# N948CA: 2008 Cessna T182T

- Status: Valid registration
- Airframe: [Cessna T182T](https://openairdocs.org/model/cessna-t182t) (registry code 2072738, 4 seats)
- Engine: [Lycoming TIO-540-AK1A](https://openairdocs.org/engine/lycoming-tio-540-ak1a) (registry code 42005)
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13) (Textron Aviation Inc.), [TCDS E14EA](https://openairdocs.org/tcds/E14EA) (Lycoming Engines) (OpenAirDocs)
- Serial number: T18208892
- Year built: 2008
- Type: Fixed wing single engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: August 18, 2008
- Certificate issued: January 7, 2009
- Expires: April 30, 2029
- Mode S code: AD2B13
- Registered owner: [Civil Air Patrol](https://openairdocs.org/faa-owner/CIVIL%20AIR%20PATROL)
- Location: [Maxwell Afb, AL](https://openairdocs.org/faa-place/AL/Maxwell%20Afb)
- Owner type: Corporation
- Owner's area on the map: 32.3809° N, 86.3637° W: Placed by OpenAirDocs at the center of ZIP code 36112, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=948CA
- Page: https://openairdocs.org/aircraft/N948CA

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): 36 in force

### Matched by airframe (Cessna T182T)

- [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 or SA02658SE). Effective Mar 21, 2022
- [AD 2013-11-11](https://openairdocs.org/ad/2013-11-11): Engine Oil Pressure · Cessna 172R, 172S, 182S and 4 more. Effective Aug 1, 2013
- [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 2008-05-09](https://openairdocs.org/ad/2008-05-09): Crew seats · Cessna 172R, 172S, 182T and 3 more. Effective Apr 8, 2008
- [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 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 2007-08-03](https://openairdocs.org/ad/2007-08-03): Flexible fuel hoses · Cessna 172R, 172S, 182T and 3 more. Effective May 2, 2007
- [AD 2007-05-10](https://openairdocs.org/ad/2007-05-10): Steel lock rod/bar on both crew seat back cylinder lock assemblies · Cessna 172R, 172S, 182S and 4 more. Effective Apr 11, 2007
- [AD 2006-17-04](https://openairdocs.org/ad/2006-17-04): Flexible fuel hoses located in the engine compartment · Cessna 172R, 172S, 182T and 3 more. Effective Sep 1, 2006
- [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 2005-13-10](https://openairdocs.org/ad/2005-13-10): Main electrical power junction box circuit breakers · Cessna 172R, 172S, 182T and 3 more. Effective Aug 9, 2005
- [AD 2005-05-53 R1](https://openairdocs.org/ad/2005-05-53-R1): Flight control system · Cessna 172R, 172S, 182T and 1 more. Effective Mar 21, 2005
- [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 2004-15-18](https://openairdocs.org/ad/2004-15-18): Honeywell KAP 140 Autopilot Computer System · Cessna 172R, 172S, 182S and 4 more. Effective Sep 12, 2004
- [AD 98-14-03](https://openairdocs.org/ad/98-14-03): Transponders · Cessna 172, 172A, 172B and 230 more. Effective Aug 16, 1998

