# Service difficulty reports: Cessna 182

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

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 90 reports

- [SDR 2024FA0000981](https://openairdocs.org/sdr/2024FA0000981.md): Fuel · unknown · Dec 23, 2024 · N1824 · Cessna 182 · Aircraft Fuel System
  > I AM CONCERNED ABOUT ADVERSE EFFECTS FROM A NEW UNLEADED FUEL (G100UL) THAT WAS APPROVED VIA THE STC PROCESS (SA01967WI & SE01966WI) AND RECENTLY INTRODUCED AT TWO LOCAL AIRPORTS (KRHV, KWVI). BASED ON PUBLIC REPORTS BY SOME USERS THAT THEY EXPERIENCED PAINT D
- [SDR 2023FA0000344](https://openairdocs.org/sdr/2023FA0000344.md): Solenoid · defective · Jun 27, 2023 · Cessna 182 · Landing Gear System
  > LANDING GEAR HYDRAULIC POWER PACK SOLENOID FAILED. AIRCRAFT LANDED WITH NOSE GEAR DOWN AND LOCKED BUT LEFT AND RIGHT MAIN GEARS FOLDED ON LANDING. DAMAGE TO RIGHT WING TIP, RIGHT SIDE OF HORIZONTAL STABILIZER AND RIGHT ELEVATOR. SOLENOID FAILURE DETERMINED BY
- [SDR CA190213015](https://openairdocs.org/sdr/CA190213015.md): Pin · dislodged · Feb 13, 2019 · Cessna 182 · Magneto/Distributor
  > (CAN) IMPULSE COUPLING PIN (NO PART NUMBER FOR ONLY THE PIN) NORMALLY PRESSED INTO MAGNETO HOUSING HAD COME OUT OF THE HOUSING ALLOWING OIL TO ENTER THE CASE OF THE MAG, THE PIN (1/4 INCH DIAMETER BY 1 1/8 INCH LONG) WAS FLUNG LOOSE AND CAME TO REST AT THE BOT
- [SDR 2017FA0000192](https://openairdocs.org/sdr/2017FA0000192.md): Barrel · broken · May 16, 2017 · N6233A · Cessna 182 · Shimmy Damper
  > NOSE WHEEL SHIMMY DAMPENER BARREL ASSEMBLY. ATTACHMENT BOSS BROKE CAUSING SHIMMY DAMPENER TO LOSE ITS FLUID CAUSING LOSS OF STEERING CONTROL.
- [SDR RJWR001](https://openairdocs.org/sdr/RJWR001.md): Angle · cracked · Jan 5, 2016 · Cessna 182 · Battery Box Structure
  > DURING MAINTENANCE, BATTERY MOUNT STRUCTURE FOUND CRACKED ACFT REQUIRING REPLACEMENT.
- [SDR 2016FA0000279](https://openairdocs.org/sdr/2016FA0000279.md): Pan · mismanufactured · Jul 20, 2015 · N5765B · Cessna 182 · Reciprocating Engine Oil System
  > ENGINE FAILURE DURING FLIGHT ON FACTORY REMANUFACTURED ENGINE WITH 406 HRS. INSPECTION FOUND MIS-MANUFACTURED OIL PAN/SUMP ASSOCIATED WITH STC 09319SC. SPECIFIC DEFECT CAUSES INTERFERENCE BETWEEN BOTTOM OF PAN AND OIL PICKUP. PART IS AVAILABLE FOR MEASUREME
- [SDR 2014FA0000202](https://openairdocs.org/sdr/2014FA0000202.md): Spar · cracked · Mar 15, 2014 · N5698B · Cessna 182 · Elevator, Spar/Rib
  > LEFT ELEVATOR SPAR, FOUND TO BE CRACKED DURING POST FLIGHT INSPECTION. NO PRIOR GROUND OR FLIGHT DAMAGE INCIDENTS REPORTED. THE LT ELEVATOR FOUND TO BE CRACKED BY VISUAL INSPECTION AFTER INDICATIONS OF EXCESSIVE VERTICAL MOVEMENT. CRACK LOCATIONS ON UPPER L
- [SDR CA140211008](https://openairdocs.org/sdr/CA140211008.md): Bolt · sheared · Feb 5, 2014 · Cessna 182 · Main Landing Gear
  > (CAN) DURING CPCP INSPECTION AND 1000 HR U-BOLT REPLACEMENT. RT GEAR U-BOLT WAS FOUND TO BE SHEARED AT BOTTOM OF REAR THREADS. SUSPECTED NUT WAS OVER TORQUED AND BOTTOMED OUT ON THREADS. TOTAL TIME ON U-BOLT IS UNKNOWN.
