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 = 'R182' 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.
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 = 'R182' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CA060316002Terminal · brokenPILOT REPORTED TOTAL LOSS OF ELECTRICAL POWER. FOUND A BROKEN TERMINAL ON ALTERNATOR OUTPUT WIRE. DURING THE GROUND RUN, FOLLOWING REPAIR, ENGINE STARTED NORMALLY FROM THE BATTERY WITHOUT CHARGING FIRST, AND CHARGING SYSTEM FUNCTIONED NORMALLY.SDR 2005FA0001100Float · saturatedENGINE RUNNING EXCESSIVELY RICH AT LOW POWER SETTINGS / TAXI.RAW FUEL RUNNING OUT OF INTAKE BOX AND EXHAUST STACKS.EXAMINATION OF CARBURATOR DISCLOSED FLOAT HAD FLOODED AND SANK.SDR 2005FA0001008Piston Rod · wornNOSE GEAR ACTUATOR FOUND LEAKING DURING PREFLIGHT. MAINTENANCE DISASSEMBLED AND FOUND A GROOVE AROUND THE PISTON ROD (P/N 1280241-2) WHERE THE 'O'RING AND BACKUP RINGS RIDE. REPLACED PISTON ROD ASSEMBLY, INSTALLED NEW SEALS. RE-RIGGED GEAR AND RELEASED A/C.SDR CA050427013Switch · failedSWITCH CONTROLLING FLAP RETRACTION FAILED DURING FLAP RETRACTION AFTER LANDING. FLAPS WERE STUCK AT APPROX 10 DEGREES. FAILURE INSIDE SWITCH AND APPEARS TO INVOLVE BROKEN INTERNAL MECHANISM.SDR 2005FA0000558Actuator · bindingPISTON NUT P/N 9880506-1, DRAGGING ON BEARING END PINS P/N 129009-2. PINS WERE PREVIOUSLY INSTALLED IAW SEB95-20 AND SK210-155. PIN CLEARANCE WAS CHECKED ON INSTALLATION, CLEARANCE WAS .020 AND.024. PINS ARE NOW DRAGGING ON PISTON NUT MAKING IT DIFFICULT TO MOSDR 2005FA0000132Support · damagedWHILE COMPLETING GROUND RUN, PRIOR TO 100 HOUR INSPECTION, NOTICED RUDDER PEDALS DID NOT FEEL RIGHT. FURTHER INVESTIGATION REVEALED THAT THE NUT-PLATES HAD RIPPED THROUGH THE RUDDER PEDAL SUPPORT PIECES. (K)SDR CA041103003Tappet · corroded(CAN) METAL FOUND IN OIL SUCTION SCREEN. AFTER REMOVAL OF NR 1 & 2 CYLINDER FOR INSIDE INVESTIGATION. BOTH HYDRAULIC TAPPET ON THAT CYLINDERS FOUND CORRODED WITH PARTS MISSING ON THE EDGE OF THE BODY. ENGINE REMOVED. FURTHER REPORTS WILL FOLLOW BY THE OVERHAUSDR 2005FA0000759Actuator · obstructedAC NOSE DAMAGE DUE TO FAILURE OF NOSE GEAR TO EXTEND FOR LANDING. PROP LINKAGE RUNS DOWN OUTSIDE NLG TUNNEL, IS ATTACHED TO IT IN 2 PLACES WITH ADEL CLAMPS, STANDOFFS, AND AN3 BOLTS. AFT ATTACH HOLE IS DIRECTLY IN LINE WITH NOSE DOOR ACT ARM, WHICH IS HOLLOWSDR CA040819008Housing · leaking(CAN) ON INSPECTION, LT ENGINE SIDE FOUND VERY OILY, AFTER CLEANING, RUN UP TEST C/O AND OIL LEAK FOUND ON NR2 INTAKE VALVE PUSH ROD HOUSING. A SMALL PIN HOLE FOUND ON THE TUBE (VISIBLE ONLY WITH