### Matched by engine (Lycoming TIO-540-AK1A)

- [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 2015-19-07](https://openairdocs.org/ad/2015-19-07): Fuel injector fuel lines · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1B and 187 more. Effective Nov 3, 2015
- [AD 2013-21-02](https://openairdocs.org/ad/2013-21-02): Turbochargers · Continental Motors LTSIO-360-RB, TSIO-360-MB, TSIO-360-RB and 2 more. Effective Nov 13, 2013
- [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 71-13-01 R1](https://openairdocs.org/ad/71-13-01-R1): Rescinding an airworthiness directive · Lycoming Engines TIO-540-A1A, TIO-540-A1B, TIO-540-A1C and 13 more. Effective Mar 8, 2012
- [AD 2012-03-06](https://openairdocs.org/ad/2012-03-06): Fuel servo diaphragm · Continental Motors 6-260-A, 6-285-A, 6-285-B and 482 more. Effective Feb 24, 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 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 2009-02-03](https://openairdocs.org/ad/2009-02-03): Fuel injection servos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 261 more. Effective Feb 9, 2009
- [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 2003-14-03](https://openairdocs.org/ad/2003-14-03): Rotary fuel pumps · Lycoming Engines AEIO-540-D4A5, AEIO-540-D4B5, AEIO-540-D4C5 and 262 more. Effective Aug 14, 2003
- [AD 97-15-11](https://openairdocs.org/ad/97-15-11): Cylinder kits · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 538 more. Effective Aug 12, 1997
- [AD 92-12-05](https://openairdocs.org/ad/92-12-05): Piston Pins · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 532 more. Effective Jul 10, 1992

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

- [AD 2005-05-53](https://openairdocs.org/ad/2005-05-53) (historical): Flight Control System · 172R, 172S, 182T and 1 more
- [AD 2003-24-13](https://openairdocs.org/ad/2003-24-13) (historical): Honeywell KAP 140 autopilot computer system · 172R, 172S, 182S and 4 more. Effective Jan 20, 2004
- [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 2012-24-09](https://openairdocs.org/ad/2012-24-09) (historical): Turbocharger turbine wheel · Continental Motors TSIO-360-MB, TSIO-360-RB, TSIO-360-SB and 1 more. Effective Dec 20, 2012
- [AD 2011-26-04](https://openairdocs.org/ad/2011-26-04) (historical): Externally mounted fuel injector fuel lines · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1B and 186 more. Effective Jan 25, 2012
- [AD 2011-15-10](https://openairdocs.org/ad/2011-15-10) (historical): Fuel servos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 256 more. Effective Aug 16, 2011
- [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 2008-14-07](https://openairdocs.org/ad/2008-14-07) (historical): Externally mounted fuel injector fuel lines · Textron Lycoming, AVCO AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1B and 185 more. Effective Aug 14, 2008
- [AD 2008-08-14](https://openairdocs.org/ad/2008-08-14) (historical): Fuel injection servo plugs · Superior Air Parts AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 242 more. Effective Apr 29, 2008
- [AD 2008-06-51](https://openairdocs.org/ad/2008-06-51) (historical): Fuel injection servo plugs · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 235 more
- [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 2002-26-01](https://openairdocs.org/ad/2002-26-01) (historical): Fuel injector fuel lines · Textron Lycoming, AVCO IGO-480-A1B6, IGO-540-B1A, IGO-540-B1C and 178 more. Effective Jan 31, 2003
- [AD 2002-23-06](https://openairdocs.org/ad/2002-23-06) (historical): Crankshaft gear retaining bolts · Textron Lycoming, AVCO AEIO-540, AEIO-540-D4A5, AEIO-540-D4B5 and 46 more. Effective Nov 19, 2002
- [AD 2002-20-51](https://openairdocs.org/ad/2002-20-51) (historical): Crankshaft gear retaining bolts · Textron Lycoming, AVCO AEIO-540, IO-540 Series (all), LTIO-540-F2BD and 39 more
- [AD 2002-17-53](https://openairdocs.org/ad/2002-17-53) (historical): Crankshaft · Lycoming Engines LTIO-540-F2BD, LTIO-540-J2B, LTIO-540-J2BD and 36 more

## Information bulletins (advisory) (13 in force)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-12-41](https://openairdocs.org/saib/CE-12-41): Flight Controls  Loose Glide Screw. Issued Aug 9, 2012
- [SAIB CE-12-15](https://openairdocs.org/saib/CE-12-15): DC Power Distribution System - Avionics Master Switch. Issued Jan 30, 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-09-12](https://openairdocs.org/saib/CE-09-12): Navigation: CRS/BARO Knob Interference in some G1000/G900X/G950 Installations. Issued Feb 11, 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 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-09-04](https://openairdocs.org/saib/NE-09-04): Fuel Control/Reciprocating Engines. Issued Jan 10, 2009
- [SAIB NE-06-32R1](https://openairdocs.org/saib/NE-06-32R1): Reciprocating Engine - Crankshaft. Issued Sep 10, 2008
- [SAIB CE-19-01](https://openairdocs.org/saib/CE-19-01) (historical): Engine Oil and Airplane Hour Meter; Pressure Switch Failure. Issued Feb 12, 2019
- [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 N948CA.

