Cessna 182G

Service difficulty reports · 33

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Query with SQL
duckdb -csv -c "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 = '182G'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 2018FA0000485Bolt · crackedDURING ACCIDENT INVESTIGATION OF N3267S, THE FORWARD OUTBOARD ATTACH BOLT P/N NAS147-34 HAD A PREEXISTING CRACK AT THE BEGINNING OF THE THREADS FROM THE SHAFT WITH THE PRESENCE OF CORROSION. THIS LEAD TO AN INSTANTANEOUS FAIL OF THE BOLT UPON LANDING AND SPRINOct 31, 2018 · N3267S · Cessna 182G · Main Landing Gear Strut/Axle/TruckSDR CA120718005Snap Ring · failed(CAN) WHILE IN CRUISE FLIGHT, PILOT NOTICED INCREASED RPM AND VIBRATION. PILOT DECREASED RMP AND CARRIED OUT A PRECAUTIONARY LANDING. PROPELLER TECH HISTORY, PROPELLER O/H 21-FEB-11 -AT 1.3 TSO PROPELLER BLADES REPAINTED DUE TO POOR ADHESION -AT 36.1 TSO ACJul 13, 2012 · Cessna 182G · Propeller AssemblySDR 2011FA0000675Casting · crackedCASTING CRACK FOUND BY VISUAL INSPECTION DURING COURSE OF ANNUAL INSPECTION. THE CRACK IS LOCATED ON THE FORWARD END OF THE SUPPORT CASTING AND RUNS FROM 1/4 INCH FROM MOUNT HOLES ON THE OUTBOARD SIDE TO WITHIN 1/4 INCH OF THE MOUNT HOLES ON THE INBOARD SIDE Oct 13, 2011 · N4944P · Cessna 182G · Fuselage, Landing Gear Attach FittingsSDR 2008FA0000146Torque Link · crackedON INSPECTION, A CRACK WAS IDENTIFIED IN THE FORGING FOR THE UPPER TORQUE LINK FOR THE NOSE LANDING GEAR. THE CRACK WAS ON BOTH SIDES OF THE BEAM SECTION ADJACENT TO THE EXTENSION STOP FOR THE GEAR.(AFT SIDE)Jan 29, 2008 · N82BG · Cessna 182G · Nose/Tail Landing GearSDR 2007FA0000840Carburetor · failedPILOT REPORTED THAT AFTER A NORMAL START, HE WAS UNABLE TO ADVANCE THE THROTTLE CONTROL TO CRUISE OR TAKEOFF POWER. A PARTIAL DISASSEMBLY OF THE CARBURETOR REVEALED THAT THE AIR METERING PIN/AIR METERING JET WAS BLOCKING THE THROTTLE SHAFT TRAVEL. THE CARBURAug 18, 2007 · N2347R · Cessna 182G · Fuel Control/Reciprocating EnginesSDR CA070823010Torque Tube · loose(CAN) MINOR PLAY (UP AND DOWN) ON THE RT ELEVATOR CAUSE BY LOOSE RIVETS ON THE TORQUE TUBE (TC NR 20070823010)Jul 25, 2007 · Cessna 182G · Elevator StructureSDR CA060327004Torque Link · cracked(CAN) NOSE GEAR UPPER TORQUE LINK WAS FOUND CRACKED INSIDE UPPER CORNER ON THE LT SIDE. FORGING NR 0543034-497, 2014 KAE-2A (TC NR20060327004)Mar 21, 2006 · Cessna 182G · Nose/Tail Landing GearSDR CA041108003Spring · brokenLEFT HAND MAIN LANDING GEAR SPRING ASSEMBLY BROKE OF AT FUSELAGE WHILE TAXIING FOR FLIGHT. THERE WAS NO VISUAL EVIDENCE OF A PREVIOUS CRACK. THE GEAR LEG WAS SENT TO TRANSPORT