# Service difficulty reports: Cessna 182Q

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

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 174 reports

- [SDR 2026FA0000158](https://openairdocs.org/sdr/2026FA0000158.md): Mount · corroded · Mar 5, 2026 · N759QH · Cessna 182Q · Engine Mount Section
  > THE DISSIMILAR METAL TAPE SUPPLIED IN STC SA00496SE (U-LINE ELECTRICAL TAPE) IS CAUSING CORROSION ON THE ENGINE MOUNT TO THE POINT OF REPLACING THE ENGINE MOUNT WITH IN 500-100HRS AFTER INSTALLING THE STC. THIS HAS HAPPENED ON THREE OF OUR FLEET AIRCRAFT IN TH
- [SDR 2025FA0000356](https://openairdocs.org/sdr/2025FA0000356.md): Circuit Breaker · burned · May 10, 2025 · N735GQ · Cessna 182Q · Electrical Power System Wiring
  > LOST AVIONICS, TRANSPONDER, AND RADIO STACK. SMELLED BURNING WIRES AND DECLARED EMERGENCY. LANDED WITHOUT FURTHER INCIDENT. FOUND SOURCE TO BE A BAD 40 AMP BREAKER SWITCH WHICH RUNS THE AVIONICS AND RADIO STACK.
- [SDR 2023FA0000760](https://openairdocs.org/sdr/2023FA0000760.md): Cylinder Head · low pressure · Nov 1, 2023 · N735BJ · Cessna 182Q · Reciprocating Engine Cylinder Section
  > CYLINDERS 2,4, AND 6 HAVE LOW COMPRESSION (30'S) THESE CONTINUE TO LOWER WITH EACH ANNUAL INSPECTION
- [SDR 2021FA0000070](https://openairdocs.org/sdr/2021FA0000070.md): Master Relay · faulty · Mar 4, 2021 · N250GC · Cessna 182Q · Engine Starter
  > ENGAGING STARTER CAUSED ALL ELECTRIC POWER TO BE LOST. CYCLING MASTER SWITCH RESTORED POWER, SUBSEQUENT STARTER ENGAGEMENT RESULTED IN LOWER THAN NORMAL CRANKING SPEED. FOUND EXCESSIVE VOLTAGE DROP ACROSS MASTER CONTACTOR. REPLACED WITH LAMAR PMA STS-M24. REMO
- [SDR IKBR2020090900008](https://openairdocs.org/sdr/IKBR2020090900008.md): Turnbuckle · corroded · Sep 9, 2020 · N513SC · Cessna 182Q · Aileron Control System
  > DURING AN ANNUAL INSPECTION WE FOUND THE LEFT FORWARD AND AFT AILERON TURN BUCKLE ENDS P/N MS21252-5LL CORRODED AND PITTED. INSTALLED NEW TURN BUCKLE ENDS AND RIGGED, AS PER CESSNA 182 MM.
- [SDR 2020FA0000352](https://openairdocs.org/sdr/2020FA0000352.md): Cylinder · leaking · Jul 31, 2020 · N11182 · Cessna 182Q · Reciprocating Engine Cylinder Section
  > CONTINENTAL (AIRBOSS) CYLINDER P/N 658598 S/N AC15FA427 INSTALLED ON AUGUST 31, 2015 PER THE ENGINE LOG BOOK. COMPRESSION TEST IN JULY 2020 IDENTIFIED LOW COMPRESSION ON THIS CYLINDER, WITH A LEAK IN THE EXHAUST VALVE. THE EXHAUST VALVE WAS REMOVED AND THE V
- [SDR 2018FA0000472](https://openairdocs.org/sdr/2018FA0000472.md): Resistor · burned · Nov 1, 2018 · N759GV · Cessna 182Q · Instrument Panel
  > PILOT REPORTED SMOKE COMING FROM AVIONICS. INVESTIGATION REVEALED SMOKE COMING FROM THE INSULATION OF THE JUMPERS AT THE VOLTAGE DROPPING RESISTOR AT THE LEFT FUEL QUANTITY GAUGE. THE SMOKE WAS BEING COLLECTED BY THE AVIONICS COOLING FAN AND BLOWN THROUGH THE
- [SDR 2016FA0000327](https://openairdocs.org/sdr/2016FA0000327.md): Shaft · sheared · Jul 15, 2016 · N377H · Cessna 182Q · Fuel Control/Reciprocating Engines
  > CARB HEAT SHAFT WAS FOUND TO BE SHEARED AT RIVET HOLE DURING ACCIDENT INVESTIGATION. SHEARING OF THE SHAFT DID NOT APPEAR TO BE RELATED TO THE ACCIDENT.
