# Service difficulty reports: Cessna TR182 A list on [Cessna TR182](https://openairdocs.org/model/cessna-tr182.md). Newest first. General aviation reporting is voluntary. Page 1 of 3 · 111 reports - [SDR 2026FA0000636](https://openairdocs.org/sdr/2026FA0000636.md): Pivot Assy · sheared · Aug 11, 2026 · N2194S · Cessna TR182 · Main Landing Gear > LEFT MAIN LANDING GEAR COLLAPSED AFTER LANDING, THEN ROLLING OUT 2000' AT THE START OF A RIGHT TURN ONTO A TAXIWAY. WHEN AIRCRAFT WAS JACKED FOR TESTING, THE GEAR WOULD RELEASE FROM EITHER THE UP/LOCKED OR DOWN/LOCKED POSITION BUT WOULD NOT CONTINUE TO THE POS - [SDR 2026FA0000434](https://openairdocs.org/sdr/2026FA0000434.md): Volt Regulator · abnormal · May 27, 2026 · N738JZ · Cessna TR182 · Electrical Connectors > WHILE AT CRUISE FLIGHT MULTIPLE AVIONICS AND INSTRUMENTATION FAILED. THE PILOT MADE AN UNSCHEDULED LANDING AT THE NEAREST SUITABLE AIRPORT. - [SDR 2020FA0000300](https://openairdocs.org/sdr/2020FA0000300.md): Bearing Cap · failed · May 8, 2020 · N73VX · Cessna TR182 · Landing Gear Actuator > NOSE LANDING GEAR COLLAPSED ON LANDING. NOSE LANDING GEAR ACTUATOR END BEARING FAILED. FAILURE OCCURRED IN END BEARING, LOWER CASTING BROKE AWAY AT DOWN LOCK PIN RETAINER YOKE ON LEFT AND RIGHT SIDES OF YOKE ALLOWING DOWN LOCK PINS TO DISLODGE, SHEAR AND FA - [SDR 8SCA201906040001](https://openairdocs.org/sdr/8SCA201906040001.md): Lifter · faulty · Dec 30, 2018 · N705R · Cessna TR182 · Reciprocating Engine Power Section > AT ANNUAL INSPECTION MECHANIC NOTED THAT IT WAS DIFFICULT TO REACH FULL RPM FOR STATIC GROUND RUN UNTIL TURBO ENGAGED. AFTER INSPECTING THE ENGINE IT WAS FOUND THAT ALL. 12 LIFTERS WERE COLLAPSING AND ROCKER ARM CLEARANCE WAS BEYOND LIMITS. THE ENGINE WAS TORN - [SDR 2018FA0000237](https://openairdocs.org/sdr/2018FA0000237.md): Landing Gear · damaged · Jul 16, 2018 · Cessna TR182 · Nose/Tail Landing Gear > AIRCRAFT SUFFERED NOSE GEAR UP LANDING UNABLE TO ID SPECIFIC CAUSE HOWEVER MECHANICAL INTERFERENCE PERMITTED GEAR DOOR FROM OPENING. AIRCRAFT SUSTAIN MINIMAL DAMAGE AND STILL IN WORK. - [SDR 2018FA0000233](https://openairdocs.org/sdr/2018FA0000233.md): Door · inoperative · Jul 16, 2018 · N182FB · Cessna TR182 · Landing Gear Door Retract Section > AIRCRAFT SUFFERED NOSE GEAR UP LANDING UNABLE TO ID SPECIFIC CAUSE HOWEVER MECHANICAL INTERFERENCE PREVENT GEAR DOOR FROM OPENING DURING LANDING.AIRCRAFT SUSTAINED MINIMAL DAMAGE, AIRCRAFT IS IN PROCESS OF REPAIR. - [SDR 2017FA0000412](https://openairdocs.org/sdr/2017FA0000412.md): Oil Cooler · vapor lock · Nov 9, 2016 · N5153R · Cessna TR182 · Engine Oil Cooler > AFTER FACTORY REMANUFACTURED, INSTALLED THE ENGINE, FOUND THE TURBO LEAKING FROM CENTER SECTION DURING IDLE, BUT NOT ABOVE 1000 RPM. TROUBLESHOT OIL LEAK AND DETERMINED OIL COOLER VAPOR LOCK CAUSING TURBO LEAK. BLEEDING AIR FROM COOLER DID