- [SDR CA131219015](https://openairdocs.org/sdr/CA131219015.md): Spar · corroded · Dec 16, 2013 · Cessna 182 · Wing Spar
  > (CAN) DURING CPCP BASE CORROSION INSPECTION. WHILE ACCOMPLISHING SID 57-11-01 WING STRUCTURE INSPECTION. DURING CLEANING OF SPAR BLOCKS SEVERE EXFOLIATION CORROSION WAS FOUND ON 3 OUT OF 4 SPAR BLOCKS. CORROSION WAS LOCATED INSIDE RADIUS OF BLOCK WHERE AN B
- [SDR CA090826015](https://openairdocs.org/sdr/CA090826015.md): Shaft · missing · Jul 13, 2009 · Cessna 182 · Propeller Governor
  > MASSIVE OIL LOSS DURING FLIGHT. ACFT LANDED ON HYW 17. ACFT LOADED ONTO TRANSPORT AND RELOCATED. INSP REVEALED ENG PLUG PN LW-13896 HANGING FROM LOCKING. PROPELLER GOVERNER IDLER SHAFT FOUND MISSING. PN LW-14021 IDLER GEAR PN LW-10541 FOUND FLOATING INSID
- [SDR 2009FA0000294](https://openairdocs.org/sdr/2009FA0000294.md): Strut · worn · Apr 10, 2009 · N5710B · Cessna 182 · Nose/Tail Landing Gear Strut/Axle
  > DURING ENGINE CHANGE AND ENGINE MOUNT CHANGE, THE AIR/OIL SEPARATOR BREATHER TUBE WAS REMOVED (ATTACHED BY THREE CLAMPS TO THE FIREWALL) FROM THE FIREWALL. THE MFG HAD ROUTED THE BREATHER TUBE SO THAT IT WOULD EXIT THE COWLING JUST AFT THE FIREWALL ONTO THE BE
- [SDR 2009FA0000281](https://openairdocs.org/sdr/2009FA0000281.md): Reinforcement · cracked · Mar 31, 2009 · N5441B · Cessna 182 · Horizontal Stabilizer Structure
  > FOUND DURING ANNUAL INSP, LT ATTACHMENT PIVOT POINT FOR HORIZ STAB (REINFORCEMENT ASSY PN 07120487) CRACKED AT BOLT HOLE EXTENDING TO EDGE OF BRACKET. REPLACED REINFORCEMENT ASSY AND IB BRACKET PN 0712302-1. ACFT TT AND PART TT 7201. (K)
- [SDR 2008FA0000848](https://openairdocs.org/sdr/2008FA0000848.md): Hose · deteriorated · Nov 19, 2008 · N72758 · Cessna 182 · Engine Fuel Distribution
  > ENGINE LOST RPM AND PARTIAL POWER ON GO-AROUND FROM REJECTED LANDING. ACFT THEN FLEW NORMAL PATTERN AND LANDED WITHOUT INCIDENT. GROUND RUN-UP SHOWED NO ABNORMALITIES. MAINT REMOVED INJECTOR NOZZLES. NR 2 CYL NOZZLE WAS PLUGGED AND CONTAMINANTS FOUND IN SE
- [SDR RIS2006F00000](https://openairdocs.org/sdr/RIS2006F00000.md): Line · chafed · Oct 5, 2006 · N933DD · Cessna 182 · Aircraft Fuel Distribution System
  > FUEL LINE WAS CHAFED 90 PERCENT THRU BY AILERON CABLE. THIS ITEM SHOULD BE CHECKED ON ALL MFG AC WITH FUEL LINES RUNNING ALONG AILERON CABLES. (K)
- [SDR 78978](https://openairdocs.org/sdr/78978.md): Hub · corroded · Mar 6, 2006 · Cessna 182 · Propeller Hub Section
  > CORRODED HUB.