- [SDR Y2GR2014102900639](https://openairdocs.org/sdr/Y2GR2014102900639.md): Cylinder · cracked · Oct 29, 2014 · N735MC · Cessna 182Q · Reciprocating Engine Cylinder Section
  > CYLINDERS REMOVED DUE TO LOW COMPRESSION, FOUND 3 CYLINDERS WITH HEAD TO BARREL LEAKAGE.
- [SDR Y2GR2014102900637](https://openairdocs.org/sdr/Y2GR2014102900637.md): Cylinder · cracked · Oct 29, 2014 · N735MC · Cessna 182Q · Reciprocating Engine Cylinder Section
  > CYLINDERS WERE REMOVED FOR LOW COMPRESSION. VISUAL INSPECTION FOUND THREE CYLINDERS LEAKING AROUND THE HEAD TO BARREL THREADS.
- [SDR 2014FA0000196](https://openairdocs.org/sdr/2014FA0000196.md): Rib · cracked · Mar 27, 2014 · N735DX · Cessna 182Q · Fuselage Main, Structure
  > RIGHT AND LT BULKHEAD RIBS WHICH SUPPORT NLG ATTACHMENT, AFT OF FIREWALL, WERE FOUND TO BE CRACKED DURING ANNUAL INSPECTION. NOTE THAT THE ACFT HAS BEEN PREVIOUSLY MODIFIED MY ANOTHER SHOP WITH MODIFIED NLG ASSEMBLY, INSTALLED IAW STC SA02069AK AND ENLARGED N
- [SDR LC1R20140311001](https://openairdocs.org/sdr/LC1R20140311001.md): Cable Assy · broken · Mar 11, 2014 · N759DB · Cessna 182Q · Flight Compartment Equipment
  > SEB07-5 SECONDARY SEAT STOP WAS COMPLIED WITH ORIGINALLY ON 9/23/09 BY INSTALLATION OF KIT NR SK210-174A ON PILOT SIDE & KIT NR SK210-175 ON COPILOT SIDE USING INSTALLATION INSTRUCTIONS D. BOTH CABLES THAT UNLOCK THE INERTIA REELS HAVE BROKEN WHERE THE CABLE
- [SDR CA140326020](https://openairdocs.org/sdr/CA140326020.md): Bearing · corroded · Mar 5, 2014 · Cessna 182Q · Propeller Hub Section
  > (CAN) PROP WAS TESTED DURING A ROUTINE INSPECTION FOR OPERATION. ROUGHNESS WAS NOTED IN CYCLING THE PROPELLER. INVESTIGATION DETERMINED THAT THE BEARINGS AND PRE-LOAD BEARINGS WERE ROUGH DUE TO PITTING. PROP REMOVED FOR O/H.
- [SDR CA140326019](https://openairdocs.org/sdr/CA140326019.md): Case · cracked · Mar 5, 2014 · Cessna 182Q · Reciprocating Engine Power Section
  > (CAN) DURING A ROUTINE 100 HR INSPECTION, OIL LEAK WAS NOTED AT THE FRONT OF THE ENGINE. INVESTIGATION FOR SOURCE OF OIL LEAK LED TO DISCOVERY OF CRACK IN CASE FROM BASE OF NR 3 CYLINDER, FORWARD AND DOWNWARD BEHIND STARTER.