STOP THE OIL LEAK, - [SDR MAMR2015FA0000607](https://openairdocs.org/sdr/MAMR2015FA0000607.md): Check Valve · broken · Oct 29, 2015 · Cessna TR182 · Exhaust Turbocharger > TURBOCHARGER: PN 465292-9002, SN ZKNOO210. TURBOCHARGER HAS SUFFERED A LACK OF LUBRICATION CONDITION DURING OPERATION THAT HAS SEVERELY DAMAGED IT. THERE IS EVIDENCE OF OIL LEAKING INTO THE COMPRESSOR HOUSING. THE MAIN BEARINGS AND THRUST SYSTEM HAVE BEEN S - [SDR NF2D2015FA0000205](https://openairdocs.org/sdr/NF2D2015FA0000205.md): Clamp · failed · Apr 26, 2015 · N423DK · Cessna TR182 · Exhaust Turbocharger > THE TURBOCHARGER WAS REPLACED, THE EXHAUST CLAMPS WERE INSPECTED AND REUSED AND THE ACFT RETURNED TO SERVICE. THE ACFT DEPARTED FOR ITS HOME AIRPORT WHERE UPON INSPECTION AFTER LANDING, IT WAS FOUND THA THE CLAMP HOLDINGTHE EXHAUST PIPE TO THE TURBOCHARGER HA - [SDR 2012FA0000170](https://openairdocs.org/sdr/2012FA0000170.md): Carburetor · failed · Mar 25, 2012 · N756KS · Cessna TR182 · Fuel Control/Reciprocating Engines > INSTALLED O/H HA-6 CARBURETOR, ON GROUND RUNS NOTED ENGINE EXTREMLY ROUGH AT POWER SETTING ABOVE 1400 RPM, STRONG ODOR OF FUEL AND BLACK SMOKE FROM EXHAUST. USE OF MIXTURE CONTROL AT 1400 RPM GAVE 200 RPM RISE AND CLEARED CONDITION. UNABLE TO REACH TAKEOFF R - [SDR CA111025009](https://openairdocs.org/sdr/CA111025009.md): Exhaust Duct · warped · Oct 25, 2011 · Cessna TR182 · Engine Collector/Tailpipe/Nozzle > (CAN) ALL EXHAUST FLANGE JOINTS WARPED. - [SDR CA101130010](https://openairdocs.org/sdr/CA101130010.md): Compressor Wheel · damaged · Nov 26, 2010 · Cessna TR182 · Exhaust Turbocharger > COMPRESSOR WHEEL OF TURBO CHARGER WAS FOUND DAMAGED AND SEIZED BY DEBRIS. UPON DISASSEMBLY, A SMALL PIECE OF A BAND (BREEZE TYPE) CLAMP WAS FOUND BETWEEN THE COMPRESSOR WHEEL AND THE HOUSING PREVENTING THE WHEEL FROM TURNING. THE LAST SERVICE ON THIS AIRCRAF - [SDR 2010FA0001172](https://openairdocs.org/sdr/2010FA0001172.md): Ignition Switch · inoperative · Oct 21, 2010 · N182SP · Cessna TR182 · Ignition Switching > ACFT LOST ELECTRICAL POWER DURING LANDING, PILOT IN COMMAND NOTICED THE GEAR WAS NOT LOCKED IN THE DOWN POSITION AND DID A GO AROUND. PILOT HAND PUMPED THE GEAR DOWN AND LANDED THE ACFT WITH ANY PROBLEMS. AFTER TROUBLESHOOTING, FOUND THAT THE STARTER AND STA - [SDR 2010FA0000475](https://openairdocs.org/sdr/2010FA0000475.md): Actuator · malfunctioned · Mar 26, 2010 · N757PE · Cessna TR182 · Landing Gear Actuator > ACFT LANDED WITH RT MAIN GEAR NOT DOWN AND LOCKED. FOUND POWER PAC WITH NO HYD FLUID IN IT. FLUID LOSS CAUSED BY NOSE GEAR ACTUATOR LEAK. WHILE INSP PARTS, FOUND O-RING ON PISTON SHAFT DAMAGED AND BACKUP RING BROKEN. ALSO, PISTON SHAFT PN 1280241-2 AND BEA - [SDR 2009FA0000966](https://openairdocs.org/sdr/2009FA0000966.md): Cylinder Head · damaged · Aug 27, 2009 · N756RW · Cessna TR182 · Reciprocating