# Service difficulty reports: Cessna 182T

A list on [Cessna 182T](https://openairdocs.org/model/cessna-182t.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 167 reports

- [SDR 2026FA0000573](https://openairdocs.org/sdr/2026FA0000573.md): Light · broken · Apr 28, 2026 · N3545J · Cessna 182T · Exterior Lighting
  > PULSE LIGHT WAS FIRST REPLACED 9-30-2025 DUE TO LT WIG WAG NOT WORKING, SOLID ON WORKED. AFTER A MONTH OF OPERATION LT WIG WAG FAILED AGAIN, DIDNT GET TO TROUBLESHOOT AGAIN UNTIL 4-20-2026 AND NOTED THAT AT THAT TIME EVEN SOLID ON DID NOT WORK, SUSPECTED FAUL
- [SDR 2026FA0000250](https://openairdocs.org/sdr/2026FA0000250.md): Cable · frayed · Mar 30, 2026 · N811CP · Cessna 182T · Aileron Control System
  > WHILE TROUBLESHOOTING A FUEL LEAK THE MECHANIC NOTICED THAT THE AILERON CARRY THROUGH CABLE WAS FRAYED.
- [SDR 2026FA0000094](https://openairdocs.org/sdr/2026FA0000094.md): Doubler · cracked · Feb 10, 2026 · N365CA · Cessna 182T · Fuselage Main, Bulkhead
  > DURING FIREWALL CLEANING/INSPECTION DURING ANNUAL/100HR INSPECTION, A CRACK, APPROXIMATELY 1.0" IN LENGTH WAS DISCOVERED IN THE UPPER RADIUS OF THE LEFT HAND SIDE OF THE LOWER FIREWALL DOUBLER DIRECTLY THROUGH THE TOP RIVET THAT HOLDS THE PARKING BRAKE BRACKET
- [SDR 2026FA0000074](https://openairdocs.org/sdr/2026FA0000074.md): Doubler · cracked · Feb 2, 2026 · N655CP · Cessna 182T · Fuselage Main, Bulkhead
  > DURING FIREWALL CLEANING/INSPECTION DURING ANNUAL/100HR INSPECTION, A CRACK, APPROXIMATELY 2.3 IN LENGTH WAS DISCOVERED IN THE UPPER RADIUS OF THE LEFT HAND SIDE OF THE LOWER FIREWALL DOUBLER DIRECTLY THROUGH THE TOP RIVET THAT HOLDS THE PARKING BRAKE BRACKET
- [SDR 2026FA0000001](https://openairdocs.org/sdr/2026FA0000001.md): Strut · cracked · Jan 6, 2026 · N3545J · Cessna 182T · Wing Main, Frame Structure
  > CRACK ON WING SIDE OF RH STRUT. AIRFRAME TOTAL TIME IS 10298.9. CRACK WAS FOUND DURING ROUTINE 100/HR INSPECTION. AIRPLANE DOES PIPELINE PATROL.
- [SDR 2026FA0000073](https://openairdocs.org/sdr/2026FA0000073.md): Doubler · cracked · Dec 2, 2025 · N397CP · Cessna 182T · Fuselage Main, Bulkhead
  > DURING FIREWALL CLEANING IN PREPARATION OF INSTALLATION OF NEWLY OVERHAULED ENGINE, A CRACK, APPROXIMATELY 2.3 IN LENGTH WAS DISCOVERED IN THE UPPER RADIUS OF THE LEFT HAND SIDE OF THE LOWER FIREWALL DOUBLER DIRECTLY THROUGH THE TOP RIVET THAT HOLDS THE PARKIN
- [SDR ODAR2025080600001](https://openairdocs.org/sdr/ODAR2025080600001.md): Skin · cracked · Aug 6, 2025 · N482CP · Cessna 182T · Wing, Plate/Skin
  > DURING 100HR / ANNUAL INSPECTION FOUND RH INBOARD FLAP COVE SKIN CRACKED ALONG WITH FLAP TRACK RIVETS WORKING OUT. INSPECTED AREA AROUND FLAP AND FOUND THE INBD FLAP TRACK/RIB ASSEMBLY TO BE CRACKED THROUGH.