- [SDR CA131107010](https://openairdocs.org/sdr/CA131107010.md): Indicator · inaccurate · Oct 23, 2013 · Cessna 182Q · Fuel Quantity Indicator
  > (CAN) THERE WAS A SIGNIFICANT ERROR IN THE INDICATION OF FUEL QTY, WHICH CREATED AN UNSAFE CONDITION. THE QTY AND FUEL USED INDICATIONS PROVIDED ON THE SAME INSTRUMENT ARE SELF CONTRADICTORY. DEPENDING UPON WHICH ONE THE PILOT NOTICES, OR TAKES AS MORE CREDI
- [SDR 2013FA0000279](https://openairdocs.org/sdr/2013FA0000279.md): Cylinder · separated · May 17, 2013 · N94937 · Cessna 182Q · Reciprocating Engine Cylinder Section
  > AT 10,000 FT, PILOT HEARD A POP AND FELT A VIBRATION, HE PULLED POWER BACK TO IDLE, LANDED AT CLOSEST AIRPORT. PILOT STATED ENGINE HELD OIL PRESSURE UNTIL SHUTDOWN. MECHANIC FOUND NR 1 CYLINDER HAD 5 STUDS BROKEN AND 1 THROUGH STUD BROKEN. NR 6 CYLINDER HA
- [SDR 2013FA0000278](https://openairdocs.org/sdr/2013FA0000278.md): Cylinder · separated · May 17, 2013 · N94937 · Cessna 182Q · Reciprocating Engine Cylinder Section
  > AT 10,000 FT, PILOT HEARD A POP AND FELT A VIBRATION, PULLED POWER BACK TO IDLE, LANDED AT CLOSEST AIRPORT. PILOT STATED ENGINE HELD OIL PRESSURE UNTIL SHUTDOWN. MECHANIC FOUND NR 1 CYLINDER HAD 5 STUDS BROKEN AND 1 THROUGH STUD BROKEN. NR 6 CYLINDER HAD
- [SDR 2011FA0000600](https://openairdocs.org/sdr/2011FA0000600.md): Bushing · defective · Sep 16, 2011 · N94669 · Cessna 182Q · Reciprocating Engine Rear Section
  > DEFECTIVE MAGENTO DRIVE BUSHINGS INSTALLED AT ENGINE O/H. CONTINUE HIS VFR FLIGHT BACK TO WHERE THE ACFT IS BASED. UPON REMOVAL OF THE VACUUM PUMP IT WAS NOTED THAT THE DRIVE SHAFT HAD MELTED/BURNED AWAY. REMOVED ACCESSORY DRIVE PAD AND NOTED THAT THE ACCES
- [SDR 2011FA0000403](https://openairdocs.org/sdr/2011FA0000403.md): Cable · loose · May 17, 2011 · N735DJ · Cessna 182Q · Engine RPM Indicating System
  > AIRCRAFT LOST OIL IN FLIGHT, WAS ABLE TO MAKE IT TO ITS FINAL DESTINATION. THE AIRCRAFT LANDED SAFELY AT AN ALTERNATE AIRPORT. A MECHANIC AT THE AIRPORT HAD DISCOVERED THE TACH DRIVE HOUSING AND TACH CABLE HAD COME LOOSE. THE ENGINE WAS REMOVED AND RETURNED
- [SDR CA100928017](https://openairdocs.org/sdr/CA100928017.md): Fitting · cracked · Sep 23, 2010 · Cessna 182Q · Fuselage, Landing Gear Attach Fittings
  > LOWER NOSE GEAR ATTACHMENT FITTING CRACKED BEHIND OLEO ATTACH SUPPORT. ACFT HAD MAJOR REBUILD 151.2 HRS PREVOUSLY (SUMMER 2008), WHICH INCLUDED FIREWALL, FWD FUSELAGE, NOSE GEAR UPPER ATTACH FITTING AND NOSE GEAR FORK. IT APPEARS THAT THIS FITTING WAS CRACKED
- [SDR 545G2010AUG251](https://openairdocs.org/sdr/545G2010AUG251.md): Magneto · defective · Aug 25, 2010 · N759JM · Cessna 182Q · Magneto/Distributor
  > WHILE TAXIING THE ACFT FOR MX, A MAGNETO CK WAS PERFORMED. THE RT MAGNETO WS ROUGH AND EXHIBITED A LG RPM DROP. THE DIFFICULTY WAS TROUBLESHOT, THE RESULT OF WHICH WAS THE DISCOVERY OF A DEFECTIVE MAGNETO. THE MAGNETO WAS REPLACED WITH AN O/H UNIT AND THE A
- [SDR 2010FA0000898](https://openairdocs.org/sdr/2010FA0000898.md): Support Bracket · cracked · Aug 18, 2010 · N97071 · Cessna 182Q · Battery Box Structure
  > (AIHR) DURING AN ANNUAL INSP, BATTERY SUPPORT BRACKETS WERE FOUND CRACKED. THEY WERE REPLACED WITH NEW PARTS. SEVERAL ACFT OF THIS SERIES HAVE HAD CRACKED BATTERY SUPPORT BRACKETS. RECOMMEND A STRONGER SUPPORT BRACKET BE DESIGNED.