Engine Cylinder Section > AN INFLIGHT CYL HEAD SEPARATION OF PN 65098, SN 85550-05 CYLINDER RESULTED IN A LOSS OF ENGINE OIL AND AN EMERGENCY LANDING. (K) - [SDR 2007FA0000055](https://openairdocs.org/sdr/2007FA0000055.md): Hydraulic Line · failed · Dec 12, 2006 · N5091S · Cessna TR182 · Hydraulic System, Main > HYDRAULIC HOSE ON RETRACT SIDE OF NOSE GEAR ACTUATOR FAILED AS AIRCRAT WAS ON APPROACH AND GEARDOWN WAS SELECTED. RESULTED IN AIRCRAFT MAKING AN EMERGENCY GEARUP LANDING. AFTER AC WAS RECOVERED, INSPECTION OF HYDRAULIC SYSTEM REVEALED; TEFLON HYDRAULIC HOSE - [SDR BG001](https://openairdocs.org/sdr/BG001.md): Line · failed · Oct 6, 2005 · N2426S · Cessna TR182 · Hydraulic System, Main > DOWN HYDRAULIC PRESSURE LINE FAILED AT ACTUATOR. LINE PULLED OUT OF SWAGED END FITTING. - [SDR SD92005F00000](https://openairdocs.org/sdr/SD92005F00000.md): Line · inoperative · Jun 22, 2005 · N851DE · Cessna TR182 · Landing Gear Brake System > PILOT REPORTED LT BRAKE INOPERATIVE ON LANDING. INSP OF AIRCRAFT FOUND LOW HYDRAULIC FLUID LEVEL IN LT MASTER CYLINDER. AFTER SERVICING BRAKES AND CHECKING SYSTEM, FOUND B-NUT ON LT BRAKE CALIPER TO BE SLIGHTLY LOOSE. THIGHT END BRAKE LINE, CLEANED AREA AND - [SDR 2005FA0000959](https://openairdocs.org/sdr/2005FA0000959.md): Drive Assy · failed · Jun 21, 2005 · N6317T · Cessna TR182 · Engine Starter > INSTALLED FACTORY OVERHAULED ENGINE ONTO AIRCRAFT. THE STARTER BENDIX WAS ENGAGED WHEN ENGINE WAS INSTALLED. AFTER FIRST START THE STARTER WOULD SPIN BUT BENDIX WOULD NOT RE-ENGAGE STARTER RING GEAR ON ENGINE. REPLAED WITH OVERHAULED SPACE STARTER (SN E1230 - [SDR 2005FA0000515](https://openairdocs.org/sdr/2005FA0000515.md): Check Valve · inoperative · Mar 15, 2005 · N1898X · Cessna TR182 · Exhaust Turbocharger > OIL LEAKING OUT OF TURBO CHARGER AFTER ENGINE SHUTDOWN, ENGINE HAD NOT BEEN RUN SINCE CHECK VALVE HAD BEEN INSTALLED. REMOVED OIL PRESSURE CHECK VALVE FOR INSPECTION, AND NOTED LOOSE NUT, TOTALLY SEPARATED INSIDE THE CHECK VALVE. THIS OBVIOUSLY WAS THAT WAY - [SDR 2005FA0000262](https://openairdocs.org/sdr/2005FA0000262.md): Rib · cracked · Oct 4, 2004 · N210BB · Cessna TR182 · Trailing Edge Flaps > LT WING IB FLAP TRACK RIB ASSY, PN 1221010-15, HAS 2 BRACKETS RIVETED TO EITHER SIDE OF IT TO ATTACH FLAP TRACK RIB ASSY TO WING LOWER IB T/E SKIN, REF TO AS FLAP WELL SKIN) PN 0720601-101. ONE OF BRACKETS HAD CRACKED ALLOWING BRACKET TO TWIST SLIGHTLY, DECRE - [SDR CA040927008](https://openairdocs.org/sdr/CA040927008.md): Pivot Assy · cracked · Sep 27, 2004 · Cessna TR182 · Brake > (CAN) RT BRAKE CONTINUALLY LOOSING FLUID. CENTER SECTION AT GEAR PIVOTS ALWAYS WET. BRAKE SWIVEL NOT LEAKING. PIVOT ASSEMBLY REMOVED AND CHECKED BY DYE PENETRATE INSPECTION FOUND TO BE CRACKED. INSTALLED NEW PIVOT ASSEMBLY IAW MAINTENANCE MANUAL. - [SDR 