## FAA accident and incident reports

None matched to N948CA.

## 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 N948CA not matched to an aircraft (67, newest 50)

They name N948CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR COMA0160879](https://openairdocs.org/sdr/COMA0160879), Nov 7, 2001: WEB. CHAFED. THE AFT PRESSURE BULKHEAD HAS A HOLE WORN IN THE WEB STRUCTURE FROM A FASTENER THAT PROTRUDED BEYOND THE CARGO LINER INSTALLATION.PERFORMED A MAJOR REPAIR TO 62
- [SDR COMA0160878](https://openairdocs.org/sdr/COMA0160878), Nov 7, 2001: WEB. CRACKED. L/H ENGINE SUPPORT BEAM I/B FORWARD CORNER CRACKEDPERFORMED A MAJOR REPAIR TO L/H ENGINE SUPPORT BEAM I/A/W CRJ REO 601R-53-61-366 REV C AND WVAC EO 601R-33-282
- [SDR COMA0160876](https://openairdocs.org/sdr/COMA0160876), Nov 7, 2001: WEB. CRACKED. R/H ENGINE SUPPORT BEAM I/B FORWARD CORNER CRACKED.PERFORMED A MAJOR REPAIR TO R/II ENGINE SUPPORT BEAM I/A/W CRJ REO 601R-53-61-366 REV C.
- [SDR COMA0160810](https://openairdocs.org/sdr/COMA0160810), Oct 13, 2001: ACTUATOR. FAULTY. FLIGHT 5555. DURING APPROACH INTO CRW, RECEIVED A FLAP FAIL CAUTION WITH FLAP POSITION AT 26 DEGREES. CREW DECLARED AN EMERGENCY AND LANDED SAFELY.REPLACED RIGH
- [SDR COMA0160809](https://openairdocs.org/sdr/COMA0160809), Oct 13, 2001: ACTUATOR. FAULTY. FLIGHT 5555. DURING APPROACH INTO CRW, RECEIVED A FLAP FAIL CAUTION WITH FLAP POSITION AT 26 DEGREES. CREW DECLARED AN EMERGENCY AND LANDED SAFELY.REPLACED LEFT
- [SDR COMA0160789](https://openairdocs.org/sdr/COMA0160789), Oct 8, 2001: BPSU. MALFUNCTIONED. FLIGHT #5431. FLAPS FAILED AT 39 DEGREES.REPLACED THE L/H BPSU.
- [SDR COMA0160787](https://openairdocs.org/sdr/COMA0160787), Oct 7, 2001: FLAP. FAILED. FLIGHT 5234 - FLAPS FAILED AT 30 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. A/C CONTINUED SERVICE.
- [SDR COMA0160697](https://openairdocs.org/sdr/COMA0160697), Sep 8, 2001: ANGLE. CRACKED. INTERCOSTAL FLANGES AT BL36 AND ANGLES AT BL27 LEFT AND RIGHT SIDES ARE CRACKED.REPAIRED ANGLE AND INTERCOSTAL AT FS484 I/A/W WVAC EO 601R-53-2701.
- [SDR COMA0160696](https://openairdocs.org/sdr/COMA0160696), Sep 8, 2001: ANGLE. CRACKED. PERFORMED A MAJOR REPAIR TO THE L/H AND R/H VERTICAL J-ANGLES AT F.S. 280, BL 9.0 L/H AND R/H BY REMOVING THE CRACKED ANGLES AND INSTALLING FABRICATED ANGLES I/
- [SDR COMA0160170](https://openairdocs.org/sdr/COMA0160170), Jan 26, 2001: COMPUTER. MALFUNCTIONED. STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER.
- [SDR COMA0160008](https://openairdocs.org/sdr/COMA0160008), Dec 21, 2000: CONTROL UNIT. MALFUNCTIONED. CONFIG SPOILERS WARNING DURING REJECTED T/O.COULD NOT DUPLICATE, SPOILER SYSTEM FUNCTION CHECK WAS NORMAL.