- [SDR 2005FA0000497](https://openairdocs.org/sdr/2005FA0000497.md): Flyweight · cracked · Feb 23, 2005 · N195RB · Cessna 182 · Propeller Governor
  > FLYWEIGHT BASE CRACKED ALSO ASSOCIATED PART C20886 SPRING HEAD AND B20882-1. SPRING DRIVE ALSO CRACKED. (K) (22124)
- [SDR 2005FA0000191](https://openairdocs.org/sdr/2005FA0000191.md): Flyweight · cracked · Feb 23, 2005 · N195RB · Cessna 182 · Propeller Governor
  > FLYWEIGHT BASE CRACKED ALSO ASSOCIATED PART, C20886 SPRING HEAD AND B20882-1, SPRING DRIVE ALSO CRACKED. (K) (REF: 22124)
- [SDR EY2R0082166A](https://openairdocs.org/sdr/EY2R0082166A.md): Hub · corroded · Aug 19, 2004 · Cessna 182 · Propeller Hub Section
  > FOUND CORROSION ON HUB.
- [SDR EY2R00082166](https://openairdocs.org/sdr/EY2R00082166.md): Hub · corroded · Aug 19, 2004 · Cessna 182 · Propeller Hub Section
  > FOUND HUB CORRODED.
- [SDR 2004FA0000193](https://openairdocs.org/sdr/2004FA0000193.md): Spar · cracked · Feb 11, 2004 · N6465A · Cessna 182 · Elevator, Spar/Rib
  > DURING ANNUAL INSPECTION WHAT APPEARED TO BE A DENT WAS FOUND ON THE LOWER LEADING EDGE SKIN OF THE LEFT ELEVATOR. THIS (DENT) WAS CROSSED BY A CRACK. EXCESSIVE MOVEMENT OF THE ELEVATOR HORN WAS NOTED WHEN THE ELEVATOR WAS FLEXED. FURTHER INSPECTION REVEALED
- [SDR 2004FA0000192](https://openairdocs.org/sdr/2004FA0000192.md): Spar · cracked · Feb 11, 2004 · N6465A · Cessna 182 · Elevator, Spar/Rib
  > DURING ANNUAL INSPECTION WHAT APPEARED TO BE A DENT WAS FOUND ON THE LOWER LEADING EDGE SKIN OF THE LT ELEVATOR. THIS (DENT) WAS CROSSED BY A CRACK. EXCESSIVE MOVEMENT OF THE ELEVATOR HORN WAS NOTED WHEN THE ELEVATOR WAS FLEXED. FURTHER INSPECTION REVEALED A C
- [SDR 2003FA0001031](https://openairdocs.org/sdr/2003FA0001031.md): Control Cable · out of position · Oct 8, 2003 · Cessna 182 · Rudder Control System
  > A SAFETY RECOMMENDATION WAS SUBMITTED IN RESPONSE TO SEVERAL INSTANCES WHERE THE RUDDER CONTROL CABLE HAD BEEN FOUND LODGED UNDER THE MOUNTING BOLT FOR THE ELEVATOR CONTROL CABLE PULLEY AT APPROXIMATELY STATION 156. A REVIEW OF THE INSTALLATION INDICATES THIS
- [SDR CA021105010](https://openairdocs.org/sdr/CA021105010.md): Shaft · loose · Oct 11, 2002 · Cessna 182 · Mixture Control
  > (CAN) CARBURETOR RUNNING LEAN AT ALTITUDE, THROTTLE SHAFT LOOSE, ENGINE RUNS POORLY WITH THIS CARBURETOR. TIME SINCE FACTORY OVERHAUL IS 542.1 HOURS.
- [SDR 2002FA0001226](https://openairdocs.org/sdr/2002FA0001226.md): Starter · inoperative · Oct 2, 2002 · N5711B · Cessna 182 · Engine Starter
  > STARTER DOES NOT ALLOW THE STARTER ADAPTER TO DISENGAGE WHEN THE ENGINE STARTS. THE RESULT IS EXCESSIVE HEAT AND WEAR WHICH RAPIDLY DESTROYS THE EFFECTIVENESS OF THE ADAPTER. WITHIN 30-60 HOURS THE ADAPTER MUST BE REPLACED.
