# N83SW: 1979 Cessna TR182

- Status: Valid registration
- Airframe: [Cessna TR182](https://openairdocs.org/model/cessna-tr182) (registry code 2072735, 4 seats)
- Engine: [Lycoming O-540-L3C5D](https://openairdocs.org/engine/lycoming-o-540-l3c5d) (registry code 42364)
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13) (Textron Aviation Inc.), [TCDS E-295](https://openairdocs.org/tcds/E-295) (Lycoming Engines) (OpenAirDocs)
- Serial number: R18200625
- Year built: 1979
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: February 2, 2007
- Certificate issued: September 27, 2019
- Expires: September 30, 2029
- Mode S code: AB57A6
- Registered owner: [Rogers Gary A](https://openairdocs.org/faa-owner/ROGERS%20GARY%20A)
- Location: [Novi, MI](https://openairdocs.org/faa-place/MI/Novi)
- Owner type: Individual
- Owner's area on the map: 42.4738° N, 83.5200° W: Placed by OpenAirDocs at the center of ZIP code 48374, 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=83SW
- Page: https://openairdocs.org/aircraft/N83SW

From the FAA registry file of October 20, 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): 40 in force

### Matched by airframe (Cessna TR182)

- [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 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). 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 2008-10-02](https://openairdocs.org/ad/2008-10-02): Part number identification placard · Cessna 172, 172R, 172RG and 64 more. Effective May 12, 2008
- [AD 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies · Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. Effective Jul 11, 2006
- [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 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 98-16-04](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 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 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 83-22-06](https://openairdocs.org/ad/83-22-06): Aileron Hinge Pin · Cessna 152, 172N, 172P and 18 more. Effective Nov 8, 1983
- [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 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

### Matched by engine (Lycoming O-540-L3C5D)

- [AD 2026-17-10](https://openairdocs.org/ad/2026-17-10): Reciprocating Engine Cylinder Section · Lycoming Engines O-235, O-235-A, O-235-AP and 159 more. Effective Sep 14, 2026
- [AD 2026-04-11](https://openairdocs.org/ad/2026-04-11): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 605 more. Effective Apr 8, 2026
- [AD 2017-16-11](https://openairdocs.org/ad/2017-16-11): Reciprocating Engine Power Section · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-360-B1G6 and 93 more. Effective Aug 15, 2017
- [AD 2012-19-01](https://openairdocs.org/ad/2012-19-01): Crankshafts · Lycoming Engines AEIO-360-A1A, AEIO-360-A1B, AEIO-360-A1B6 and 321 more. Effective Oct 24, 2012
- [AD 2012-03-07](https://openairdocs.org/ad/2012-03-07): Carburetor · Lycoming Engines GO-435, GO-435-C2 (O-435-17), GO-435-C2A and 389 more. Effective Mar 27, 2012
- [AD 2011-13-03](https://openairdocs.org/ad/2011-13-03): Turbocharger Turbine · Lycoming Engines LTO-360-E1A6D, O-540-L3C5D, TIGO-541-E1A and 20 more. Effective Jul 13, 2011
- [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 2009-26-12](https://openairdocs.org/ad/2009-26-12): Cylinder assemblies · Engine Components Reciprocating Engine Cylinder Assemblies, AEIO-320-D1B, AEIO-320-D2B and 264 more. Effective Feb 4, 2010
- [AD 2005-19-11](https://openairdocs.org/ad/2005-19-11): Crankshafts · Lycoming Engines AEIO-360-A1B6, AEIO-360-A1E6, AEIO-540-D4A5 and 59 more. Effective Oct 21, 2005
- [AD 2005-12-06](https://openairdocs.org/ad/2005-12-06): Riveted-impulse coupling assemblies and snap-ring coupling assemblies · Lycoming Engines AEIO-540-D4A5, AEIO-540-D4B5, AEIO-540-D4C5 and 154 more. Effective Jul 19, 2005
- [AD 2004-10-14](https://openairdocs.org/ad/2004-10-14): Crankshaft gear · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 642 more. Effective Jun 25, 2004
- [AD 2004-05-24](https://openairdocs.org/ad/2004-05-24): Zinc-plated Crankshaft Gear Retaining Bolts · Lycoming Engines AEIO-540-D4A5, AEIO-540-D4B5, AEIO-540-D4C5 and 161 more. Effective Mar 30, 2004
- [AD 2002-12-07](https://openairdocs.org/ad/2002-12-07): Oil Filter Converter Plate Gasket or the Converter Plate Kit · Lycoming Engines HIO-360-E1AD, HIO-360-E1BD, HIO-360-F1AD and 95 more. Effective Jul 3, 2002
- [AD 96-23-03](https://openairdocs.org/ad/96-23-03): High pressure fuel pumps · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 174 more. Effective Dec 23, 1996
- [AD 95-07-01](https://openairdocs.org/ad/95-07-01): Connecting Rod Bolt · Lycoming Engines AEIO-360-A1E, AEIO-360-B1G6, AEIO-360-H1A and 177 more. Effective Apr 12, 1995
- [AD 87-10-06 R1](https://openairdocs.org/ad/87-10-06-R1): Rocker Arm Assembly · Lycoming Engines IO-360-B4, IVO-360-A1A, O-340-A1A and 243 more. Effective Sep 1, 1989
- [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 79-08-06](https://openairdocs.org/ad/79-08-06): Carburetors · Lycoming Engines O-540-L3C5D and Carburetors. Effective Apr 25, 1979
- [AD 75-08-09](https://openairdocs.org/ad/75-08-09): Oil Pump Drive Shaft · Lycoming Engines AEIO-360-A1B, AEIO-360-A1B6, AEIO-360-A1C and 365 more. Effective Aug 18, 1977
- [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 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