- [SDR COMA0061038](https://openairdocs.org/sdr/COMA0061038), Dec 11, 2000: PLATE. WORN. CABIN DOOR WARNING. REPLACED THE INNER DOOR HANDLE CAM PLATE.
- [SDR COMA0061022](https://openairdocs.org/sdr/COMA0061022), Dec 8, 2000: LATCH. OUT OF ADJ. CABIN DOOR LATCH CAUTION MESSAGE. ADJUSTED DOOR LATCH MECHANISM.
- [SDR COMA0060944](https://openairdocs.org/sdr/COMA0060944), Nov 20, 2000: COMPUTER. MALFUNCTIONED. STALL FAIL MESSAGE DURING T/O. RESET STALL COMPUTER.
- [SDR COMA0060919](https://openairdocs.org/sdr/COMA0060919), Nov 13, 2000: SENSOR. MALFUNCTIONED. LANDING GEAR DISAGREE MESSAGE. NOSE LANDING GEAR PROXIMITY SENSOR WAS DAMAGED BY GROUND HANDLING TECHNIQUE. ADJUSTED THE NLG PROXIMITY SENSOR.
- [SDR COMA0060891](https://openairdocs.org/sdr/COMA0060891), Nov 6, 2000: IDG. LOW. RT IDG CAUTION MESSAGE. SERVICED IDG WITH OIL TO PROPER LEVEL.
- [SDR COMA0060769](https://openairdocs.org/sdr/COMA0060769), Sep 28, 2000: LIGHT. INOPERATIVE. FWD FLOOR LEVEL EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT STRIP.
- [SDR COMA0060746](https://openairdocs.org/sdr/COMA0060746), Sep 17, 2000: PLATE. MISMANUFACTURED. TWO SPLICE PLATES (P/N 601R31030-77) FABRICATED INCORRECTLY BY THE MANUFACTURER. FABRICATED A NEW DOUBLER PLATE IAW WVAC EO 601R-53-1698.
- [SDR COMA0060630](https://openairdocs.org/sdr/COMA0060630), Aug 8, 2000: LIGHT. INOPERATIVE. EMERGENCY FLOOR LIGHTING BETWEEN ROWS 2 THRU 5 IS INOPERABLE. SECURED ELECTRICAL CONNECTION, SYSTEM TEST NORMAL.
- [SDR COMA0060373](https://openairdocs.org/sdr/COMA0060373), Apr 24, 2000: TRANSPONDER. FAILED. NR 2 TRANSPONDER FAILED. DEFERRED THE NR 2 TRANSPONDER PER MEL.
- [SDR COMA0060358](https://openairdocs.org/sdr/COMA0060358), Apr 20, 2000: WARNING SYSTEM. ACTIVATED. FLIGHT SPOILER FAULT MESSAGE. RESET THE SECU CIRCUIT BREAKERS. SYSTEM TEST NORMAL. COULD NOT DUPLICATE.
- [SDR COMA0060286](https://openairdocs.org/sdr/COMA0060286), Mar 24, 2000: HARNESS. DEFECTIVE. RIGHT HAND ENGINE N1 FLUCTUATES. REPLACED THE ENGINE BROWN WIRE HARNESS.
- [SDR COMA0060265](https://openairdocs.org/sdr/COMA0060265), Mar 14, 2000: WARNING SYSTEM. ACTIVATED. ANTI-SKID CAUTION MESSAGE WHEN GEAR SELECTED DOWN. COULD NOT DUPLICATE. NO FAULT CODES IN COMPUTER. AIRCRAFT RETURNED TO SERVICE.
- [SDR COMA0060232](https://openairdocs.org/sdr/COMA0060232), Mar 2, 2000: EEC. MALFUNCTIONED. RIGHT ENGINE N1 DROPPED FROM 87 PERCENT TO 78 PERCENT. DEFERRED THE ENGINE ELECTRONIC CONTROL SYSTEM PER MEL.
- [SDR COMA0060231](https://openairdocs.org/sdr/COMA0060231), Mar 2, 2000: WIRE. BROKEN. EMERGENCY EXIT LIGHT AT ROW 5 IS INOPERABLE. REPLACED POWER WIRE.