2688200410001](https://openairdocs.org/sdr/2688200410001.md): Crossover Tube · cracked · Sep 3, 2004 · N5091T · Cessna TR182 · Engine Exhaust System > DURING ANNUAL INSPECTION, DISCOVERED CRACK APPROXIMATELY 1.5 INCHES IN LENGTH AROUND THE LT CROSSOVER ASSEMBLY (PN 2254008). UPON REMOVAL, ALSO FOUND DETERIORATION IN THE SLIP JOINT CONNECTING THE RT CROSSOVER ASSEMBLY (PN 2254013). REPLACED BOTH PARTS WITH - [SDR 2688200400001](https://openairdocs.org/sdr/2688200400001.md): Crossover Tube · cracked · Sep 3, 2004 · N5091T · Cessna TR182 · Engine Exhaust System > DURING ANNUAL INSPECTION, DISCOVERED CRACK APPROXIMATELY 1.5 INCHES IN LENGTH AROUND THE LT CROSSOVER ASSEMBLY (PN 2254008). UPON REMOVAL, ALSO FOUND DETERIORATION IN THE SLIP JOINT CONNECTING THE RT CROSSOVER ASSEMBLY (PN 2254013). REPLACED BOTH PARTS WITH - [SDR 2689200410001](https://openairdocs.org/sdr/2689200410001.md): Crossover Tube · cracked · Sep 2, 2004 · N5091T · Cessna TR182 · Engine Collector/Tailpipe/Nozzle > DURING ANNUAL INSPECTION, DISCOVERED CRACK APPROXIMATELY 1.5 INCHES IN LENGTH AROUND THE LT CROSSOVER ASSEMBLY. UPON REMOVAL, ALSO FOUND DETERIORATION IN THE SLIP JOINT CONNECTING THE RT CROSSOVER ASSEMBLY (PN 2254013). REPLACED BOTH PARTS WITH FACTORY NEW. - [SDR 2004FA0000534](https://openairdocs.org/sdr/2004FA0000534.md): Nut · missing · Apr 27, 2004 · N738PK · Cessna TR182 · Power Lever > JUST TURNED FINAL AND WENT TO PULL POWER BACK AND FOUND NO THROTTLE RESPONSE. PILOT WAS ABLE TO LAND USING MAG SWITCH TO ADD AND REDUCE POWER. UPON INSPECTION FOUND LOCK NUT MISSING FROM THROTTLE CONNECTION AND BOLT LAYING HALF OUT OF THROTTLE /TURBO ACTUATO - [SDR 2004FA0000386](https://openairdocs.org/sdr/2004FA0000386.md): Exhaust Stack · fractured · Apr 5, 2004 · N738QV · Cessna TR182 · Engine Collector/Tailpipe/Nozzle > DURING CRUISE FLT AT 7,500 FT. VFR, AIRCRAFT WOULD NOT MAINTAIN 25 INCHES MP. MP DROPPED TO 23 INCHES AFTER APPROX. 15 MIN. MP DROPPED ABRUPTLY TO 18.5 INCHES MP MADE EMERGENCY DESCENT & UNSCHEDULING LANDING AT VNX WITHIN 3 MINUTES OF POWER LOSS. UPON EXAMINAT - [SDR 2004FA0000352](https://openairdocs.org/sdr/2004FA0000352.md): Autopilot Sys · inoperative · Mar 12, 2004 · N738QV · Cessna TR182 · Autopilot System > IN APR AND NAV MODE, AUTOPILOT WILL NOT PROPERLY INTERCEPT AND TRACK LOCALIZER AND/OR VOR SIGNAL. AUTOPILOT WILL SCALLOP ACROSS COURSE. AUTOPILOT HAS BEEN SENT IN FOR EVALUATION. WE HAVE EVALUATED OUR PN-101 HSI TO DETERMINE IF THEY ARE THE SOURCE. AFTER EVAL - [SDR 2003FA0001239](https://openairdocs.org/sdr/2003FA0001239.md): Cooling Fins · blocked · Dec 5, 2003 · N4922S · Cessna TR182 · Reciprocating Engine Cylinder Section > VISUAL INSPECTION REVEALED MAJORITY OF COOLING FINGS BETWEEN INTAKE AND EXHAUST PORTS BLOCKED. VIRTUALLY NO AIR FLOW ALLOWED TO PASS BETWEEN ALL FINS ON ALL CYLINDERS. - [SDR 2003FA0001259](https://openairdocs.org/sdr/2003FA0001259.md): Bulkhead · cracked · Oct 7, 2003 · N5125T · Cessna TR182 · Fuselage Main, Bulkhead > DURING THE MFG OF THIS AC, THE OPTIONAL FACTORY OXYGEN SYS WAS INSTALLED. IT LOOKS LIKE THIS WAS KNOWN WHEN THE TAIL CONE WAS BUILT AS RIVETS IN THE AREA WHERE THE OXYGEN BOTTLE BRACKETS WERE OMITTED TO PROVIDE FOR INSTALLING THE BRACKETS. ONCE THE BRACKETS - [SDR 2003FA0000013](https://openairdocs.org/sdr/2003FA0000013.md): Line · leaking · Dec 18, 2002 · N757PD · Cessna TR182 · Hydraulic System, Main > THE POWERPACK CONTROL LINE WAS LEAKING HYDRAULIC FLUID, CAUSED BY AN IMPROPER SECURITY AND/OR ROUTING OF THE HYDRAULIC POWERPACK CONTROL LINE IN PROXIMITY TO THE MIXTURE CONTROL CABLE. AREA AROUND THE HYDRAULIC POWERPACK CONTROL LINE SHOULD BE INSPECTED UNDER - [SDR AUS20021408](https://openairdocs.org/sdr/AUS20021408.md): Gasket · leaking · Dec 5, 2002 · Cessna TR182 · Reciprocating Engine Cylinder Section > (AUS) NR 1 CYLINDER LEAKING AT EXHAUST GASKET. DAMAGE TO COOLING FINS AND BAFFLE. - [SDR 2002FA0001165](https://openairdocs.org/sdr/2002FA0001165.md): Fitting · cracked · Oct 9, 2002 · N6584S · Cessna TR182 · Main Landing Gear Attach Section > MLG AXLE ATTACHMENT FITTING, FOUND CRACKED AT TOP OUTBOARD EDGE. CRACK IS VISIBLE WITHOUT ADDITIONAL AIDS. CRACK ORIGINATES AT THIN EDGE WHERE FITTING WAS MACHINED DURING MANUFACTURE. CRACK IS ALSO IN ALIGNMENT WITH FORGING LINE. - [SDR CA020801015](https://openairdocs.org/sdr/CA020801015.md): Armature · separated · Jul 31, 2002 · Cessna TR182 · Starter-Generator > (CAN) PILOT REPORTED START ATTEMPT FAILED DUE TO EXCESSIVE ELECTRICAL DRAW AND STARTER MOTOR DID NOT TURN. STARTER REMOVED TO INSPECT AND FOUND COMMUTATOR COMPLETELY DISINTEGRATED ALONG WITH THE BRUSH BLOCKS AND HOLDER ASSY. THE CONNECTING WIRES TO THE ARMAT - [SDR AUS20020233](https://openairdocs.org/sdr/AUS20020233.md): Resistor · misinstalled · Feb 23, 2002 · Cessna TR182 · ATC Transponder System > (AUS) TRANSPONDER VOLTAGE DROPPING RESISTOR INCORRECTLY MOUNTED. THE RESISTOR IS MOUNTED ON THE REAR OF THE TRANSPONDER MOUNTING RACK. THE INSTALLATION MANUAL STATES THAT IT MUST BE MOUNTED AWAY FROM THE AVIONICS STACK TO AVOID OVERHEATING OF THE POWER SUPPLY. - [SDR AUS20020232](https://openairdocs.org/sdr/AUS20020232.md): Mount · loose · Feb 23, 2002 · Cessna TR182 · ATC Transponder System > (AUS) TRANSPONDER MOUNT LOOSE. MOUNT MADE OF THIN METAL. - [SDR AUS20020231](https://openairdocs.org/sdr/AUS20020231.md): Indicator · faulty · Feb 23, 2002 · Cessna TR182 · Engine Oil Temperature > (AUS) ENGINE OIL TEMPERATURE INDICATOR FAULTY. - [SDR AUS20020230](https://openairdocs.org/sdr/AUS20020230.md): Screw · missing · Feb 23, 2002 · Cessna TR182 · Integrated Flight System > (AUS) HSI TOP RT SCREW MISSING. - [SDR AUS20020229](https://openairdocs.org/sdr/AUS20020229.md): Ballast · broken · Feb 23, 2002 · Cessna TR182 · Exterior Lighting > (AUS) TAIL BEACON BALLAST RESISTOR BROKEN IN THREE PLACES. - [SDR AUS20020228](https://openairdocs.org/sdr/AUS20020228.md): Indicator · unserviceable · Feb 23, 2002 · Cessna TR182 · Autopilot System > (AUS) AUTOPILOT TURN AND BANK UNIT FAULTY. - [SDR AUS20020225](https://openairdocs.org/sdr/AUS20020225.md): Light · unserviceable · Feb 23, 2002 · Cessna TR182 · Flight Compartment Lighting > (AUS) LH CLOCK/MICROPHONE JACK POST LIGHT UNSERVICEABLE. THE CENTRE CONTACTOR ASSEMBLY WAS MISSING FROM THE LIGHT HOLDER. - [SDR AUS20020224](https://openairdocs.org/sdr/AUS20020224.md): Lens · loose · Feb 23, 2002 · Cessna TR182 · Exterior Lighting > (AUS) TAIL LIGHT LENS LOOSE. - [SDR AUS20020223](https://openairdocs.org/sdr/AUS20020223.md): Lens · misinstalled · Feb 23, 2002 · Cessna TR182 · Exterior Lighting > (AUS) RT NAVIGATION LIGHT LENS GLUED IN WITH SILASTIC. UNAPPROVED PART. - [SDR AUS20020222](https://openairdocs.org/sdr/AUS20020222.md): Light · faulty · Feb 23, 2002 · Cessna TR182 · Exterior Lighting > (AUS) BOTH STROBE LIGHT FLASH TUBES BLACKENED. - [SDR AUS20020221](https://openairdocs.org/sdr/AUS20020221.md): Light · unserviceable · Feb 23, 2002 · Cessna TR182 · Instrument System Wiring > (AUS) RH ARTIFICIAL HORIZON HAD NO INTERNAL OR EXTERNAL LIGHTING. INTERNAL LIGHTS WIRING CONNECTED TO AN UNKNOWN SOURCE. - [SDR AUS20020220](https://openairdocs.org/sdr/AUS20020220.md): Wire · cut · Feb 23, 2002 · Cessna TR182 · Navigation System Wiring > (AUS) WIRING TO RT SIDE OF ADF RACK CUT THROUGH BY RACK. - [SDR AUS20020219](https://openairdocs.org/sdr/AUS20020219.md): Light · misinstalled · Feb 23, 2002 · Cessna TR182 · Flight Compartment Lighting > (AUS) LT AND RT INSTRUMENT PANEL COVER POST LIGHT CONNECTION WIRES FITTED WITH INCORRECT TERMINALS. - [SDR AUS20020218](https://openairdocs.org/sdr/AUS20020218.md): Light · misinstalled · Feb 23, 2002 · Cessna TR182 · DC Indicating System > (AUS) ALTERNATOR LOW VOLTAGE WARNING LIGHT SECURED TO RT DASH WITH PVC ELECTRICAL TAPE. UNAPPROVED PART. - [SDR AUS20020217](https://openairdocs.org/sdr/AUS20020217.md): Pipe · corroded · Feb 23, 2002 · Cessna TR182 · Engine Oil Pressure > (AUS) PIPE BETWEEN OIL PRESSURE INDICATOR AND HOUR-METER BLOCK CORRODED AND FLARE SPLIT. HOUR-METER BLOCK FIREWALL FITTING LOOSE AND REAR FITTING HAD INCORRECT THREAD TYPE. OIL LEAKING FROM BEHIND DASH. - [SDR AUS20020216](https://openairdocs.org/sdr/AUS20020216.md): Light · unserviceable · Feb 23, 2002 · Cessna TR182 · Flight Compartment Lighting > (AUS) CONTROL COLUMN MAP LIGHT FAULTY. LAMP AND LAMP HOLDER MISSING. Next page: https://openairdocs.org/model/cessna-tr182/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'TR182' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/cessna-tr182/reports --- 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.