SAFETY BOARD TO BE ANALYZED.Oct 25, 2004 · Cessna 182G · Landing Gear Retraction/Extension SystemSDR AUS20030693Rivet · faulty(AUS) AILERON MASS BALANCE WEIGHT ATTACHMENT RIVETS FAULTY. APPROXIMATELY HALF OF THE RIVETS FAILED TESTING AND INSPECTION IAW AD/CESSNA180/28.Jul 7, 2003 · Cessna 182G · AileronsSDR 2003FA0000660Bulkhead · crackedTHIS DEFECT WAS FOUND AS A RESULT OF INSPECTION REQUIRED BY AD. THIS PART WAS REPLACED AT THIS TIME JUNE 17, 2003. TT 5187.97. THIS REPORT REQUIRED BY AD PART (I).Jun 17, 2003 · N2157R · Cessna 182G · Fuselage Main, BulkheadSDR 2002FA0000589Air Box · crackedSEVERAL CRACKS IN HOUSING, BOTH IN ALUMINUM AND STAINLESS STEEL. SERVICEABLE PART INSTALLED ABOUT 375 HOURS OPERATING TIME. SUGGEST MORE ATTENTION BE GIVEN THIS ITEM AND THE WAY IT IS ATTACHED, FOR SECURITY. HIGH VIBRATION AREA. CHECK PROPELLER FOR BALANCEApr 10, 2002 · N3736U · Cessna 182G · Engine Air Intake SystemSDR 20010320CW006Hub · crackedEDDY CURRENT INSPECTION REVEALED A CRACK IN THREADS OR NR1 BLADE HUB SOCKET AT APPROX 7 OCLOCK POSITION WHEN VIEWED FROM SIDE WITH CYLINDER END POINTING UP AND APPROX 1.25 INCH IN LENGTH HUB WAS NOT MODIFIED TO OIL FILL CONFIGURATION.Feb 14, 2001 · N3107S · Cessna 182G · Propeller Hub SectionSDR CA001103009Generator · failed(CAN) 4 GENERATORS WERE TRIED ON THIS AIRCRAFT OVER A PERIOD OF 15 - 18 MONTHS, THE END RESULT WAS INSTALLING AN ALTERNATOR KIT, AS THE COMPANY OVERHAULED THE GENERATOR WAS DOING SUBSTANDARD WORK.Oct 20, 2000 · Cessna 182G · DC Generator-AlternatorSDR 20000505SH019Muffler · deterioratedDURING ANNUAL INSPECTION, THE LT INTERNAL BAFFLE WAS FOUND TO HAVE SEPARATED AND WAS PARTIALLY BLOCKING THE EXHAUST PORT IN THE MUFFLER. UPON REMOVAL, THE RT EXHAUST STACK WAS FOUND BADLY DETERIORATED WITH SEVERAL PIECES MISSING. ONLY MINOR EXHAUST LEAK WASMar 29, 2000 · N2354R · Cessna 182G · Engine Noise SuppressorSDR 20000505SH018Muffler · separatedDURING ANNUAL INSPECTION, THE LT INTERNAL BAFFLE WAS FOUND TO HAVE SEPARATED AND WAS PARTIALLY BLOCKING THE EXHAUST PORT IN THE MUFFLER. UPON REMOVAL, THE RT EXHAUST STACK WAS FOUND BADLY DETERIORATED WITH SEVERAL PIECES MISSING. ONLY MINOR EXHAUST LEAK WASMar 29, 2000 · N2354R · Cessna 182G · Engine Noise SuppressorSDR AU000015Fuel Cell · contaminated(AUS) FUEL SYSTEM CONTAMINATED WITH ETHYLENE DIAMINE. MOBIL BRAND FUEL WAS USED OUTSIDE OF PUBLISHED DATES. CARBURETTOR ALSO CONTAMINATED.Mar 9, 2000 · Cessna 182G · Fuel StorageSDR 99ZZZX4154Data Plate · detachedPARTIAL POWER LOSS AT FULL THROTTLE WAS EXPERIENCED ON ACFT REGISTERED, 6Y-JDK, PRIOR TO THE COMMENCEMENT OF TAKEOFF ROLL AT