A MAGNIFYING GLASS). NEW TUBE P/N LW11485 INSTALLED, OPERATIONSDR CA040804010Hinge · crackedDOOR HINGE WAS NOTED AS CRACKED. UPON REMOVAL OF DOOR TO REPLACE HINGE, CRACKS WERE ALSO FOUND IN THE MATING PART OF THE HINGE (0711037-11) AND IN THE UPPER AFT HINGE (0711037-16). THE DOOR RIGGING IS SUCH THAT THE EDGES OF THE DOOR AND AIR FRAME SKINS COME SDR 2004FA0000353Torque Tube · detachedLT RUDDER BAR TORQUE TUBE ASSEMBLY, PN 2260114-5 FAILURE. FAILURE OCCURRED IN FLIGHT RESULTING IN LT SIDE PILOT'S TOTAL LOSS OF LT RUDDER AND STEERING CONTROL. NATURE OF FAILURE; LT OB RUDDER PEDAL SOCKET ON TORQUE TUBE BROKE AWAY FROM THE TORQUE TUBE. THERE SDR RAFAR182Torque Tube · detachedLT RUDDER BAR TORQUE TUBE ASSEMBLY, PN 2260114-5 FAILURE. FAILURE OCCURRED IN FLIGHT RESULTING IN LT SIDE PILOT'S TOTAL LOSS OF LT RUDDER AND STEERING CONTROL. NATURE OF FAILURE; LT OB RUDDER PEDAL SOCKET ON TORQUE TUBE BROKE AWAY FROM THE TORQUE TUBE. THERE ISDR AUS20040126Valve · separated(AUS) CARBURETOR ACCELERATOR PUMP DISCHARGE CHECK VALVE LOOSE AND SEPARATED.SDR 2004FA0000234Plate · crackedDURING AN INSPECTION, THE BULKHEAD MOUNTING PLATES WERE FOUND CRACKED AND BROKEN AROUND THE HOLES THROUGH WHICH THE PROPELLER MOUNTING STUDS PASS. THIS CONDITION IS FOUND VERY OFTEN AND THE PLATES REALLY NEED TO BE REDESIGNED TO NOT CRACK AS EASILY AS THEY DOSDR 2004FA0000195Plug · looseDURING CLIMB OUT ENGINE RPM WOULD START CLIMBING AND THE PROP CONTROL HAD NO EFFECT ON REDUCING RPM. DURING TROUBLESHOOTING FOUND THE REAR CRANKSHAFT PLUG HAD COME LOOSE IN THE CRANKSHAFT ALLOWING OIL TO BYPASS BACK TO THE ENGINE SUMP. UNABLE TO DETERMINE THSDR 2004FA0000075Contactor · shortedA NEW LIGHT WEIGHT STARTER WAS INSTALLED WHEN THE EXISTING STARTER FAILED. THE STARTER CONTACTOR WELDS ITSELF TOGETHER AFTER ABOUT 15 STARTS. 2 NEW MFG CONTACTORS WERE INSTALLED AND HAD THE SAME RESULTS. A HEAVY DUTY CONTACTOR HAS BEEN INSTALLED IAW MFG SERSDR 2003FA0001231Fitting · crackedDURING ANNUAL INSPECTION FOUND THE AFT ATTACH FITTING FOR THE NOSE GEAR ACTUATOR CRACKED IN TWO PLACES. THE CRACKS START AT THE ACTUATOR PIN BOSS AND PROGRESS UPWARD THROUGH THE FLANGE AREA TO THE EDGE OF THE FITTING. UNABLE TO DETERMINE CAUSE (AGE, FATIGUE SDR AUS20030923Housing · cracked(AUS) LANDING GEAR ACTUATOR BODY CRACKED. FOUND DURING INSPECTION IAW CESSNA SB 01-2 REV1.SDR 2003FA0000770Hose · rottedVACUUM SUPPLY LINE (MFG PART NO S 5202-10) LINES FROM THE INLET FILTER TO THE INSTRUMENTS (EASTMAN HY---ON B906 REDI- PLASTICE LINE FELL APART WHEN TOUCHED. THIS AIRCRAFT IS AN ORIGINAL INSTALLATION AND THE SECOND