- [SDR CA020430003](https://openairdocs.org/sdr/CA020430003.md): Rib · failed · Apr 10, 2002 · Cessna 182 · Wing, Rib/Bulkhead
  > (CAN) RT WING STA 172.00 - DURING INSTALATION OF AUXILIARY WING TANKS, AN INSPECTION ACCESS HOLE WAS CUT IN LOWER RING SKIN AT STA. 169.00 SURVEILLANCE INSPECTON OF THE WING RIB AT STA 172.00 REVEALED AN EXTENSIVE COMPRESSION FAILURE ALONG THE ENTIRE LENGTH O
- [SDR CA020213011](https://openairdocs.org/sdr/CA020213011.md): Support · cracked · Feb 1, 2002 · Cessna 182 · Nose/Tail Landing Gear Attach Section
  > (CAN) RT OUTBOARD LANDING GEAR SUPPORT CASTING FOUND TO BE CRACKED IN TWO PLACES. FAULT WAS DISCOVERED WHEN GEAR LEG WAS REMOVED FOR NDT OF LANDING GEAR COMPONENTS. NO OTHER FAULTS FOUND. LANDING GEAR NDT INSPECTION WAS CARRIED OUT AT OWNER'S REQUEST.
- [SDR 2002FA0001052](https://openairdocs.org/sdr/2002FA0001052.md): Rheostat · shorted · Dec 3, 2001 · N5379B · Cessna 182 · Instrument Panel
  > FLYING LOW THROUGH A MOUNTAIN PASS TRIED TO TURN ON INSTRUMENTS LIGHTS. SMOKE IN CABIN. TURNED OFF MASTER. FOUND RESISTOR WINDINGS FAILED. CONTACT ARM BURNED THRU TO CASE. ALSO CIRCUIT BREAKER DID NOT OPEN.
- [SDR 2002FA0000443](https://openairdocs.org/sdr/2002FA0000443.md): Rheostat · shorted · Dec 3, 2001 · N5379B · Cessna 182 · Instrument Panel
  > FLYING LOW THRU MOUNTAIN PASS, TRIED TO TURN ON INSTRUMENT LIGHTS. MUCH SMOKE IN CABIN, TURNED OFF MASTER. FOUND RESISTOR WINDINGS FAILED, CONTACT ARM BURNED THRU TO CASE, ALSO CIRCUT BREAKER DID NOT OPEN. FOUND PLASTIC TRIM PANEL HOLE HAD EGG SHAPE, BUTTO
- [SDR 2001FA0000646](https://openairdocs.org/sdr/2001FA0000646.md): Valve · worn · Oct 25, 2001 · N5670B · Cessna 182 · Reciprocating Engine Cylinder Section
  > CYLINDER REMOVED DUE TO LOW COMPRESSION. VALVE STEM WORN TO 0.005.
- [SDR 20010418CW005](https://openairdocs.org/sdr/20010418CW005.md): Gyro · misinstalled · Apr 18, 2001 · N5590B · Cessna 182 · Directional Gyro and Indicating System
  > THE DIRECTIONAL GYRO WAS POWERED BY A WIRE OF THREE SIZES NR 12, NR 16 AND NR 18, SPLICED TOGETHER OVER A LENGTH OF 20 INCHES, THE LARGE END WAS BENT INTO A HOOK, TINNED WITH SOLDER AND CONNECTED TO THE AMMETER.
- [SDR 20010418CW004](https://openairdocs.org/sdr/20010418CW004.md): Wire · damaged · Apr 18, 2001 · N5590B · Cessna 182 · Battery/Charger System
  > THE BATTERY CABLE WAS BARE IN MANY PLACES INCLUDING THE PENETRATION OF THE FIREWALL. IT HAD ALSO BEEN PENETRATED BY A SCREW THROUGH THE BELLY OF AIRCRAFT, JUST FORWARD OF THE BATTERY BOX.
- [SDR 20010418CW003](https://openairdocs.org/sdr/20010418CW003.md): Heat Shield · missing · Apr 18, 2001 · N5590B · Cessna 182 · Engine Mount Section
  > THE ENGINE MOUNT HEAT SHIELDS HAD BEEN REMOVED AT SOME POINT ALLOWING HEAT DAMAGE REQUIRING 3 WELD REPAIRS.