### 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 2024-21-02](https://openairdocs.org/ad/2024-21-02) (historical): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 548 more. Effective Dec 5, 2024
- [AD 2008-19-05](https://openairdocs.org/ad/2008-19-05) (historical): Parallel Valve'' reciprocating engines · Engine Components Reciprocating Engine Cylinder Assemblies, AEIO-320-D1B, AEIO-320-D2B and 262 more. Effective Oct 20, 2008
- [AD 2006-20-09](https://openairdocs.org/ad/2006-20-09) (historical): Certain crankshafts replacing · Lycoming Engines AEIO-360-A1B6, AEIO-360-A1E6, AEIO-540-D4A5 and 82 more. Effective Nov 3, 2006
- [AD 2005-26-10](https://openairdocs.org/ad/2005-26-10) (historical): ECi cylinder assemblies. · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 413 more. Effective Jan 31, 2006
- [AD 2000-18-53](https://openairdocs.org/ad/2000-18-53) (historical): Oil Filter Converter Plate Gaskets · Textron Lycoming, AVCO AEIO-540, IO-360-A1B6D, IO-360-A1D6D and 73 more

## Information bulletins (advisory) (15 in force)

- [SAIB CE-17-16](https://openairdocs.org/saib/CE-17-16): Main Landing Gear  Actuator Inspection. Issued Jun 9, 2017
- [SAIB CE-13-16](https://openairdocs.org/saib/CE-13-16): Hydraulic Power Pack/Landing Gear System. Issued Feb 8, 2013
- [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-09-10](https://openairdocs.org/saib/CE-09-10): Availability of Secondary Seat Stops for Pilot and Copilot Seats. Issued Feb 5, 2009
- [SAIB CE-08-02](https://openairdocs.org/saib/CE-08-02): Flight Controls. Issued Nov 2, 2007
- [SAIB CE-02-10](https://openairdocs.org/saib/CE-02-10): . Issued Jan 4, 2002
- [SAIB NE-19-08](https://openairdocs.org/saib/NE-19-08): Reciprocating Engine Cylinder Section - Lycoming Engines Parallel Valve Cylinders. Issued May 2, 2019
- [SAIB NE-08-32R1](https://openairdocs.org/saib/NE-08-32R1): Propeller Governor  Idler Gear Shaft Set Screw. Issued May 13, 2016
- [SAIB NE-14-13](https://openairdocs.org/saib/NE-14-13): Reciprocating Engine - Cylinder Mounting Studs. Issued Mar 24, 2014
- [SAIB NE-13-06](https://openairdocs.org/saib/NE-13-06): Pushrod Shroud Spring Retainers, Engine Components Part No. AEL14995, for Lycoming Engines 320, 360, and 540 Series Engines. Issued Nov 21, 2012
- [SAIB NE-08-26R3](https://openairdocs.org/saib/NE-08-26R3): Magneto/Distributor. Issued Mar 31, 2011
- [SAIB NE-06-32R1](https://openairdocs.org/saib/NE-06-32R1): Reciprocating Engine - Crankshaft. Issued Sep 10, 2008
- [SAIB NE-05-40](https://openairdocs.org/saib/NE-05-40): . Issued Mar 18, 2005
- [SAIB NE-08-26R1](https://openairdocs.org/saib/NE-08-26R1) (historical): Dual Magnetos. Issued Jul 8, 2008
- [SAIB NE-08-32](https://openairdocs.org/saib/NE-08-32) (historical): Propeller Governor Set Screw. Issued Jul 3, 2008

## NTSB investigations

None matched to N83SW.