WITH THIS PLASTIC INSTALLED.SDR AUS20030621Pin · sheared(AUS) NOSE LANDING GEAR DOWNLOCK PIN SHEARED.SDR 2003FA0000608Control Cable · looseWHEN RUDDER IS DEFLECTED TO THE FAR RIGHT, THE RIGHT RUDDER CABLE GOES SLACK AND HANGS UP UNDER THE NUT FOR THE ELEVATOR PULLEY CLUSTER LOCATED BY THE FUSELAGE RIGHT SIDE ACCESS PANEL. TO PREVENT THIS, INSTALLED A SECOND NUT ON THE BOLT AND INSTALLED AN AN4-1SDR 2003FA0000408Control Cable · jammedWHEN THE RUDDER IS DEFLECTED TO THE FAR RIGHT , THE RIGHT RUDDER CABLE GOES SLACK AND HANGS UP UNDER THE NUT FOR THE ELEVATOR PULLEY CLUSTER LOCATED BY THE FUSELAGE RIGHT SIDE ACCESS PANEL. TO PREVENT THIS A GUARD WAS SUGGESTED TO PREVENT THE CABLE FROM SLIPPSDR 2003FA0000389Control Cable · out of rigWHEN THE RUDDER IS DEFLECTED TO THE FAR RIGHT, THE RIGHT RUDDER CABLE GOES SLACK AND HANGS UP UNDER THE NUT FOR THE ELEVATOR PULLEY CLUSTER LOCATED BY THE FUSELAGE RIGHT SIDE ACCESS PANEL. TO PREVENT THIS A GUARD WAS SUGGESTED TO PREVENT THE CABLE FROM SLIPPISDR 2003FA0000709Actuator · crackedCRACK INDICATIONS IN THE 2.28 INCH BORE. CRACK FOUND WHILE INSPECTING ACTUATOR IAW SB 01-2 REV 1. RIGHT MAIN GEAR.SDR 2002FA0001026Line · failedWHEN PILOT SELECTED GEAR DOWN AND PRESSURE WAS APPLIED TO DOWN HOSE. THE HOSE FAILED AT THE SWAGED END BLOWING ALL HYDRAULIC FLUID OVERBOARD. RECOMMEND CLOSER INSPECTION OF HOSES AND A MANDATORY TIME CHANGE OR BOTH HOSES. (PN S217840102) DOWN AND (PN S21784SDR 2002FA0000916Carburetor · leakingPILOT BROUGHT IN AIRCRAFT WITH ROUGH RUNNING ENGINE. ENGINE WOULD SURGE BELOW 900 RPM AND MIXTURE CONTROL WOULD NOT SHUT DOWN ENGINE. FOUND FUEL DRIPPING FROM CARBURETOR THROAT. THE CARBURETOR WAS REPLACED AND OPERATION RETURNED TO NORMAL.SDR 2002FA0000506Indicator · misrepairedA FUEL PRESSURE GAUGE WAS RETURNED TO MFG. FOR REPAIR. THEY SENT A REPLACEMENT GAUGE IN ITS PLACE. THE NEW GAUGE CAME WITH AN AN816-2D NIPPLE THREADED IN THE PRESSURE INLET PORT. THE PROBLEM IS THE TEFLON THREAD TAPE WAS IMPROPERLY APPLIED. NOT ONLY DID ITSDR 2002FA0000300Plate · crackedDURING A 50 HOUR INSPECTION THE SPINNER ASSEMBLY WAS DETECTED TO BE VERY LOOSE ON THE PROP. UPON FURTHER EXAMINATION BOTH SPINNER ATTACH PLATES WERE FOUND CRACKED ALL THE WAY AROUND FOUR OF SIX PROP ATTACH BOLT HOLES. CRACKS EMANATED FROM THE CORNER OF EACH SDR 2002FA0000039Pivot Assy · crackedFORWARD BEARING AREA OF RIGHT MAIN GEAR PIVOT WAS DETERMINED TO BE CRACKED AND LEAKING BRAKE FLUID. THE PIVOT ASSY WILL BE REPLACED WITH A NEW PIVOT ASSY PART NUMBER 2241102-13 AS OUTLINED IN MFG SB.SDR 2002FA0000040Pivot Assy · crackedFORWARD