 INCHES TO 24 INCHES, RT AFT LAV. REPAIRED WEB PER SRM 51-40-2. (M)
- [SDR AALA981507](https://openairdocs.org/sdr/AALA981507), Aug 11, 1998: SKIN. CREASED. TUL- FUSELAGE SKIN HAS SHARP CREASE STATION 277, STRINGER 17 LEFT OUT OF LIMITS PER SRM 53-30-1. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-30-3 PAGE 14B. 
- [SDR AALA981504](https://openairdocs.org/sdr/AALA981504), Aug 11, 1998: STRINGER. CRACKED. TUL - FOUND STRINGER 15 CRACKED AT END STATION 720C. REPAIRED STRINGER 15L, STATION 720C PER SRM 53-10-3. (M)
- [SDR AALA981503](https://openairdocs.org/sdr/AALA981503), Aug 11, 1998: STRINGER. CRACKED. TUL - FOUND CRACK IN STRINGER END STATION 720 PLUS 5 INCHES, STRINGER 15R. REPAIRED STRINGER 15R AT STATION 720B PER SRM 53-10-3. (M)
- [SDR AALA981502](https://openairdocs.org/sdr/AALA981502), Aug 11, 1998: STRINGER. CRACKED. TUL - FOUND STRINGER 15L CRACKED AT END STATION 720B PLUS 3 INCHES. REPAIRED STRINGER 15L, STATION 720B PLUS 3 INCHES PER SRM 53-10-3. (M)
- [SDR AALA981501](https://openairdocs.org/sdr/AALA981501), Aug 11, 1998: STRINGER. CORRODED. TUL - FOUND STATION 720L PLUS 13 INCHES STRINGER 27L OUTBOARD SIDE HAS CORROSION. CUT OUT STRINGER SECTION AND SPLICED IN NEW SECTION PER SRM 53-10-3. (M)
- [SDR AALA981500](https://openairdocs.org/sdr/AALA981500), Aug 11, 1998: FLOORBEAM. CORRODED. TUL - FLOORBEAM CORRODED UNDER SEAT TRACK TOP AND BOTTOM SIDE OF UPPER FLANGES. FLOORBEAM REPAIRED PER SRM 53-10-8. (M)
- [SDR AALA981499](https://openairdocs.org/sdr/AALA981499), Aug 11, 1998: FLOORBEAM. CORRODED. TUL - FLOORBEAM CORRODED UPPER FLANGE UNDER SEAT TRACK STATION 1110 LBL 24. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-10-8. (M)
- [SDR AALA981498](https://openairdocs.org/sdr/AALA981498), Aug 11, 1998: FLOORBEAM. CORRODED. TUL - FLOORBEAM AT STATION 1110 RBL 8 HAS CORROSION ON UPPER FLANGE AROUND FLOORBOARD HOLE. CUT OUT SECTION OF TOP FLANGE AND REPAIRED PER SRM 53-10-8 PAGE 9A A
- [SDR AALA981497](https://openairdocs.org/sdr/AALA981497), Aug 11, 1998: FLOORBEAM. CORRODED. TUL - FOUND FLOORBEAM 1130 RBL 25 CORRODED AT BOLT HOLE. REPAIRED FLOORBEAM PER ESO 11697, DATED 7/19/98. (M)