- [SDR 2010FA0000271](https://openairdocs.org/sdr/2010FA0000271.md): Rudder Pedal · loose · Mar 2, 2010 · N759UP · Cessna 182Q · Rudder Control System
  > DURING AN ANNUAL INSP THE PILOT`S RT RUDDER PEDAL WAS FOUND LOOSE. UPON REMOVAL, THE BRAKE ATTACH HOLE AND THE PIVOT HOLES WERE FOUND WORN.
- [SDR CA090902001](https://openairdocs.org/sdr/CA090902001.md): Skin · corroded · Sep 2, 2009 · Cessna 182Q · Fuselage Main, Plate/Skin
  > DURING A NR3 AND NR4 INSP, CORROSION WAS FOUND ON SURFACE OF LWR LT AND RT FUSELAGE SKIN. IT WAS FOUND INSIDE THE COCKPIT BY THE PILOT`S/CO-PILOTS RUDDER PEDALS AREA, BEHIND THE TRIM PANEL. SKIN IN QUESTION ARE ONLY ALCLADDED, NO PRIMER OR PAINT WERE EVER AP
- [SDR 2009FA0000432](https://openairdocs.org/sdr/2009FA0000432.md): Rib · cracked · May 27, 2009 · N769DB · Cessna 182Q · Elevator, Spar/Rib
  > ACFT EQUIPPED WITH STOL CANARDS. FOUND BOTH INBD CANARD ELEVATOR RIBS CRACKED AT ALL BOLT HOLES. BOTH ELEVATORS RETURNED TO MFG FOR MODIFICATIONS AND REPAIRS.
- [SDR CA081014002](https://openairdocs.org/sdr/CA081014002.md): Control Tube · gouged · Oct 8, 2008 · Cessna 182Q · Elevator Control System
  > (CAN) THE BOLT PN AN21-10 ATTACHING THE LT ELEVATOR CONTROL CABLE PN 0510105-90 TO THE LT BELLCRANK CONTROL ARM ASSEMBLY PN 0760686-1 IS RUBBING ON THE LT BELLCRANK CONTROL TUBE SUPPORT PN 0760693-1. THE DAMAGE IS 0.039 DEEP, 1.750 LONG AND 0.250 WIDE.