## 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; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19851012067299I](https://openairdocs.org/incident/19851012067299I), Oct 12, 1985: Boeing 7372H4 (N83SW), Ft Worth, TX, Minor damage. While turning into parking area, jet blast caused tied down aircraft to strike each other causing minor damage.

## Service difficulty reports (44)

As reported by operators and repair stations.

- [SDR SWAA000514](https://openairdocs.org/sdr/SWAA000514), Mar 16, 2000: BEAM. CORRODED. DURING SCHEDULED D CHECK, FOUND CORROSION ON UPPER FLANGE OF LONGITUDINAL BEAM, BS 540-727, RBL 25. REMOVED AND REPLACED LONGITUDINAL BEAM UPPER FLANGE PER SRM.
- [SDR SWAA000507](https://openairdocs.org/sdr/SWAA000507), Mar 15, 2000: SKIN. CRACKED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED ON LOWER FWD CORNER OF AFT CARGO DOOR CUTOUT. REPAIRED SKIN PER ER 00-0244.
- [SDR SWAA000506](https://openairdocs.org/sdr/SWAA000506), Mar 15, 2000: STRINGER. CRACKED. DURING SCHEDULED D-CHECK, FOUND STRINGER 10L CRACKED BS 297. REPAIRED STRINGER PER SRM.
- [SDR SWAA000505](https://openairdocs.org/sdr/SWAA000505), Mar 15, 2000: BEAM. CRACKED. DURING SCHEDULED D-CHECK, FOUND CENTER SECTION LONGITUDINAL BEAM CRACKED IN 2 PLACES, BS 663 AND BS 667, LBL 25. REPAIRED BEAM PER ACO523-57.
- [SDR SWAA000500](https://openairdocs.org/sdr/SWAA000500), Mar 14, 2000: STRINGER. CORRODED. DURING SCHEDULED D-CHECK, FOUND STRINGER 20R CORRODED, BS 901-913. REPAIRED STRINGER PER SRM.
- [SDR SWAA000499](https://openairdocs.org/sdr/SWAA000499), Mar 14, 2000: FRAME. CRACKED. DURING SCHEDULED D-CHECK, FOUND 2 FRAMES CRACKED, BS 480 AND BS 460 LBL 21. REPAIRED FRAMES PER SRM.
- [SDR SWAA000498](https://openairdocs.org/sdr/SWAA000498), Mar 14, 2000: FRAME. CRACKED. DURING SCHEDULED D-CHECK, FOUND BS 727, FRAME CRACKED IN 3 PLACES LBL 37-RBL 45. REPAIRED FRAME PER SRM.
- [SDR SWAA000497](https://openairdocs.org/sdr/SWAA000497), Mar 14, 2000: STRINGER. CRACKED. DURING SCHEDULED D-CHECK, FOUND BS 663.75, STRINGERS 3L AND 9R CRACKED. REPAIRED STRINGERS PER SRM.
- [SDR SWAA000487](https://openairdocs.org/sdr/SWAA000487), Mar 13, 2000: FLOORBEAM. CORRODED. DURING SCHEDULED D CHECK, FOUND BS 707 FLOORBEAM CORRODED, LBL 17. REPAIRED BEAM PER SRM.
- [SDR SWAA000486](https://openairdocs.org/sdr/SWAA000486), Mar 13, 2000: FLOORBEAM. CORRODED. DURING SCHEDULED D CHECK, FOUND BS 1016 FLOORBEAM CORRODED, LBL 36-RBL 36. REPAIRED BEAM PER SRM.
- [SDR SWAA000469](https://openairdocs.org/sdr/SWAA000469), Mar 10, 2000: FRAME. CRACKED. DURING SCHEDULED D CHECK, FOUND BS 1156 AFT BULKHEAD CHORD CRACKED AT 8 O'CLOCK POSITION. REPAIRED CHORD SECTION PER SRM.
- [SDR SWAA000457](https://openairdocs.org/sdr/SWAA000457), Mar 9, 2000: FRAME. CRACKED. DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 360, RBL 62. REPAIRED FRAME PER SRM.
- [SDR SWAA000456](https://openairdocs.org/sdr/SWAA000456), Mar 9, 2000: FRAME. CORRODED. DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED, BS 227, RBL 41. REPAIRED FRAME PER SRM.
- [SDR SWAA000426](https://openairdocs.org/sdr/SWAA000426), Mar 6, 2000: FRAME. CORRODED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED, BS 1016, BETWEEN STRINGERS 26R-27R. REPAIRED FRAME PER SRM.