BEARING AREA OF LEFT MAIN GEAR PIVOT WAS DETERMINED TO BE CRACKED AND LEAKING BREAK FLUID. THE PIVOT ASSEMBLY WAS REPLACED WITH A USED SERVICEABLE PIVOT ASSEMBLY OF THE SAME PART NUMBER.SDR 2001FA0000593Wheel · crackedCRACK, 1.25 INCHES IN LENGTH, EMANATING FROM BOLT HOLE.SDR 2001FA0000479Accell Pump · stiffCARBURETOR CHANGED BECAUSE OF ACCELERATOR PUMP STIFFNESS. PRECISION SIL CW AND HAD NO EFFECT ON EITHER CARBURETOR.SDR 2001FA0000416Clamp · bentNOSE GEAR FAILED TO EXTEND, BUT FELL OUT WHEN AIRCRAFT WAS LIFTED FROM RUNWAY. ON JACKS, GEAR OPS WAS NORMAL. THIS CLAMP WAS BENT WHICH MAY HAVE ALLOWED SHIMMY DAMPENER TO JAM THE GEAR. MAY HAVE BEEN DAMAGED FROM TUG OVER TURNING THE GEAR.SDR 2001FA0000414Fuel Strainer · backed outDURING ANNUAL INSPECTION NOTICED FUEL STRAINER STANDPIPE HAD BACKED OUT AND WAS ABLE TO PULL IT OUT OF TOP ASSEMBLY WITH FINGERS.SDR 2001FA0000311Contactor · failedCONTACTOR FAILED/ CLOSED CAUSING STARTER TO BURN OUT. THIS IS SECOND FAILURE OF A NEW CONTACTOR IN LESS THAN 140 HOURS. (ONE STARTER CONTACTOR, ONE MASTER CONTACTOR)SDR CA011102008Crankcase · cracked(CAN) THE PILOT NOTICED AFTER AN HOUR OF FLIGHT THAT THE OIL PRESSURE WAS DROPPING. HE PERFORMED A PRECAUTIONARY LANDING ON THE ROAD WITHOUT ANY PROBLEM. AFTER INSPECTION OF THE ENGINE, A CRACK WAS FOUND ON THE ENGINE BLOCK BETWEEN NR 1 AND 3 CYLINDERS. THE ENSDR AUS20010677Flap · damaged(AUS) RH TRAILING EDGE FLAP TOP AND BOTTOM SKINS, LEADING EDGE SKIN AND SPAR DAMAGED. INVESTIGATION FOUND THE DAMAGE WAS CAUSED BY THEINBOARD FORWARD FLAP ROLLER JAMMING DUE TO EXCESSIVE WEAR OF THEFLAP TRACK AND ROLLERS.SDR 2001FA0000478Accell Pump · stiffTHE CARB HAD TO BE CHANGED BECAUSE OF STIFF THROTTLE. THE CAUSE BEING THE ACCELERTOR PUMP, LINKAGE RODS. PRECISION SIL-MS-1CW. HAD NO EFFECT ON THE PUMP RODS.SDR 2001FA0000085Plate · crackedTHIS PROPELLER INSTALLATION UTILIZES 2 SPINNER AFT BULKHEAD ATTACH PLATES, PN A1639-9. BOTH PLATES WERE FOUND TO BE CRACKED WITHIN 50 HR OF INSTALLATION OF PROP AFTER OVERHAUL. BECAUSE BULKHEAD ATTACHMENT PLATES ARE INSTALLED UNDER ATTACHMENT NUTS, PN A1639-SDR AUS20010422Bearing · failed(AUS) COPILOTS CONTROL COLUMN BEARING BLOCK NEEDLE ROLLER BEARING WORNOUT AND THE ROLLERS DISLODGED DUE TO LACK OF LUBRICATION. THE ROLLER BEARING SHAFT GROOVED FROM VIBRATION INDUCED WEAR.SDR CA011102006Spring · broken(CAN) ENGINE VIBRATION WHILE IN FLIGHT. AFTER INSPECTION, THE NR 2 ENGINE CYLINDER WAS FOUND WITHOUT COMPRESSION. THE ADMISSION VALVE WAS FOUND INOPERATIVE. A NEW CYLINDER WAS INSTALLED AND SUCCESSFUL ENGINE TESTS WERE CARRIED OUT. THE