- [SDR COMA0060207](https://openairdocs.org/sdr/COMA0060207), Feb 26, 2000: SKIN PANEL. CRACKED. 5 LEFT LOWER WING ACCESS HOLES CRACKED, 540-EB - WS 116.366, 540 FB - WS 136.676, 550AB - WS 163.000, 550DB-WS 280.415, AND 550 GB - WS 294.048. REPAIRED DAMAGE
- [SDR COMA0060090](https://openairdocs.org/sdr/COMA0060090), Jan 24, 2000: ACTUATOR. MALFUNCTIONED. GEAR DISAGREE, LEFT MLG DID NOT RETRACT. COULD NOT DUPLICATE, REPLACED THE SIDE STAY ACTUATOR.
- [SDR COMA0060079](https://openairdocs.org/sdr/COMA0060079), Jan 20, 2000: ANGLE. CRACKED. ANGLE AT FS 280 AT LBL9 OUTBOARD SIDE IS CRACKED P/N 601R31113-57. INSTALLED NEW CLIP P/N 601R31113-57 IAW CRJ SRM 51-42-21 AND WVAC EO 601R-53-0868.
- [SDR COMA0060077](https://openairdocs.org/sdr/COMA0060077), Jan 20, 2000: WEB. DAMAGED. WEB ASSY AT FS 349.00 TO 364 HAS DAMAGED ON LBL 9. FABRICATED NEW WEB FROM 2024T3 .032, INSTALLED NEW WEB IAW WVAC EO 601R-53-0862.
- [SDR COMA0060075](https://openairdocs.org/sdr/COMA0060075), Jan 20, 2000: SKIN. DAMAGED. WHILE COMPLYING WITH S/B 601R-53-050 INSTALLATION OF AN EXTERNAL REINFORCING STRAP FOUND FOUR HOLES BIRLLED THROUGH THE SKIN AND FRAME AT FS 409 AND 128 BETWEEN
- [SDR COMA0060074](https://openairdocs.org/sdr/COMA0060074), Jan 20, 2000: SILL. CORRODED. INTERCOSTAL AT RBL 42 BETWEEN 349 - FS 360 IS CORRODED. REMOVED CORROSION ON INTERCOSTAL AND INSTALLED REINFORCING ANBLE IAW WVAC EO601R-53-0880A.
- [SDR COMA0060073](https://openairdocs.org/sdr/COMA0060073), Jan 20, 2000: FRAME. CRACKED. FRAME 280 IS CRACKED OUTBOARD OF RBL 9, APROXIMATELY .25 CRACK. FLOOR MEMBER P/N 600-34017-17 AT FS 280 REPAIRED IAW WVAC EO NO 601R-53-0869.
- [SDR COMA0060080](https://openairdocs.org/sdr/COMA0060080), Jan 19, 2000: FRAME. DAMAGED. WHILE ACCOMPLISHING CANADAIR SERVICE BULLETIN 601R-53-030, FOUR FASTENER HOLES DRILLED THROUGH THE SKIN AND FRAME AT FS 409 AND 128, BETWEEN STRINGER 24L AND 24
- [SDR COMA0060067](https://openairdocs.org/sdr/COMA0060067), Jan 18, 2000: ANGLE. CORRODED. SERVICE DOOR ANGLE IS CORRODED AT FS 317 TO FS 342.0 P/N 601R38303-105. REMOVED CORRODED ANGLE AND REPLACED WITH NEW ANGLE IAW WVAC EO 601R-53-0865.
- [SDR COMA0060066](https://openairdocs.org/sdr/COMA0060066), Jan 18, 2000: FLOORBEAM. CORRODED. TOP OF FLOORBEAM CAPS LBL9 AT FS 280 TO FS 409.0 RBL9 AT FS 280 TO FS 409.0 AND RBL 27 AT FS 280 TO FS 349 CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOORBEA
- [SDR COMA0060065](https://openairdocs.org/sdr/COMA0060065), Jan 18, 2000: PLATE. CORRODED. TOP PLATES OUTBOARD OF LBL 27, LBL9, RBL 9 AND RBL 27FS 349.0 CORRODED. REMOVED AND INSTALLED NEW TOP PLATES IAW WVAC EO 601R-53-0866.