- [SDR 2024FA0000717](https://openairdocs.org/sdr/2024FA0000717.md): Attach Fitting · cracked · Sep 17, 2024 · N153FC · Cessna 182T · Fuselage Main, Attach Fittings
  > DURING A 50-HOUR OIL CHANGE / INSPECTION EVENT THE NOSE LANDING GEAR LOWER STRUT FITTING WAS DISCOVERED TO BE CRACKED IN TWO ON THE RIGHT-HAND WEB SECTION. AFTER REMOVAL OF BROKEN MOUNT, EVIDENCE SHOWED THE CRACK HAD OCCURRED PRIOR TO THE FINAL FAILURE OF THE
- [SDR 2024FA0000515](https://openairdocs.org/sdr/2024FA0000515.md): Fitting · cracked · Jul 23, 2024 · N894CP · Cessna 182T · Nose/Tail Landing Gear
  > NOSE GEAR LOWER ATTACH FITTING CRACKED. DISCOVERED DURING ANNUAL INSPECTION.
- [SDR 2024FA0000512](https://openairdocs.org/sdr/2024FA0000512.md): Fitting · cracked · Jul 23, 2024 · N738C · Cessna 182T · Nose/Tail Landing Gear
  > NOSE GEAR, LOWER ATTACH STRUT FITTING CRACKED IN RADIUS.
- [SDR 2024FA0000520](https://openairdocs.org/sdr/2024FA0000520.md): Fitting · cracked · Jul 17, 2024 · N410CV · Cessna 182T · Nose/Tail Landing Gear
  > NOSE STRUT LOWER ATTACH FITTING CRACKED IN RADIUS. DISCOVERED DURING ANNUAL INSPECTION, CONFIRMED VIA DYE PENETRANT INSPECTION.
- [SDR 2024FA0000519](https://openairdocs.org/sdr/2024FA0000519.md): Fitting · cracked · Jul 10, 2024 · N408CV · Cessna 182T · Nose/Tail Landing Gear
  > NOSE STRUT, LOWER ATTACH FITTING CRACKED IN RADIUS. CRACK DISCOVERED DURING ANNUAL INSPECTION. CONFIRMED WITH DYE PENETRANT.
- [SDR 2024FA0000518](https://openairdocs.org/sdr/2024FA0000518.md): Fitting · cracked · May 1, 2024 · N486CP · Cessna 182T · Nose/Tail Landing Gear
  > NOSE STRUT, LOWER ATTACH FITTING CRACKED IN RADIUS. CRACK DISCOVERED DURING ANNUAL INSPECTION.
- [SDR 2023FA0000671](https://openairdocs.org/sdr/2023FA0000671.md): Tube · deflated · Oct 24, 2023 · N1552S · Cessna 182T · Tire Tube
  > ON THE 5TH UPON GETTING TO THE HANGAR I FOUND THE TIRE STILL FULLY INFLATED AND AT PROPER PSI. I REMOVED THE TIRE AND REPLACED THE TUBE WITH NEW. UPON INSPECTING THE OLD TUBE I FOUND A SMALL HOLE ON THE SIDE OF THE TUBE THAT WAS NOT LEAKING WHEN FULLY INFLATED
- [SDR 2023FA0000395](https://openairdocs.org/sdr/2023FA0000395.md): Alternator · seized · Jul 31, 2023 · N859JA · Cessna 182T · DC Generator-Alternator
  > CREW REPORTED DURING GROUND RUN AND PRIOR TO TAXI, ENGINE MADE A LOUD NOISE, AND THE ENGINE WAS SHUT DOWN IMMEDIATELY. THIS HAPPENED PRIOR TO FLIGHT, WITH NO INDICATION OF A PENDING FAILURE. MAINTENANCE TECHNICIAN REPORTED THAT THE ALTERNATOR HAD SEIZED, AN
- [SDR 2023FA0000310](https://openairdocs.org/sdr/2023FA0000310.md): Points · broken · Jun 12, 2023 · N177CP · Cessna 182T · Magneto/Distributor
  > TEST, TEST, TEST: MAGNETO POINT FAILURE
- [SDR 2024FA0000517](https://openairdocs.org/sdr/2024FA0000517.md): Fitting · cracked · Oct 20, 2022 · N849CP · Cessna 182T · Nose/Tail Landing Gear
  > NOSE STRUT, LOWER ATTACH FITTING CRACKED IN RADIUS. DISCOVERED DURING ANNUAL INSPECTION.