- [SDR AALA981496](https://openairdocs.org/sdr/AALA981496), Aug 11, 1998: STRINGER. CRACKED. TUL - STRINGER CRACKED ON TOP OF RIB AT WING LT STATION 629 AFT OF FUEL DUMP TUBE 5TH OPENING FROM TIP. INSTALLED STRINGER REPAIR PER BOEING SB 727-57A159. (M)
- [SDR AALA981495](https://openairdocs.org/sdr/AALA981495), Aug 11, 1998: SHEAR TIE. CORRODED. TUL - SHEAR TIE CORRODED STATION 720B BETWEEN STRINGER 20R AND 26R. REPLACED SHEAR TIE PER SRM 51-10-1. (M)
- [SDR AALA981440](https://openairdocs.org/sdr/AALA981440), Jul 28, 1998: FRAME. BENT. TUL - BELL FRAME BENT AT STATION 990 BETWEEN STRINGER 25L-26L. INSTALLED DOUBLER PER SRM 53-10-4. (M)
- [SDR AALA981439](https://openairdocs.org/sdr/AALA981439), Jul 28, 1998: FRAME. DENTED. TUL - DENT AT STATION 1030 STRINGER 25-26R. INSTALLED DOUBLER PER SRM 53-10-4. (M)
- [SDR AALA981505](https://openairdocs.org/sdr/AALA981505), May 11, 1998: BEAM. CORRODED. TUL - UPPER TE BEAM HAS CORROSION ON TOP SURFACE OF BEAM, ABOVE NR 4 RIB SUPPORT CASTING. REF E58 NR 0123429. REMOVED CORROSION PER SRM 51-10-6. INSTALLED BEAM 
- [SDR AALA972249](https://openairdocs.org/sdr/AALA972249), Nov 25, 1997: LIGHT. INOPERATIVE. TUL - RIGHT AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. OVERHEAD TOP OF DOOR. REPLACED RT AFT SERVICE DOOR BATTERY PACK. TST: 67,128.48 HOURS. CYCLES: 44
- [SDR AALA972239](https://openairdocs.org/sdr/AALA972239), Nov 22, 1997: CONNECTOR. LOOSE. DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 17 THROUGH 23 INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY P
- [SDR AALA972115](https://openairdocs.org/sdr/AALA972115), Nov 5, 1997: BATTERY PACK. DISCHARGED. TUL - SLIDE LIGHT FOR FORWARD ENTRY SERVICE DOOR INOPERATIVE. REMOVED, INSTALLED SERVICEABLE BATTERY PACK. TST: 66,894.26 HOURS. CYCLES: 44,081. (X)
- [SDR AALA970835](https://openairdocs.org/sdr/AALA970835), Apr 23, 1997: SKIN. CORRODED. AFW - SKIN AT STA 970 TO STA 1010, STR 17R BULGED AS MARKED. (CORROSION) REPAIRED SKIN PER SRM 53-30-3 FIGURE 3A. TST: 65,744.04 HOURS. CYCLES, 43,423. (X)