- [SDR 2008FA0000527](https://openairdocs.org/sdr/2008FA0000527.md): Cam · worn · Jun 19, 2008 · N16MS · Cessna 182Q · Magneto/Distributor
  > REMOVED NEW MAGNETOS PN 6310, SN 07061308 & 07061310. ACCOMPLISHED SB 2-08, MAGNETO CONTACT POINT CAMP PREMATURE WEAR. INSTALLED 2 NEW CONTACT POINT ASSEMBLIES PN M3081; SET "E" GAP AND TIMED TO THE ENGINE. (K)
- [SDR 2008FA0000526](https://openairdocs.org/sdr/2008FA0000526.md): Distributor · worn · Jun 19, 2008 · N16MS · Cessna 182Q · Magneto/Distributor
  > REMOVED NEW MAGNETOS PN 6310, SN 07061208 & 07061310.. ACCOMPLISHED SB 3-08 PREMATURE CARBON BRUSH WEAR. BOTH CARBON BRUSHES HAD PREMATURE WEAR AS DEPICTED IN THE CENTER ILLUSTRATION FIG 1, PAGE 3 OF 5. (K)
- [SDR 2008FA0000256](https://openairdocs.org/sdr/2008FA0000256.md): Panel · corroded · Mar 21, 2008 · N97660 · Cessna 182Q · Passenger Compartment Equipment
  > DURING AN AGING AC INSP OF FLEET AC, VEERING SEVERITY OF SURFACE CORROSION HAS BEEN FOUND IN AC CONTAINING SOUNDPROOFING PANELS SHOWN IN MFG IPC FIG 90. THE HEAVIEST AND MOST SEVERE CORROSION WAS FOUND UNDER SOUNDPROOFING PANELS PN 07000762-23 ITEM 7, PN 1700
- [SDR 2007FA0000543](https://openairdocs.org/sdr/2007FA0000543.md): Needle Valve · missing · Jun 25, 2007 · Cessna 182Q · Fuel Control/Reciprocating Engines
  > AT THE END OF THE FLIGHT, PILOT REPORTED THAT THE ENGINE WOULD NOT IDLE. DURING INSPECTION OF THE CARBURETOR, MECHANIC FOUND THE MIXTURE ADJUSTMENT NEEDLE VALVE MISSING. CARBURETOR WAS REMOVED AND SENT BACK FOR REPAIR.
- [SDR LAT2006F00001](https://openairdocs.org/sdr/LAT2006F00001.md): Elt · inoperative · May 10, 2006 · N4768N · Cessna 182Q · Emergency Locator Beacon
  > G-SWITCH INOPERATIVE, PART NO LONGER AVAILABLE. INSTALL NEW UNIT. (K)
- [SDR 2006FA0000410](https://openairdocs.org/sdr/2006FA0000410.md): Mount · cracked · Apr 6, 2006 · N7551S · Cessna 182Q · Engine Mount Section
  > DURING ANNUAL INSPECTION THE LT AFT ENGINE MOUNT P/N 0751600-1 WAS FOUND CRACKED THRU THE ENGINE MOUNT BOLT AREA.
- [SDR CA050706006](https://openairdocs.org/sdr/CA050706006.md): Alternator · arced · Jul 2, 2005 · Cessna 182Q · DC Generator-Alternator
  > (CAN) DURING APPROACH INTO YYC, THE PILOT NOTED A SHORT, MODERATE BUZZING NOISE IN HEADSET. THERE WAS NO SIGN OF SMOKE BUT THE AMMETER INDICATED ZERO AMPS. THE PILOT LANDED WITH NO OTHER INDICATIONS. THE SYSTEM WAS INSPECTED AND FOUND THAT THE BATTERY STUD
- [SDR 2005FA0000369](https://openairdocs.org/sdr/2005FA0000369.md): Cable · burned · Jan 20, 2005 · N735WR · Cessna 182Q · Fuselage Main, Bulkhead Fuselage wiring
  > DEFECT WAS FOUND AT ENGINE REMOVAL AND FIREWALL CLEANING. THE ELECTRICAL CABLE BETWEEN AUX POWER RELAY AND STARTER RELAY WAS FOUND TO HAVE BURN MARKS AND OBVIOUS DAMAGE TO INSULATION. ADJACENT TO THE DAMAGED PORTION OF THE CABLE WAS A SHEET METAL SCREW IN TH
- [SDR LX52005F00000](https://openairdocs.org/sdr/LX52005F00000.md): Cylinder · cracked · Dec 9, 2004 · N831LL · Cessna 182Q · Reciprocating Engine Cylinder Section
  > ON NORMAL APPROACH TO THE AIRPORT A DISTINCT TICKING SOUND WAS OBSERVED FROM THE ENGINE AREA. THE PILOT REPORTED THAT THE ENGINE HAD GOOD OIL PRESSURE AND POWER AND CONTINUED TO MAKE A NORMAL LANDING AND SHUTDOWN WITHOUT INCIDENT. MAINTENANCE WAS CONTACTED.