- [SDR 2022FA0000270](https://openairdocs.org/sdr/2022FA0000270.md): Points · broken · May 31, 2022 · N177CP · Cessna 182T · Magneto/Distributor
  > MAGNETO POINT FAILURE
- [SDR 2022FA0000171](https://openairdocs.org/sdr/2022FA0000171.md): None · loose · Mar 24, 2022 · N215DJ · Cessna 182T · Elevator Structure
  > DURING THE PREFLIGHT INSPECTION OF THE RH ELEVATOR, A CREAKING NOISE WAS HEARD FROM THE ELEVATOR PIVOTING TORQUE TUBE. AFTER AN IN DEPTH INSPECTION SMOKING RIVETS WERE FOUND ON THE RH ELEVATOR TORQUE TUBE END PLATE. WHEN THE ELEVATOR WAS REMOVED TO MAKE THE NE
- [SDR 2024FA0000516](https://openairdocs.org/sdr/2024FA0000516.md): Fitting · cracked · Jan 17, 2022 · N395CV · Cessna 182T · Nose/Tail Landing Gear
  > NOSE GEAR STRUT, LOWER ATTACH FITTING CRACKED IN RADIUS. DISCOVERED DURING ANNUAL INSPECTION.
- [SDR JRUR202012090014](https://openairdocs.org/sdr/JRUR202012090014.md): Control Rod · broken · Dec 9, 2020 · N12HP · Cessna 182T · Cabin Temperature Control System
  > NO HEAT FLOW INTO THE CABIN WHEN IN FLIGHT. FOUND THAT WELD THAT ATTACHED THE CONTROL ROD TO THE VALVE PLATE HINGE CRACKED & BROKEN CAUSING THE VALVE PLATE TO NOT FUNCTION AS DESIGNED TO OPEN OR CLOSE ALLOWING HOT AIR FROM ENTERING THE CABIN.
- [SDR 2024FA0000514](https://openairdocs.org/sdr/2024FA0000514.md): Fitting · cracked · Sep 18, 2020 · N709CP · Cessna 182T · Nose/Tail Landing Gear
  > NOSE GEAR LOWER ATTACH FITTING CRACKED IN RADIUS. DISCOVERED DURING ANNUAL INSPECTION.
- [SDR 2024FA0000513](https://openairdocs.org/sdr/2024FA0000513.md): Fitting · cracked · Sep 16, 2020 · N452CP · Cessna 182T · Nose/Tail Landing Gear
  > NOSE GEAR LOWER ATTACH FITTING CRACKED.
- [SDR JRUR2020032560002](https://openairdocs.org/sdr/JRUR2020032560002.md): Magneto · unserviceable · Mar 25, 2020 · N17HP · Cessna 182T · Magneto/Distributor
  > SLICK BY CHAMPION SB2-19A MANDATORY INSPECTION OF IMPULSE COUPLING. THE SB HAS YOU INSPECT THE IMPULSE COUPLING PER THE MAINTENANCE MANUAL. IF ANY MOVEMENT IS FOUND IN THE RIVETS, THE IMPULSE COUPLING MUST BE REJECTED. INSPECTED MAGNETO MODEL NO. 6351 P/N:
- [SDR JRUR202003120012](https://openairdocs.org/sdr/JRUR202003120012.md): Impulse Coupling · unserviceable · Mar 12, 2020 · N19HP · Cessna 182T · Magneto/Distributor
  > SLICK BY CHAMPION SB2-19A MANDATORY INSPECTION OF IMPULSE COUPLING. THE SB HAS YOU INSPECT THE IMPULSE COUPLING PER THE MAINTENANCE MANUAL. IF ANY MOVEMENT IS FOUND IN THE RIVETS, THE IMPULSE COUPLING MUST BE REJECTED. MAGNETO INSTALLED WITH TSN 0.0 AT AN A
- [SDR JRUR202003120011](https://openairdocs.org/sdr/JRUR202003120011.md): Impulse Coupling · unserviceable · Mar 12, 2020 · N19HP · Cessna 182T · Magneto/Distributor
  > SLICK BY CHAMPION SB2-19A MANDATORY INSPECTION OF IMPULSE COUPLING. THE SB HAS YOU INSPECT THE IMPULSE COUPLING PER THE MAINTENANCE MANUAL. IF ANY MOVEMENT IS FOUND IN THE RIVETS, THE IMPULSE COUPLING MUST BE REJECTED. MAGNETO INSTALLED WITH TSN 0.0 AT AN A