- [SDR COMA0060064](https://openairdocs.org/sdr/COMA0060064), Jan 18, 2000: WEB. DAMAGED. WEB ASSY AT FS 349.0 TO 364.0 HAS DAMAGED HOLE ON LBL.9. INSTALLED NEW WEBW WVAC EO 601R-53-0862.
- [SDR COMA0060062](https://openairdocs.org/sdr/COMA0060062), Jan 17, 2000: FRAME. CRACKED. FRAME FS 718.00 STR 11-12 CRACKED IN RADIUS LHS. REPAIRED PER CANADAIR REO 601R-53-61-193A.
- [SDR COMA0060061](https://openairdocs.org/sdr/COMA0060061), Jan 17, 2000: FRAME. CRACKED. AFT DOUBLER OF FRAME FS 718.00 STR 11-12 RHS CRACKED. REPLACED PER CANADAIR REO 601R-53-61-193A.
- [SDR COMA0060060](https://openairdocs.org/sdr/COMA0060060), Jan 17, 2000: FRAME. CRACKED. FRAME FS 718.00 STR 11-12 RHS CRACKED IN RADIUS. REPAIRED PER CANADAIR REO 601R-53-61-192A.
- [SDR COMA0060059](https://openairdocs.org/sdr/COMA0060059), Jan 17, 2000: FRAME. CRACKED. AFT DOUBLER OF FRAME FS 718.00, STR 11-12 LHS CRACKED. REPLACED PER CANADAIR REO 601R-53-61-193A.
- [SDR COMA9960764](https://openairdocs.org/sdr/COMA9960764), Dec 14, 1999: FILTER. CLOGGED. RIGHT HAND ENGINE OIL PRESSURE AT 130 PSI. REPLACED CLOGGED OIL FILTER, AND CLEANED THE OIL PUMP SCAVENGE SCREENS.
- [SDR COMA9960759](https://openairdocs.org/sdr/COMA9960759), Dec 10, 1999: WINDOW HEAT. INOPERATIVE. LEFT WINDOW HEAT INOPERABLE. SWITCHED WIRE TERMINALS TO THE BACK UP TERMINAL BLOCK, OPERATIONAL CHECK NORMAL.
- [SDR COMA9960548](https://openairdocs.org/sdr/COMA9960548), Sep 19, 1999: INTERCOSTAL. MISDRILLED. HOLES FOR A CANNON PLUG MOUNTING BRACKET WERE INCORRECTLY LOCATED ON THE INTERCOSTAL BETWEEN FS 217.75 AND FS 226 AT RBL 12 DURING ACCOMPLISHMENT OF COMAIR EO 6
- [SDR COMA9960547](https://openairdocs.org/sdr/COMA9960547), Sep 18, 1999: DOUBLER. CRACKED. DOUBLER PLATE (P/N 600-31068-19) AT RBL 9 AT 461.00 CRACKED. REPLACED DOUBLER PLATE FOR RBL 9 AT FS 461.00 IAW WVAC EO 601R-53-0342.
- [SDR COMA9960362](https://openairdocs.org/sdr/COMA9960362), Jul 12, 1999: SMOKE DETECTOR. MALFUNCTIONED. CARGO SMOKE WARNING. REPLACED THE CARGO SMOKE DETECTOR.
- [SDR COMA9960148](https://openairdocs.org/sdr/COMA9960148), Apr 7, 1999: CONNECTOR. DEFECTIVE. EMERGENCY FLOOR LIGHTING, AFT SECTION, IS INOPERABLE. REPLACED WIRE CONNECTOR.
- [SDR COMA9860337](https://openairdocs.org/sdr/COMA9860337), Nov 8, 1998: TR UNIT. MALFUNCTIONED. LEFT THRUST REVERSER MESSAGE DURING TAKEOFF. DEFERRED LEFT HAND THRUST REVERSER.
- [SDR COMA9860289](https://openairdocs.org/sdr/COMA9860289), Oct 1, 1998: PUMP. FAILED. RIGHT HAND HYDRAULIC PUMP FAILED. REPLACED THE RIGHT HAND ENGINE DRIVEN HYDRAULIC PUMP.
- [SDR COMA9860208](https://openairdocs.org/sdr/COMA9860208), Jul 29, 1998: LIGHT. INOPERATIVE. SEVERAL SECTIONS OF EMERGENCY FLOOR LIGHTING ARE INOPERABLE. REPLACED TWO SECTIONS OF FLOOR TRACK LIGHTING.