CYLINDER WAS SENT TO A RSDR 20010425CW007Tube · looseDURING ANNUAL INSPECTION THE TWO ALUMINUM RIVETS SECURING THE FORWARD END OF SHAFT WERE FOUND LOOSE AND THE BUCK TAILS MISSING . THE SQUARK TUBE PORTION OF ASSEMBLY APPEARS TO BE ALUMINUM. THE FORWARD THREADED END IS STEEL. THE FIT OF THE TWO PARTS IS NOT VSDR 20010410AP004Rib · crackedDURING AN ANNUAL INSPECTION FOUND THE RT HORIZONTAL STABILIZER INBOARD LEADING EDGE RIB CRACKED. DETECTED CRACK DUE TO EXCESSIVE SKIN PLAY AT RIB AND A WORKING FASTNER. CONFIRMED CRACK USING A BORESCOPE. DISASSEMBLED THE EMPENNAGE ENOUGH TO FACILITATE RIB RESDR 20010321CW005Plate · missingWHILE IN FLIGHT, THE C50462 SPINNER MOUNTING PLATES FAILED, RELEASING THE SPINNER FROM THE AIRCRAFT. THE PROPELLER BECAME LOOSE ON THE CRANKSHAFT DUE TO THE MISSING PLATES. WAS DAMAGED BEYOND REPAIR DUE TO SEVERE FRETTING. A NUMBER OF THE ATTACHING STUDS WESDR 20010322CW001Pin · shearedWHILE ATTEMPTING TO TRIM THE AIRCRAFT FOR STRAIGHT AND LEVEL FLIGHT, THE PILOT RAN OUT OF NOSE DOWN TRIM. AFTER A SUCCESSFUL LANDING AND MAINTENANCE INVESTIGATION IT WAS FOUND THAT THE ELEVATOR TRIM TAB WAS NOT MAKING IT ALL THE WAY TO THE NOSEDOWN/ TABUP LIMSDR 20010228CW011Battery · corrodedUPON INSPECTION OF ELT AND BATTERIES, WERE FOUND TO BE CORRODED AND SWELLING, THE BATTERY COMPARTMENT IS WET WITH A LIQUID. COMPOSITION OF LIQUID UNKNOWN. ELT IS INSIDE TAIL SECTION OF AC AND NOT SUBJECT TO WATER EXPOSURE.SDR 20010206CW004Seat Track · misinstalledDURING COMPLIANCE OF AD, FOUND SEAT TRACKS INSTALLED WITH CHERRY MAX BLIND FASTENERS AND OVERSIZED RIVETS, WHICH DID NOT MEET THE REQUIRED 2D EDGE DISTANCE REQUIREMENT. FLOOR AND TRACKS HAD TO BE REPLACED AND SUB FLOOR REPAIRED. CHERRY MAX RIVETS ANRE NOT APSDR 20010508CW010Line · leakingSTEELE BRADED FUEL LINE FOUND SEVERLY LEAKING AT ANNUAL INSPECTION. NOTICED ENGINE COMPARTMENT VERY WASHED FROM FUEL LEAKING WHILE RUNNING. FUEL LINE WAS PRESSURE LINE FROM ENGINE FUEL PUMP TO CARBURETOR. INSTALLED 2.97 391TT VERY COMMON PROBLEM. TIME LIMISDR 20001204SH014Seat · brokenREAR ATTACH POINT ON LOWER SEAT WHERE IT ATTACHES TO THE PEDESTAL ASSEMBLY. ONE SIDE BROKEN OFF THE OTHER SIDE IS CRACKED. BROKE AT CUT-OUT FOR SEAT PIVOT BRACKET PN 0514060-5. (X)SDR 20000912SH001Hose · separatedHOSE SEPARATED AT SWAGED END CAUSING LOSS OF FLUID AND NOSE GEAR TO FALL INTO AIRSTREAM. CESSNA INSPECTION CHECKLIST CALLS OUT FOR THIS HOSE ALONG WITH REST OF LANDING GEAR HOSES TO BE REPLACED ON CONDITION FOR THIS AIRCRAFT. SUBMITTER RECOMMENDED CHANGING R
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