- [SDR SWAA000380](https://openairdocs.org/sdr/SWAA000380), Mar 1, 2000: STRINGER. CRACKED. DURING SCHEDULED D-CHECK, FOUND STRINGER 25L CRACKED, BS 381. REPAIRED STRINGER PER SRM.
- [SDR SWAA000379](https://openairdocs.org/sdr/SWAA000379), Mar 1, 2000: FRAME. CRACKED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED, BS 344, STRINGER 23L. REPAIRED FRAME PER SRM.
- [SDR SWAA000371](https://openairdocs.org/sdr/SWAA000371), Feb 29, 2000: FRAME. CRACKED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED, BS 1098, STRINGER 5L. REPAIRED FRAME PER SRM.
- [SDR SWAA000304](https://openairdocs.org/sdr/SWAA000304), Feb 18, 2000: CLIP. CRACKED. DURING SCHEDULED D-CHECK, FOUND 2 STRINGER CLIPS CRACKED, BS 727, STRINGER 14R, AND BS 727B, STRINGER 6R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.
- [SDR SWAA990783](https://openairdocs.org/sdr/SWAA990783), May 3, 1999: CONNECTOR. FAILED. INFLIGHT ENGINE SHUT DOWN, AIR RETURN WITH THE NR 1 ENGINE SHUT DOWN DUE TO START VALVE OPEN LIGHT ILLUMINATED. REMOVED AND REPLACED START VALVE AND OPEN LIGHT 
- [SDR SWAA990255](https://openairdocs.org/sdr/SWAA990255), Feb 13, 1999: LIGHT. INOP. DURING PREFLIGHT CHECK, FOUND CAPT OVERWING EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER BOEING M/M.
- [SDR SWAA990256](https://openairdocs.org/sdr/SWAA990256), Feb 12, 1999: LIGHT. INOP. DURING PREFLIGHT, FOUND CAPT SIDE OVERWING LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY.
- [SDR SWAA970645](https://openairdocs.org/sdr/SWAA970645), Jul 29, 1997: SKIN. CRACKED. DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED FWD OF BS 947, S24R. REPAIRED PER BOEING SRM.
- [SDR SWAA970524](https://openairdocs.org/sdr/SWAA970524), Jun 1, 1997: BATTERY. DISCHARGED. DURING SCHEDULED TERMINAL CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.
- [SDR SWAA970504](https://openairdocs.org/sdr/SWAA970504), May 27, 1997: BRACKET. BROKEN. AFTER TAKEOFF, NOTED LOUD NOISE FROM NOSE GEAR DURING RETRACTION. LOWERED GEAR AND RETURNED TO TPA AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND GEAR DOOR
- [SDR SWAA961240](https://openairdocs.org/sdr/SWAA961240), Nov 11, 1996: SLIDE. PRESS LOW. DURING WALKAROUND CHECK, FOUND FWD ENTRY DOOR SLIDE PRESSURE BELOW MINIMUM LIMITS. REPLACED SLIDE PER BOEING M/M.
- [SDR SWAA960781](https://openairdocs.org/sdr/SWAA960781), Aug 2, 1996: SKIN. CRACKED. DURING SCHEDULED SV CHECK, FOUND 2 CRACKS ALONG S24L AND BETWEEN BS 781-800. REPAIRED PER BOEING SRM.
- [SDR SWAA960453](https://openairdocs.org/sdr/SWAA960453), May 23, 1996: BATTERY PACK. DISCHARGED. DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE AFT ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK PER BOEING M/M.
- [SDR SWAA960217](https://openairdocs.org/sdr/SWAA960217), Apr 14, 1996: ANGLE. CRACKED. DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 302 AT S10L. REPLACED PER BOEING SRM.
- [SDR SWAA960216](https://openairdocs.org/sdr/SWAA960216), Apr 14, 1996: ANGLE. CRACKED. DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED FWD OF SERVICE DOOR AT BS 289 WL 248. REPLACED PER BOEING SRM.
- [SDR SWAA960215](https://openairdocs.org/sdr/SWAA960215), Apr 14, 1996: ANGLE. CRACKED. DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 294 RBL 55 WL 208. REPLACED PER BOEING SRM.