- [SDR JRUR202003060005](https://openairdocs.org/sdr/JRUR202003060005.md): Magneto · unserviceable · Mar 6, 2020 · N113HP · Cessna 182T · Magneto/Distributor
  > SLICK BY CHAMPION SB2-19A MANDATORY INSPECTION OF IMPULSE COUPLING. THE SB HAS YOU INSPECT THE IMPULSE COUPLING PER THE MAINTENANCE MANUAL. IF ANY MOVEMENT IS FOUND IN THE RIVETS, THE IMPULSE COUPLING MUST BE REJECTED. MAGNETO INSTALLED WITH TSN 952.3 AT AN
- [SDR JRUR202003060004](https://openairdocs.org/sdr/JRUR202003060004.md): Magneto · unserviceable · Mar 6, 2020 · N311HP · Cessna 182T · Magneto/Distributor
  > SLICK BY CHAMPION SB2-19A MANDATORY INSPECTION OF IMPULSE COUPLING. THE SB HAS YOU INSPECT THE IMPULSE COUPLING PER THE MAINTENANCE MANUAL. IF ANY MOVEMENT IS FOUND IN THE RIVETS, THE IMPULSE COUPLING MUST BE REJECTED. MAGNETO INSTALLED WITH TSN 0.0 AT AN A
- [SDR JRUR202003060003](https://openairdocs.org/sdr/JRUR202003060003.md): Magneto · unserviceable · Mar 6, 2020 · N6HP · Cessna 182T · Magneto/Distributor
  > SLICK BY CHAMPION SB2-19A MANDATORY INSPECTION OF IMPULSE COUPLING. THE SB HAS YOU INSPECT THE IMPULSE COUPLING PER THE MAINTENANCE MANUAL. IF ANY MOVEMENT IS FOUND IN THE RIVETS, THE IMPULSE COUPLING MUST BE REJECTED. MAGNETO INSTALLED WITH TSN 493.9 AT AN
- [SDR JRUR202003060001](https://openairdocs.org/sdr/JRUR202003060001.md): Magneto · unserviceable · Mar 6, 2020 · N17HP · Cessna 182T · Magneto/Distributor
  > SUPPLEMENTAL INFORMATION SLICK BY CHAMPION SB2-19A MANDATORY INSPECTION OF IMPULSE COUPLING. THE SB HAS YOU INSPECT THE IMPULSE COUPLING PER THE MAINTENANCE MANUAL. IF
- [SDR JRUR2020030560002](https://openairdocs.org/sdr/JRUR2020030560002.md): Magneto · unserviceable · Mar 5, 2020 · N17HP · Cessna 182T · Magneto/Distributor
  > SLICK BY CHAMPION SB2-19A MANDATORY INSPECTION OF IMPULSE COUPLING. THE SB HAS YOU INSPECT THE IMPULSE COUPLING PER THE MAINTENANCE MANUAL. IF ANY MOVEMENT IS FOUND IN THE RIVETS, THE IMPULSE COUPLING MUST BE REJECTED. INSPECTED MAGNETO MODEL NO. 6351 P/N:
- [SDR CA190723009](https://openairdocs.org/sdr/CA190723009.md): Wheel · damaged · Jul 22, 2019 · Cessna 182T · Wheel/Ski/Float
  > (CAN) DURING AN OPERATION 3 INSPECTION IT WAS DISCOVERED THAT BOTH LEFT AND RIGHT MAIN LANDING GEAR TIRES HAD BEEN EXPOSED TO A SKID WHICH RENDERED THE TIRES UNSERVICEABLE. AFTER REMOVING THE TIRES THE WHEEL HALVES WERE INSPECTED AND FOUND TO HAVE INTER-GRANUL
- [SDR 2019FA0000155](https://openairdocs.org/sdr/2019FA0000155.md): Switch · failed · May 20, 2019 · N528CP · Cessna 182T · Trailing Flap Position Indicating System
  > FLAPS SELECTED AND MOVED FULL DOWN FOR PREFLIGHT INSPECTION AND THEN WOULD NOT RETRACT. FOUND FLAP UP SELECTOR MICROSWITCH (S1007) BROKEN INTERNALLY.