All 63: https://openairdocs.org/aircraft/N731AA/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (586, 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 (Cessna 182N)

- [STC SA00709CH](https://openairdocs.org/stc/SA00709CH): Installation of replacement wing root vent described by Dwg Nos. 8-30-96-1& 8-30-96-2, no rev, both dtd 8/30/96, or later FAA app rev. Gallagher Aviation, LLC
- [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 SA02069AK](https://openairdocs.org/stc/SA02069AK): Fabrication and installation of the Airglas, Inc., Landes PA32-206LA Nose Fork equipped with up to a 8.50 x 6 tire. Airglas Inc
- [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 SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [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 SA04439NY](https://openairdocs.org/stc/SA04439NY): Installation of an X cam Pod. J & C Engineering Services LTD
- [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 SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies
- [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 SA00152WI](https://openairdocs.org/stc/SA00152WI): 1) Installation of Continental IO-520-D engine and Hartzell PHC-L3YF-1RF/F7691 propeller OR 2) Installation of Continental IO-550-D engine and Hartzell PHC-L3YF-1RF/F7691 or PHC-G3YF-1RF/F8468A()-6R propeller. Air Plains Services Corporation
- [STC SA01302AT](https://openairdocs.org/stc/SA01302AT): Installation of Teledyne Continental Motors Model IO-520-D engine and either a McCauley Model D3A34C401/90DFA-10 or Hartzell Model PHC-C3YF-1RF/F8468A( )-6R or PHC-C3YF-1RF/F7691( ) or PHC-G3YF-1RF/F8468A( )-6Ror PHC-G3YF-1RF/F7691( ) 3-blade propeller. Air Plains Services Corporation
- [STC SA01218AT](https://openairdocs.org/stc/SA01218AT): Installation of a Teledyne Continental Motors Model IO-550-D engine and either a Hartzell Model PHC-C3YF-1RF/F8468A( )-6R or PHC-C3YF-1RF/F7691( ) or PHC-G3YF-1RF/F8468A( )-6R or PHC-G3YF-1RF/F7691( )or McCauley Mod D3A34C401/90DFA-10 3-blade propeller. Air Plains Services Corporation
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA12284IB](https://openairdocs.org/stc/SA12284IB): Installation of Bulkhead Reinforcing Kit. Acorn Welding Ltd
- [STC SA01866WI](https://openairdocs.org/stc/SA01866WI): Installation of Garmin GFC 500 Autopilot with Electronic Stability and Protection. Garmin International Inc
- [STC SA12276IB](https://openairdocs.org/stc/SA12276IB): Payload System Installation. Icarus Aero Inc
- [STC SA04075CH](https://openairdocs.org/stc/SA04075CH): Installation of Dynon EFIS-D10A EAA sales kit part number 102778-000. Dynon Avionics Inc
- [STC SA02266AK](https://openairdocs.org/stc/SA02266AK): Replacement of Rudder and Elevator Hinge Bearings with P. Ponk Aviation Bearing p/n PPA-1401. McFarlane Aviation LLC
- [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector. 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 SA04491CH](https://openairdocs.org/stc/SA04491CH): Installation of Hartzell Propeller Model HC-( )3YF-1RF/F8429(K,B)-( ) 3 bladed metal propeller in accordance with the installation instructions specified on FAA Approved Model List (AML) No. SA04491CH. Hartzell Propeller LLC
- [STC SA01330LA](https://openairdocs.org/stc/SA01330LA): Installation of alternate avionics support assembly. Radiorax Aviation Systems LLC
- [STC SA04643CH](https://openairdocs.org/stc/SA04643CH): Installation of Hartzell Propeller model HC-(C,G,J)3YF-1N/NM8411-( ). Hartzell Propeller LLC
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA01120SE](https://openairdocs.org/stc/SA01120SE): Installation of Door Steward. Mountain View Aviation LLC
- [STC SA865SO](https://openairdocs.org/stc/SA865SO): Installation of portable hand control. Union Aviation 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 SA02784SE](https://openairdocs.org/stc/SA02784SE): Installation of third lap seat belt for rear bench seat to accommodate additional passenger. Mohr Engineering Services LLC
- [STC SA00871SE](https://openairdocs.org/stc/SA00871SE): Installation of cockpit sunvisors. Rosen Sunvisor Systems LLC
- [STC SA2000CE](https://openairdocs.org/stc/SA2000CE): Operation of airplane on unleaded automotive gasoline, 87 minimum antiknock index and leaded automotive gasoline, 88 minimum antiknock index (RON + MON)/2 per ASTM Specification D-4814. Petersen Aviation Inc
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA04353CH](https://openairdocs.org/stc/SA04353CH): Installation of Hartzell propeller model DHC-G2YF-1BFP/F8068+2 and applicable spinner. Hartzell Propeller Inc
- [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc
- [STC SA04835NY](https://openairdocs.org/stc/SA04835NY): Installation of sky dive step and door modification. Sealand Aviation Ltd
- [STC SA02575AK](https://openairdocs.org/stc/SA02575AK): Installation of the nose tire scraper P/N TSL-100. Aero Twin Inc
- [STC SA02576AK](https://openairdocs.org/stc/SA02576AK): Installation of Cleveland and ABI, LLC Wheel and Brake Kits. ABI LLC
- [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 SA3-44](https://openairdocs.org/stc/SA3-44): Installation of model AWB-2500A(aircraft skis) main and AWN-1200 nose wheel-skis. ee Dodge Aircraft Services. Lists 182 Series
- [STC SA1686WE](https://openairdocs.org/stc/SA1686WE): Installation of Vibration Isolation Products (VIP) engine mount P/Ns VIP 50525-1 and VIP 50545-1 on various aircraft as shown on FAA Approved Model List (AML) No. SA1686WE. FTG, Inc

All 586: https://openairdocs.org/aircraft/N731AA/stcs.md

## Related

- Other Cessna 182N aircraft: https://openairdocs.org/model/cessna-182n/aircraft.md
- The Continental O-470R engine: https://openairdocs.org/engine/continental-o-470r.md

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