KIRKVINE AERODROME IN JAMACIA. SEVERAL FULL POWER CHKS ACHIEVED ONLY 2,350 RPM INSTEAD OF THE REQUISITE 2,600 RPM. ACFT RETURNED TO ROct 5, 1999 · N6YJDK · Cessna 182G · Engine Collector/Tailpipe/NozzleSDR 99ZZZX3192Fitting · crackedFOUND CRACK IN LOWEST (AS INSTALLED) RIVET HOLE. INSPECTING SIMILAR (1963-1974) 182'S, SUBMITTER HAS FOUND 3 CRACKS IN A MONTH.Aug 10, 1999 · N3111S · Cessna 182G · Wing Miscellaneous StructureSDR 98ZZZX3306Drain Valve · malfunctionedOWNER STATED ONE VALVE WOULD NOT OPEN AND A 'GREENISH STICKY' SUBSTANCE WAS FOU ND IN THE OTHER. REPLACED BOTH WING TANK DRAIN VALVES. CHECKED AND CLEANED ALL FUEL SYSTEM SCREENS AND FILTERS. NO DEFECTS NOTED. DRAINED 5 GALLONS FROM EACH TANK, NO DEBRIS NOAug 7, 1998 · N2105R · Cessna 182G · Fuel StorageSDR CA980814005Skin · wrinkled(CAN) ON LANDING OF FLOAT EQUIPPED AIRCRAFT HIT LARGE WAVE. ON RETURN TO DOCK, INVESTIGATON FOUND THE SIDE SKINS AND LOWER COWL WERE WRINKLED. FURTHER EXAMINATION FOUND THE FIREWALL AND BELLY SKINS WERE ALSO WRINKLED. NEW REINFORCED FIREWALL AND TUNNEL INSTAug 6, 1998 · Cessna 182G · Fuselage Main, Plate/SkinSDR 98ZZZX2449Chain · failedTHE ELEVATOR TRIM BECAME INOPERATIVE WHEN INSPECTED. THE LAST PIVOT PIN OF THE CHAIN WAS FOUND SEPARATED FROM THE SIDE LINK. THIS IS DIFFICULT TO INSPECT BECAUSE IT IS LOCATED INSIDE THE CENTER CONSOLE.Jun 1, 1998 · Cessna 182G · Elevator Tab Control SystemSDR 97ZZZX4959Piston · crackedSIX ENGINE PISTONS FOUND CRACKED IN PISTON PIN BOSS. CRACKS WERE ALL IN SAME AREA, UPPER PIN BOSS RUNNING PARALLEL TO PISTON PIN. ONE PISTON HAD LOST ONE-FOURTH OF THE CASTING AROUND PIN. THIS CONDITION DID NOT CAUSE ANY OPERATIONAL PROBLEMS. JUDGING FROM Nov 14, 1997 · N3235S · Cessna 182G · Reciprocating Engine Cylinder SectionSDR 97ZZZX4798Torque Link · crackedDURING AN ANNUAL INSPECTION, THE UPPER TORQUE LINK OF THE NOSE LANDING GEAR WAS FOUND CRACKED IN THE RADIUS OF THE UPPER FORGED RIB ADJACENT TO THE ATTACH BOLT HOLE. BOTH SIDES WERE CRACKED.Nov 5, 1997 · N3281S · Cessna 182G · Nose/Tail Landing Gear Strut/AxleSDR CA970609023Blade · stone damage(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. STONE DAMAGE ON FACE AND LEADING EDGE OF PROPELLER BLADES. DAMAGE REPAIRED AND CYLINDER SUPPORT REPLACED.May 24, 1997 · Cessna 182G · Propeller Blade SectionSDR 97ZZZX1861Gear Leg · rustedDURING ANNUAL INSPECTION, RUST WAS NOTICED ON THE LANDING GEAR LEGS (MAIN GEAR) MOST SEVERE RUST WAS FOUND UNDER STOP. METAL WAS RUSTED TO THE POINT OF 'DELAMINATION'. THE RUST APPEARED TO HAVE BEEN CAUSED BY THE GLUE THAT WAS USED BY CESSNA TO HELP ATTACH THMar 1, 1997 · N3791U · Cessna 182G · Main Landing Gear Strut/Axle/TruckSDR 97ZZZX1860Gear Leg · rustedDURING ANNUAL INSPECTION, RUST WAS NOTICED ON THE LANDING GEAR LEGS (MAIN GEAR) MOST SEVERE RUST WAS FOUND UNDER STOP. METAL WAS RUSTED TO THE POINT OF 'DELAMINATION'. THE RUST APPEARED TO HAVE BEEN CAUSED BY THE GLUE THAT WAS USED BY CESSNA TO HELP ATTACH THMar 1, 1997 · N3791U · Cessna 182G · Main Landing Gear Strut/Axle/TruckSDR 97ZZZX867Bulkhead · crackedBULKHEAD WAS FOUND CRACKED AT LEFT RUDDER STOP BOLT AREA. THIS INSPECTION IS REQUIRED BY AD 72-07-09. THE CRACK WAS NOT IN THE AREA CALLED OUT IN THE AD. THE BULKHEAD IS CALLED OUT FOR REPLACEMENT IF FOUND CRACKED.Feb 1, 1997 · N28EM · Cessna 182G · Fuselage Main, BulkheadSDR 96ZZZX4985Line · chafingINSPECTION FOUND THE PINS ON THE JUMP DOOR THAT EXTEND INTO THE DOOR POSTS WERE HITTING THE FUEL LINES THAT RUN PARALLEL WITH THE DOOR POST, BOTH FORWARD AND AFT, ON THE RIGHT SIDE. SPLICED IN A NEW SECTION OF TUBING AND ROUTED THE LINES OUT AND AROUND THE PISep 6, 1996 · N2444R · Cessna 182G · Aircraft Fuel Distribution SystemSDR 96ZZZX4984Line · chafingINSPECTION FOUND THE PINS ON THE JUMP DOOR THAT EXTEND INTO THE DOOR POSTS WERE HITTING THE FUEL LINES THAT RUN PARALLEL WITH THE DOOR POST, BOTH FORWARD AND AFT, ON THE RIGHT SIDE. SPLICED IN A NEW SECTION OF TUBING AND ROUTED THE LINES OUT AND AROUND THE PISep 6, 1996 · N2444R · Cessna 182G · Aircraft Fuel Distribution SystemSDR CA960126035Cylinder · cracked(CAN)IN CRUISE ENGINE BEGAN TO RUN ROUGH, AIRCRAFT LANDED AT NEAREST AIRPORT AND GROUND INSPECTION FOUND #5 CYLINDER CRACKED AT THE EXHAUST VALVE & SPARKK PLUG HOLE. CYLINDER REPLACED & AIRCRAFT RETURNED T O SERVICE.Dec 30, 1995 · Cessna 182G · Reciprocating Engine Cylinder SectionSDR 95ZZZX6564Fuel Cap · leakingFUEL CAPS BEGAN LEAKING CAUSING LOSS OF FUEL DURING FLIGHT. REPLACED WITH FUEL CAPS BY MONARCH AIR TYPE SA2376CE.Oct 25, 1995 · N2468R · Cessna 182G · Fuel StorageSDR 95ZZZX5957Generator · shortedINVESTIGATION FOR COCKPIT ODOR FOUND UPON OPENING THE BATTERY COMPARTMENT, THE BATTERY WAS EXTREMELY HOT AND MOST OF THE ELECTROLYTE HAD BOILED OUT. TROUBLESHOOTING REVEALED THE FIELD COIL HAD GROUNDED OUT IN THE GENERATOR.Sep 21, 1995 · N3289S · Cessna 182G · DC Generator-AlternatorSDR 95ZZZX2317Bracket · brokenDURING ANNUAL INSPECTION, GENERATOR BELT WAS FOUND LOOSE. INVESTIGATION SHOWED THE REAR BRACKET OF THE GENERATOR WAS BROKEN. THE BRACKET WAS REPLACED. A/C TOTAL TIME 4,645 HRS. TIME ON PART UNKNOWN.Apr 28, 1995 · N3281S · Cessna 182G · Alternator-Generator Drive
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