- [SDR JRUR201905060002](https://openairdocs.org/sdr/JRUR201905060002.md): Exhaust Valve · out of tolerance · May 6, 2019 · N113HP · Cessna 182T · Reciprocating Engine Cylinder Section
  > DURING PERFORMANCE OF SB 388C, IT WAS FOUND THAT THE NR 4 CYLINDER EXHAUST VALVE TO GUIDE CLEARANCE MEASURED.031". THIS EXCEEDS THE MAXIMUM ALLOWABLE CLEARANCE OF.030". THIS ENGINE WAS OVERHAUL. THE TOTAL TIME SINCE NEW IS NOT BEING LISTED AS IT IS NOT KNOWN
- [SDR JRUR201905060001](https://openairdocs.org/sdr/JRUR201905060001.md): Exhaust Valve · out of tolerance · May 6, 2019 · N113HP · Cessna 182T · Reciprocating Engine Cylinder Section
  > DURING PERFORMANCE OF SB 388C, IT WAS FOUND THAT THE NR 3 CYLINDER EXHAUST VALVE TO GUIDE CLEARANCE MEASURED.031". THIS EXCEEDS THE MAXIMUM ALLOWABLE CLEARANCE OF.030". THIS ENGINE WAS OVERHAUL. THE TOTAL TIME SINCE NEW IS NOT BEING LISTED AS IT IS NOT KNOWN
- [SDR 2018FA0000339](https://openairdocs.org/sdr/2018FA0000339.md): Autopilot Sys · corrupted · Aug 20, 2018 · N365CA · Cessna 182T · Global Positioning System
  > AUTOPILOT INTEGRATED WITH G1000 REFUSED TO DISCONNECT.
- [SDR 2017FA0000460](https://openairdocs.org/sdr/2017FA0000460.md): Sprocket · broken · Aug 23, 2017 · N153FC · Cessna 182T · Elevator Tab Control System
  > ELEVATOR TRIM LOCKED UP IN FLIGHT. TRIM ACTUATOR SPROCKET FOUND TO BE BROKEN WHERE PIN ATTACHES IT TO ACTUATOR ASSEMBLY.
- [SDR 2017FA0000106](https://openairdocs.org/sdr/2017FA0000106.md): Pushrod · scored · Mar 17, 2017 · N514NY · Cessna 182T · Reciprocating Engine Cylinder Section
  > DURING THE PUSHROD INSPECTION FOUND THE NR 3, 4, 5, AND 6 PUSHRODS SCORED AND REPLACED.
- [SDR 2017FA0000105](https://openairdocs.org/sdr/2017FA0000105.md): Pushrod · scored · Mar 17, 2017 · N361DB · Cessna 182T · Reciprocating Engine Cylinder Section
  > DURING INSPECTION OF PUSHRODS FOUND THE NR 5, 4, & 1 PUSHRODS WORN OUT OF TOLERANCE, BOTH PUSHRODS AND ROCKER ARMS REPLACED WITH NEW.
- [SDR 2017FA0000103](https://openairdocs.org/sdr/2017FA0000103.md): Pushrod · scored · Mar 17, 2017 · N962JB · Cessna 182T · Reciprocating Engine Cylinder Section
  > DURING THE INSPECTION OF PUSHRODS FOUND TWO PUSHRODS AT THE NR 2 AND 6, SCORED BEYOND LIMITS. REPLACED THE PUSHRODS AND MATING ROCKER ARMS WITH NEW.
- [SDR 2017FA0000092](https://openairdocs.org/sdr/2017FA0000092.md): Pushrod · scored · Mar 7, 2017 · N916WR · Cessna 182T · Reciprocating Engine Cylinder Section
  > DURING INSPECTION OF PUSHRODS, FOUND NR 4 CYLINDER EXHAUST PUSHROD SCORED, REPLACED PER SA-167A.