- [SDR SWAA960214](https://openairdocs.org/sdr/SWAA960214), Apr 14, 1996: FRAME. CRACKED. DURING SCHEDULED D-CHECK, FOUND LEFT FRAME CRACKED AT BS 349 WL 225. REPLACED FRAME CHORD PER BOEING SRM.
- [SDR SWAA960183](https://openairdocs.org/sdr/SWAA960183), Mar 22, 1996: SKIN. CRACKED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACK INDICATION AROUND FASTENER HEAD AT BS 178 WL 234 RBL 10. REPAIRED PER BOEING SRM.
- [SDR SWAA960182](https://openairdocs.org/sdr/SWAA960182), Mar 22, 1996: SKIN. CRACKED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 663 RBL 24 AND LBL 24 WL 201. REPAIRED PER BOEING SRM AND BOEING DRAWING 691A0032.
- [SDR SWAA960181](https://openairdocs.org/sdr/SWAA960181), Mar 22, 1996: WEB. CRACKED. DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 530, RBL 43 WL 161. REPAIRED PER BOEING SRM.
- [SDR SWAA960180](https://openairdocs.org/sdr/SWAA960180), Mar 22, 1996: BULKHEAD WEB. CRACKED. DURING SCHEDULED D-CHECK, FOUND 1.8 INCH CRACK AT BS 178 BULKHEAD PRESSURE WEB, LBL 11.3 WL 219. REPAIRED PER BOEING SRM.
- [SDR SWAA960179](https://openairdocs.org/sdr/SWAA960179), Mar 22, 1996: BULKHEAD WEB. CRACKED. DURING SCHEDULED D-CHECK, FOUND 2 INCH CRACK AT BS 178 BULKHEAD PRESSURE WEB, RBL 9.7 WL 219. REPAIRED PER BOEING SRM.
- [SDR SWAA960160](https://openairdocs.org/sdr/SWAA960160), Mar 18, 1996: SPLICE. CORRODED. DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT AFT BAY AT BS 907, S25L, LBL 21, WL 168. REPLACED SECTION PER BOEING SRM.
- [SDR SWAA960159](https://openairdocs.org/sdr/SWAA960159), Mar 18, 1996: FRAME. CRACKED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, RBL 55, BETWEEN S20R AND 21R. REPAIRED PER BOEING SRM.
- [SDR SWAA960158](https://openairdocs.org/sdr/SWAA960158), Mar 18, 1996: SKIN. CRACKED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 663, RBL 24 AND LBL 24. REPAIRED PER BOEING SRM.
- [SDR SWAA960157](https://openairdocs.org/sdr/SWAA960157), Mar 18, 1996: SUPPORT. CRACKED. DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 540, BL 0 TO LBL 25, WL 208. REPLACED PER BOEING SRM.
- [SDR SWAA960156](https://openairdocs.org/sdr/SWAA960156), Mar 18, 1996: BEAM. CRACKED. DURING SCHEDULED D-CHECK, FOUND INBOARD CREASE BEAM CRACKED AT BS 616, RBL 65, WL 208. REPAIRED PER BOEING SRM.
- [SDR SWAA960155](https://openairdocs.org/sdr/SWAA960155), Mar 18, 1996: WEB. CRACKED. DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 726, STRINGER 18A, RBL 61, WL 188.25. ALSO, AT BS 530, RBL 43, WL 161. REPAIRED PER BOEING SRM.
- [SDR SWAA960153](https://openairdocs.org/sdr/SWAA960153), Mar 18, 1996: BLKHD WEB. CRACKED. DURING SCHEDULED D-CHECK, FOUND BULKHEAD 178 PRESSURE WEB CRACKED AT RBL 9.7, WL 219. ALSO, AT LBL 11.3, WL 219. REPAIRED PER BOEING SRM.
- [SDR SWAA960152](https://openairdocs.org/sdr/SWAA960152), Mar 18, 1996: FLOOR BEAM. CORRODED. DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294, RBL 36 AND RBL 46, WL 208. ALSO, AT BS 328, RBL 15 AND 25, WL 208. REPAIRED PER BOEING SRM.

## Related

- Other Cessna TR182 aircraft: https://openairdocs.org/model/cessna-tr182/aircraft.md
- STCs for the Cessna TR182: https://openairdocs.org/model/cessna-tr182/stcs.md
- The Lycoming O-540-L3C5D engine: https://openairdocs.org/engine/lycoming-o-540-l3c5d.md

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