- [SDR 20010418CW002](https://openairdocs.org/sdr/20010418CW002.md): Fastener · loose · Apr 18, 2001 · N5590B · Cessna 182 · Nacelle/Pylon, Bulkhead/Firewall
  > OWNER REPORTED 2 LOOSE RIVETS AT THE FIREWALL ATTACH POINT STA. 5. INVESTIGATION REVEALED 2 MISSING RIVET HEADS AN426AD4 AND A FURTHER 25 RIVET HEADS HELD ON BY PAINT ALONE. 1 OTHER RIVET HEAD HAD A STRANGE APPEARANCE, SCRAPING THE PAINT OFF REVEALED A BON
- [SDR 20010418CW001](https://openairdocs.org/sdr/20010418CW001.md): Gyro · inoperative · Apr 18, 2001 · N6312A · Cessna 182 · Directional Gyro and Indicating System
  > DURING ROUTINE ANNUAL INSPECTION THE ELEVATOR WAS FOUND TO TRAVEL ONLY 19 DEGREE UP. THE TYPE CERTIFICATE CALLS FOR 25 DEGREE. INVESTIGATION FOUND THE D. G. MOUNTED DIRECTLY ABOVE THE CONTROL WHEEL TUBE. AS THE WHEEL WAS PULLED AFT THE AN3-10A BOLT CONTACTE
- [SDR 20010420CW007](https://openairdocs.org/sdr/20010420CW007.md): O-Ring · leaking · Apr 2, 2001 · Cessna 182 · Engine Drains
  > THE QUICK DRAIN ORING THAT CAME WITH THE NEW QUICK DRAIN, SWELLED UP SO THAT IT IS PUSHED OUT OF THE GROOVE. OIL LEAKS PASSED IT EASILY.
- [SDR 20000829SH009](https://openairdocs.org/sdr/20000829SH009.md): Gear · failed · Jul 15, 2000 · N6473A · Cessna 182 · Main Landing Gear
  > DURING TAXI, LANDING GEAR SPRING FAILED AT MATING AREA OF P/N 0541121-2 SUPPORT. CAUSED SUBSTANTIAL DAMAGE TO RIGHT CABIN AFT OF CREW DOOR, RIGHT SIDE OF HORIZONTAL STABILIZER AND ELEVATOR, AND OUTBOARD SECTION OF RIGHT WING. (X)
- [SDR 20000712SH033](https://openairdocs.org/sdr/20000712SH033.md): Cooler · leaking · Jun 21, 2000 · Cessna 182 · Engine Oil Cooler
  > PART HAD BEEN REPAIRED USING EPOXY TO STOP A LEAK. DURING NORMAL SERVICE, EPOXY FAILED CAUSING THE OIL COOLER TO LEAK AT POINT OF ORIGINAL REPAIR. SUBMITTER RECOMMENDED ELIMINATING USE OF EPOXY IN OIL COOLERS AS EPOXY FAILURE IS COMMON. (X)
- [SDR AU000567](https://openairdocs.org/sdr/AU000567.md): Fitting · corroded · Jun 12, 2000 · Cessna 182 · Wing, Attach Fittings
  > (AUS) LEFT ABD RIGHT WING ATTACHMENT BLOCKS CONTAIN EXFOLIATION CORROSION.
- [SDR 99ZZZX3620](https://openairdocs.org/sdr/99ZZZX3620.md): Support · cracked · Aug 30, 1999 · N182MT · Cessna 182 · Fuselage Miscellaneous Structure
  > BATTERY BOX SUPPORT ANGLES WERE FOUND CRACKED DURING ANNUAL INSPECTION.
- [SDR 20000714SH013](https://openairdocs.org/sdr/20000714SH013.md): Spring · broken · Aug 11, 1999 · N6284A · Cessna 182 · Nose/Tail Landing Gear Strut/Axle
  > AIRCRAFT TT 7,577 HOURS. RIGHT SIDE MAIN SPRING LANDING GEAR BROKE ON LANDING. SPRING LANDING GEAR BROKE APPROXIMATELY 3 INCHES FROM FUSELAGE ON A LINE THROUGH THE DIMPLES IN THE SPRING GEAR THAT HOLDS THE BRAKE LINE RETAINER BRACKET. (X)
- [SDR 99ZZZX2616](https://openairdocs.org/sdr/99ZZZX2616.md): Oil Cooler · leaking · Jun 30, 1999 · Cessna 182 · Engine Oil Cooler
  > PART WS REPAIRED USING EPOXY. EPOXY FAILED DURING NORMAL SERVICE ALLOWING PART TO LEAK AT POINT OF ORIGINAL REPAIR. EPOXY FAILURE IS COMMON. SUBMITTER RECOMMENDED ELIMINATING USE OF EPOXY IN OIL COOLERS.
- [SDR 99ZZZX2508](https://openairdocs.org/sdr/99ZZZX2508.md): Hub · corroded · Jun 14, 1999 · Cessna 182 · Propeller Hub Section
  > SUBMITTER STATED PART SHOULD HAVE BEEN REJECTED AT OVERHAUL FOR CORROSION CAUSING METAL TO FLAKE OFF THE EXTERIOR HUB SERVICES.
