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 = 'SF340A' 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 = 'SF340A' 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 OZCA20141218008Smoke Detector · inoperativeCARGO SMOKE DETECTORS 1, 2, 3 & 4 INOPERATIVE. TROUBLE SHOT CARGO SMOKE SYS & FOUND FAULTY NR 2 B1 COMPARTMENT SMOKE DETECTOR INOPERATIVE. R & R NR 2 SMOKE DETECTOR IAW MM. OPERATIONAL CHECKED NORMAL.SDR OZCA20141211007Gearbox · failedON APPROACH, RT ENG SURGED. RIGHT ENG OIL PRESS INDICATOR AT RED LINE. TROUBLE SHOT & FOUND RT ENG PROPELLER GEAR BOX CASE CRACKED DUE TO INTERNAL FAILURE. R & R PROPELLER GEAR BOX & POWER UNIT ASSEMBLY IAW MM. PERFORMED GND RUNS & LEAK CHECKS.SDR OZCA20141207006Clamp · looseRIGHT TAIL PIPE HOT WARNING IN FLIGHT. INSPECTED RT ENG. FOUND LOOSE CLAMP ON LOW PRESS BLEED LINE. TORQUED CLAMP IAW MM. PERFORMED OPERATIONAL CHECK OF SYS. OPERATIONAL CHECKED SATISFACTORY IAW MM. COMPLIED WITH PARAGRAPH C OF AIRWORTHINESS DIRECTIVE 20SDR OZCA20141119004Smoke Detector · inoperativeAIRCRAFT RETURNED DUE TO CARGO SMOKE INDICATION. AFTER TROUBLESHOOTING, FOUND ZONE A CARGO SMOKE DETECTOR INOPERATIVE. R & R ZONE A CARGO SMOKE DETECTOR IAW MM CHAPTER 26. OPERATIONS CHECKED OK.SDR OZCA20141029003Clamp · looseTAKEOFF ABORTED AT 105 KT DUE TO RT ENG OVER TEMP INDICATION. INSPECTED RT ENG FOR BLEED LEAKS. FOUND RT PRIMARY BLEED TUBE & LOW PRESS BLEED TUBE CLAMPS LOOSE. SECURED CLAMPS AT BLEED TUBES IAW MAINTENANCE MANUALS. PERFORMED GND POWER RUNS. ALL POWER RUNSSDR OZCA20141024002Warning Light · false indicationTAKEOFF ABORTED DUE TO LT TAIL PIPE HOT INDICATION. INSPECTED LT TAIL PIPE FIRE DETECTOR WIRE HARNESS & FOUND NO DEFECTS. INSPECTED LT TAIL PIPE FIRE DETECTOR SENSORS & SEALANT & NOTED WATER ON SENSORS. CLEANED SENSORS . PERFORMED OPS CHECK AT GROUND IDLE SDR OZCA20140922001Control Cable · damagedDURING FLIGHT CREW EXPERIENCED A LOSS OF THE NR 2 PROPELLER RPM. ACFT RETURNED BACK TO AIRPORT & LANDED SAFELY. INSPECTED THE ACFT & FOUND THE RT WING TO NACELLE CONTROL CABLE AT FAULT. AFFECTED CABLE WAS REPLACED. RIGGING CHECKS WERE SATISFACTORY & ENG RUSDR OZCA20140327001Control Box · faultyRIGHT ENGINE FIRE WARNING, RETURNED TO AIRPORT. REPLACED RT FIRE DETECTOR CONTROL BOX WITH AN INSPECTED PART & ACFT WAS RELEASED TO SERVICE.SDR TSAA20140206003Flap · malfunctionedFLIGHT KH1104, ON APPROACH FLAPS WOULD NOT EXTEND. ACFT DECLARED AN EMERGENCY & LANDED IN A NO-FLAP CONDITION. ACFT LANDED UNEVENTFULLY & TAXIED BACK TO PARKING AREA.SDR