- [SDR 2017FA0000090](https://openairdocs.org/sdr/2017FA0000090.md): Pushrod · scored · Mar 7, 2017 · N404KR · Cessna 182T · Reciprocating Engine Cylinder Section
  > DURING INSPECTION OF SA-167A FOUND THE NR 2 CYLINDER EXHAUST PUSHROD SCORED, REPLACED THE PUSHROD AND ROCKER ARM.
- [SDR 2017FA0000088](https://openairdocs.org/sdr/2017FA0000088.md): Governor · malfunctioned · Mar 6, 2017 · Cessna 182T · Propeller Governor
  > PILOT STATED THAT DURIUNG DESCENT, THE ENGINE ROLLED BACK TO 1500 RPM, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE PROPELLER GOVERNOR WAS REPLACED AND NO FURTHER DEFECTS WERE NOTED.
- [SDR 2017FA0000087](https://openairdocs.org/sdr/2017FA0000087.md): Pushrod · scored · Mar 6, 2017 · N311SB · Cessna 182T · Reciprocating Engine Cylinder Section
  > FIVE PUSHRODS FOUND TO BE SCORED ON THE NR 5, 3 AND 4 CYLINDERS, FOUND DURING THE SA-167A INSPECTION.
- [SDR 2017FA0000086](https://openairdocs.org/sdr/2017FA0000086.md): Pushrod · scored · Mar 6, 2017 · N311SB · Cessna 182T · Reciprocating Engine Cylinder Section
  > FIVE PUSHRODS FOUND TO BE SCORED ON THE NR 5, 3 AND 4 CYLINDERS, FOUND DURING THE SA-167A INSPECTION.
- [SDR 2017FA0000053](https://openairdocs.org/sdr/2017FA0000053.md): Pushrod · scored · Feb 9, 2017 · N311SB · Cessna 182T · Reciprocating Engine Cylinder Section
  > INSPECTION REVEALED NR 5 CYLINDER, EXHAUST AND INTAKE, NR 3 CYLINDER EXHAUST AND INTAKE AND NR 4 CYLINDER EXHAUST AND INTAKE PUSHRODS SCORED BEYOND LIMITS AND REPLACED.
- [SDR 2017FA0000052](https://openairdocs.org/sdr/2017FA0000052.md): Pushrod · worn · Feb 9, 2017 · N984SJ · Cessna 182T · Reciprocating Engine Cylinder Section
  > INSPECTION SHOWS 10 OF THE PUSHRODS HAVE WEAR. THE MAINTENANCE PROVIDER SAID THE 10 PUSHRODS, ROCKER ARMS AND ALL OF THE VALVE ROCKER SHAFTS NEED TO BE REPLACED. ON 10 AUGUST 2012, TAC TIME 578.9 NR 3 CYLINDER WAS REPLACED. DURING THE CHANGE ABNORMAL WEAR WA
- [SDR 2017FA0000051](https://openairdocs.org/sdr/2017FA0000051.md): Pushrod · out of limits · Feb 9, 2017 · N514NY · Cessna 182T · Reciprocating Engine Cylinder Section
  > DURING INSPECTION OF PUSHRODS, FOUND 6 PUSHRODS AND 6 ROCKER ARMS OUT OF LIMITS IN ACCORDANCE WITH SA-167A, PARTS REPLACED UNDER WARRANTY.
- [SDR 2017FA0000043](https://openairdocs.org/sdr/2017FA0000043.md): Pushrod · scored · Feb 3, 2017 · N361DB · Cessna 182T · Reciprocating Engine Cylinder Section
  > NR 1 INTAKE AND EXHAUST SCORED, NR 4 INTAKE AND EXHAUST SCORED, AND NR 5 EXHAUST SCORED, PARTS REPLACED PER SA-167A.
- [SDR 2017FA0000031](https://openairdocs.org/sdr/2017FA0000031.md): Pushrod · scored · Jan 30, 2017 · N962J · Cessna 182T · Reciprocating Engine Cylinder Section
  > NR 2 AND 6 PUSHRODS AND ROCKER ARMS REPLACED FOR EXHAUST SIDE DUE TO SA-167A INSPECTION. SCORING IS OBVIOUS AND TRANSLATED TO ROCKER ARM AS WELL. REPLACED PARTS AS NECESSARY.

Next page: https://openairdocs.org/model/cessna-182t/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 = '182T'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-182t/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.