All 67: https://openairdocs.org/aircraft/N948CA/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (325, 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 T182T)

- [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 SA01844WI](https://openairdocs.org/stc/SA01844WI): Installation of Garmin GFC 600 Automatic Flight Control System. Garmin International Inc
- [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 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 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 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 SA01120SE](https://openairdocs.org/stc/SA01120SE): Installation of Door Steward. Mountain View 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 SA02006CH](https://openairdocs.org/stc/SA02006CH): Installation of air conditioning system. Kelly Aerospace Thermal Systems LLC
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA01105DE](https://openairdocs.org/stc/SA01105DE): Installation of the Persistent Systems MPU5 Wave Radio System. Persistent Systems
- [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International 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 SA00673DE](https://openairdocs.org/stc/SA00673DE): Installation of B&C Specialty Standby Alternator System. Freedom Aviation Inc
- [STC SA01552WI](https://openairdocs.org/stc/SA01552WI): Installation of Supplemental Audio System, including #2 GMA 1347 Audio Panel. Yingling Aircraft Inc
- [STC SA04586CH](https://openairdocs.org/stc/SA04586CH): Installation of Electroair Back Up Battery Panel System Control. Electroair Aquisition Corp
- [STC SA950CE](https://openairdocs.org/stc/SA950CE): Installation STOL kits (wing leading edge cuffs, drooped tips, stall fences and aileron gap seals). Curry Aviation LLC
- [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA01830WI](https://openairdocs.org/stc/SA01830WI): G1000 Integrated Avionics System hardware and software updates including optional Flight Stream 510. Textron Aviation Inc
- [STC SA00753WI](https://openairdocs.org/stc/SA00753WI): Installation of the Concorde VRSLA (RG-24-15, RG-24-16, RG-35AXC and RG-35A) batteries. Aero-Mach Wilco LLC
- [STC SA01827WI](https://openairdocs.org/stc/SA01827WI): Installation of LED Position Lights. Aero-Mach Wilco 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 SA00026IB](https://openairdocs.org/stc/SA00026IB): Validation for the Installation of Beringer Wheels, axles, brake and master-cylinders. Beringer Aero
- [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 SA02553AK](https://openairdocs.org/stc/SA02553AK): Fabrication and installation of a Tail Wheel Anti-Shimmy Dampener. Keller Engineering Group LLC
- [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King)

All 325: https://openairdocs.org/aircraft/N948CA/stcs.md

## Related

- Other Cessna T182T aircraft: https://openairdocs.org/model/cessna-t182t/aircraft.md
- The Lycoming TIO-540-AK1A engine: https://openairdocs.org/engine/lycoming-tio-540-ak1a.md

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