- [SDR CA040913003](https://openairdocs.org/sdr/CA040913003.md): Block · worn · Sep 11, 2004 · Cessna 182Q · Aileron Control System
  > (CAN) AILERON SYSTEM CONTROL TUBE ASSEMBLY FORWARD SHAFT P/N 1260141-6/10 WAS WORN 25-30% DUE TO A FAILED CORRODED SUPPORT BEARING P/N 0760633-1. SOME NEEDLES FROM THE BEARING ASSEMBLY WERE MISSING.
- [SDR 2004FA0000743](https://openairdocs.org/sdr/2004FA0000743.md): Cylinder · cracked · Aug 27, 2004 · N735UL · Cessna 182Q · Reciprocating Engine Cylinder Section
  > ON TAKEOFF AT CLIMB OUT, PILOT HEARD LOUD BANG FOLLOWED BY ROUGH ENGINE, DECLARED EMERGENCY AND LANDED WITHOUT FURTHER PROBLEMS. WITH OIL LEAKING FROM COWL, VISUAL INSPECTION NOTED HEAD SEPARATED FROM NR 6 CYLINDER. WITH COWL REMOVED AND CYLINDER OFF, IT WAS
- [SDR FSI072304](https://openairdocs.org/sdr/FSI072304.md): Cylinder Head · separated · Jul 23, 2004 · N97660 · Cessna 182Q · Reciprocating Engine Cylinder Section
  > ON CLIMB OUT THE NR 4 CYLINDER HEAD SEPARATED FROM THE BARREL.
- [SDR 2004FA0000370](https://openairdocs.org/sdr/2004FA0000370.md): Cylinder · separated · Apr 26, 2004 · N97660 · Cessna 182Q · Reciprocating Engine Cylinder Section
  > NR 1 CYLINDER HEAD SEPARATED FROM CYLINDER BASE IN FLIGHT. (SO09200406841)
- [SDR 2004FA0000385](https://openairdocs.org/sdr/2004FA0000385.md): Cylinder Head · separated · Apr 26, 2004 · N97660 · Cessna 182Q · Reciprocating Engine Cylinder Section
  > NR 1 CYLINDER HEAD SEPARATED FROM CYLINDER BASE IN FLT. MAY NEED TO BE ADDED TO AD 2004-08-10.
- [SDR CA040322005](https://openairdocs.org/sdr/CA040322005.md): Magneto · failed · Mar 10, 2004 · Cessna 182Q · Magneto/Distributor
  > (CAN) THE LT MAGNETO FAILED OPERATIONAL MAGNETO CHECK DURING PRE FLIGHT RUN-UP. AT TIMES THE RPM WAS NOTED TO HAVE DROPPED BY 200. DURING SUBSEQUENT TROUBLESHOOTING IT WAS NOTED THAT THE MAGNETO DROP WAS WELL WITHIN LIMITS AT 50 RPM BUT WOULD LATER DROP TO A T
- [SDR 2004FA0000058](https://openairdocs.org/sdr/2004FA0000058.md): Oil Cooler · loose · Jan 10, 2004 · N4810N · Cessna 182Q · Engine Oil Cooler
  > 8/22/2002, OIL COOLER TCM 639171. TACH TIME NOT LOGGED. APPROX 830 SMOH. 12/1/2003 A MAJOR OIL LEAK DEVELOPED AROUND THE OIL COOLER AND THE NR 5 CYL PUSH ROD TUBES. ISOLATED LEAK TO OIL COOLER GASKETS. 1036 SMOH. DURING REMOVAL OF OIL COOLER BASE PLATE, IT
- [SDR 2004FA0000057](https://openairdocs.org/sdr/2004FA0000057.md): Piston · broken · Jan 9, 2004 · N4810N · Cessna 182Q · Reciprocating Engine Power Section