- [SDR AU980474](https://openairdocs.org/sdr/AU980474.md): Screw · dislodged · Apr 21, 1998 · Cessna 182 · Control Column Section
  > (AUS) RT CONTROL COLUMN SCREW P/N NAS22014 WAS FOUND ADRIFT ALONG WITH GLIDE P/N 0760651-2 AND PLUG P/N 0760681-1. THE LT CONTROL COLUMN WAS CHECKED AND ITS SCREW WAS ALSO FOUND TO BE LOOSE.
- [SDR 98ZZZX893](https://openairdocs.org/sdr/98ZZZX893.md): Gear Support · cracked · Nov 15, 1997 · N5553B · Cessna 182 · Main Landing Gear Attach Section
  > BOTH LANDING GEAR OUTBOARD SUPPORT CASTINGS FOUND CRACKED AT ANNUAL INSPECTION. AIRCRAFT CARRY 5 PERSONS (PER STC) DURING SKYDIVING OPERATIONS. NO RECORD OF PREVIOUS CHANGE OF THESE SUPPORTS. LANDING GEAR SHOULD BE INSPECTED AFTER HARD LANDINGS.
- [SDR 98ZZZX892](https://openairdocs.org/sdr/98ZZZX892.md): Gear Support · cracked · Nov 15, 1997 · N5553B · Cessna 182 · Main Landing Gear Attach Section
  > BOTH LANDING GEAR OUTBOARD SUPPORT CASTINGS FOUND CRACKED AT ANNUAL INSPECTION. AIRCRAFT CARRY 5 PERSONS (PER STC) DURING SKYDIVING OPERATIONS. NO RECORD OF PREVIOUS CHANGE OF THESE SUPPORTS. LANDING GEAR SHOULD BE INSPECTED AFTER HARD LANDINGS.
- [SDR 98ZZZX888](https://openairdocs.org/sdr/98ZZZX888.md): Gear Support · cracked · Nov 15, 1997 · N6346A · Cessna 182 · Main Landing Gear Attach Section
  > BOTH LANDING GEAR OUTBOARD SUPPORT CASTINGS FOUND CRACKED DURING ANNUAL INSPECTION. AIRCRAFT CARRIES 5 PERSONS (PER STC) DURING SKYDIVING OPERATIONS. NO RECORD OF PREVIOUS CHANGE OF THESE SUPPORTS. LANDING GEAR SHOULD BE CHECKED AFTER HARD LANDINGS.
- [SDR 98ZZZX887](https://openairdocs.org/sdr/98ZZZX887.md): Gear Support · cracked · Nov 15, 1997 · N6346A · Cessna 182 · Main Landing Gear Attach Section
  > BOTH LANDING GEAR OUTBOARD SUPPORT CASTINGS FOUND CRACKED DURING ANNUAL INSPECTION. AIRCRAFT CARRIES 5 PERSONS (PER STC) DURING SKYDIVING OPERATIONS. NO RECORD OF PREVIOUS CHANGE OF THESE SUPPORTS. LANDING GEAR SHOULD BE CHECKED AFTER HARD LANDINGS.
- [SDR 97ZZZX4388](https://openairdocs.org/sdr/97ZZZX4388.md): Bushing · broken · Jul 15, 1997 · N6285A · Cessna 182 · Propeller Blade Section
  > PILOT REPORTED VIBRATION AND POWER LOSS. INVESTIGATION FOUND PITCH CHANGE PHENOLIC BUSHING ON ONE BLADE BROKEN ALLOWING BLADE TO MOVE TO LOWER PITCH THAN OTHER BLADE.
- [SDR CA970421092](https://openairdocs.org/sdr/CA970421092.md): Support · cracked · Apr 10, 1997 · Cessna 182 · Main Landing Gear Attach Section
  > (CAN) BOTH MLG CASTING HAD BEEN REPLACED.
- [SDR EY2R9601341](https://openairdocs.org/sdr/EY2R9601341.md): Hub · corroded · Dec 1, 1996 · Cessna 182 · Propeller Hub Section
  > CORROSION FOUND ON HUB.

Next page: https://openairdocs.org/model/cessna-182/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 = '182'
ORDER BY difficulty_date DESC
```

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From OpenAirDocs.org, an independent open copy of FAA and NTSB data. This list as a web page: https://openairdocs.org/model/cessna-182/reports