  > ENGINE OVERHAULED. REBARRELED CYL, ECI PISTONS. LOSS OF OIL PRESSURE, 260 STOH, 1043 SMOH. CAUSE, BROKEN NR 2 PISTON, PARTS BLOCKING OIL PICKUP SCREEN. POSSIBLE CAUSES. DEFECTIVE PISTON CASTING, DROPPED PISTON OR IMPROPERLY MACHINED NR 4 RING GROOVE, SQUA
- [SDR 2004FA0000055](https://openairdocs.org/sdr/2004FA0000055.md): Piston · broken · Jan 9, 2004 · N4810N · Cessna 182Q · Reciprocating Engine Power Section
  > REBARRELED CYL, ECI PISTONS. LOSS OF OIL PRESSURE, 260 STOH, 1043 SMOH. CAUSE, BROKEN NR 2 PISTON, PARTS BLOCKING OIL PICKUP SCREEN. POSSIBLE CAUSES. DEFECTIVE PISTON CASTING, DROPPED PISTON OR IMPROPERLY MACHINED NR 4 RING GROOVE, SQUARE CUT BOTTOM OF GRO
- [SDR AUS20031176](https://openairdocs.org/sdr/AUS20031176.md): Nut · loose · Nov 19, 2003 · Cessna 182Q · Reciprocating Engine Cylinder Section
  > (AUS) CYLINDER HOLDDOWN STUD NUTS MISSING OR LOOSE. MISSING NUTS FOUND IN ENGINE COWL.
- [SDR AUS20030749](https://openairdocs.org/sdr/AUS20030749.md): Dowel Pin · misinstalled · Jul 1, 2003 · Cessna 182Q · Propeller Assembly
  > (AUS) CRANKSHAFT PROPELLER MOUNTING FLANGE PROPELLER LOCATING DOWELS INCORRECTLY FITTED. DOWELS HAVE A SLIGHT TAPER WHICH ALLOWS FOR A SLIP FIT INTO THE CRANKSHAFT AND AN INTERFERENCE FIT ONTO THE PROPELLER. THE DOWELS WERE INCORRECTLY FITTED WITH THE INTERFER
- [SDR AUS20030636](https://openairdocs.org/sdr/AUS20030636.md): Regulator · leaking · Jun 12, 2003 · Cessna 182Q · Portable Oxygen System
  > (AUS) PORTABLE OXYGEN SYSTEM REGULATOR LEAKING PAST TEFLON SEAL.OXYGEN LEAKING FROM HIGH PRESSURE SIDE TO LOW PRESSURE SIDE INCREASED TO OUTLET PRESSURE ABOVE THE REGULATED 50PSI. RELIEFVALVE OPENED AND LOW PRESSURE OUTLET TUBING BURST.
- [SDR AUS20030487](https://openairdocs.org/sdr/AUS20030487.md): Mount · cracked · May 2, 2003 · Cessna 182Q · Engine Mount Section
  > (AUS) RT REAR ENGINE MOUNT FOOT CRACKED AT CORNER OF FOOT SUPPORT.CRACK LENGTH APPROXIMATELY 44.45MM (1.75IN). CRACK ALSO FOUND ALONGSIDE WELD OF FOOT. CRACK LENGTH APPROXIMATELY 50.8MM (2IN).FOUND DURING INSPECTION IAW AD/182/4A1.
- [SDR 2003FA0000317](https://openairdocs.org/sdr/2003FA0000317.md): Line · chafed · Mar 21, 2003 · N97832 · Cessna 182Q · Fuel Storage
  > FUEL LINE FROM FUEL SELECTOR VALVE TO FUEL STRAINER. RUDDER PEDALS HAD WORN A DEEP GROOVE IN FUEL LINE.
- [SDR AUS20030375](https://openairdocs.org/sdr/AUS20030375.md): Bar · cracked · Mar 12, 2003 · Cessna 182Q · Rudder Structure
  > (AUS) RUDDER BAR CRACKED AT BASE OF RUDDER PEDAL POST.

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

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

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