PNSA2014011504Warning Light · false activationRIGHT TAIL PIPE HOT LIGHT ON DURING TAXI. CHECKED CONNECTOR AND CYCLED CIRCUIT BREAKER. PERFORMED RT ENGINE NACELLE FIRE DETECTION TEST PROCEDURE 1 OPS CHECKED GOOD.SDR PNSA2013122607Pitot Tube · failedF/O AIRSPEED INOPERATIVE. F/O ALT 1000 FEET OFF. R & R RT PITOT STATIC TUBE.SDR TSAA20131031004Fitting · chafedMAIN ENTRY DOOR LOCK PIN FITTING CHAFED. NO LIMITS STATED IN SRM. BLENDED CHAFE AND INSPECTED FOR DAMAGE. RESTORED PROECTIVE FINISH IAW SRM 51-20. AFTER BLENDING, DAMAGE ACCEPTED FOR CONTINUDED OPERATION IAW REPAIR STATEMENT 340SDS034517.SDR TSAA20131031001Skin · puncturedCARGO DOOR OUTER SKIN LOWER EDGE PUNCTURED FROM FOREIGN OBJECT CONTACT. DAMAGE INSPECTED FOR CRACKS, FILLED, AND SEALED IAW 340 SRM, CH 51-20-56; ACCEPTED FOR CONTINUED OPERATION IAW REPAIR STATEMENT 340SDS034488.SDR 2013FA0000658Structure · damagedCOMPOSITE DAMAGE NOTED ON FUSELAGE RT VENTRAL FIN OTBD FACE, SEVERAL LOCATIONS BETWEEN FS 756.0 AND 768.5. DAMAGE DETERMINED TO BE BEYOND SRM LIMITS. DAMAGE REPAIRED IAW PRINCIPLES OF SRM, CH 53-90-10 IAW REPAIR STATEMENT 340SDS034517.SDR 2013FA0000657Shroud · crackedRT UPPER EDUCTOR SHROUD CRACKED AT FORWARD CIRCUMFERENTIAL FLANGE; BEYOND LIMITS IAW SRM. REPAIRED IAW REPAIR STATEMENT 340SDS034475.SDR 2013FA0000656Door · crackedRT MLG INBD DOOR INNER SKIN CRACKED ALONG LOWER EDGE OF COMPOSITE. DAMAGE FOUND TO BE BEYOND LIMITS OF SRM; SUBMITTED TO MFG FOR REPAIR APPROVAL. PERFORMED COMPOSITE REPAIR IAW SRM, CHS. 51-70 AND 52-80 IAW REPAIR STATEMENT 340SDS034475.SDR 2013FA0000655Skin · corrodedCORROSION NOTED ON FUSELAGE RT LOWER SKIN, EXTERNAL, AT FS 339.0, BELOW STRINGER SL 1622. DAMAGE DETERMINED TO BE BEYOND SRM LIMITS AFTER BLENDING TO REMOVE CORROSION. REMAINING MATERIAL THICKNESS SENT TO MFG FOR EVALUATION. REPLACED DAMAGED FASTENERS AND ISDR 2013FA0000654Fitting · chafedMAIN ENTRY DOOR LOCK PIN FITTING CHAFED; NO LIMITS STATED IN SRM. BLENDED CHAFE AND INSPECTED FOR FURTHER DAMAGE; SUBMITTED DAMAGE TO MFG FOR EVALUATION. RESTORED PROTECTIVE FINISH IAW 340SRM, CH 51-20. AFTER BLENDING, DAMAGE ACCEPTED FOR CONTINUED OPERATIOSDR 2013FA0000653Skin · damagedFUSELAGE LT SKIN EDGE, EXTERNAL, GOUGED AT FS 258.0, WL 80, FWD EDGE OF MAIN DOOR OPENING. DAMAGE DETERMINED TO BE BEYOND SRM LIMITS. DAMAGE REPAIRED BY TRIMMING, INSPECTING AND RESTORING PROTECTIVE FINISH IAW SRM, CH 51-20 IAW REPAIR STATEMENT 340SDS034517.SDR 2013FA0000652Skin · dentedFUSELAGE LT AFT SKIN, EXTERNAL, DENTED BETWEEN FS 739 AND 749, ABOVE LT VENTRAL FIN; ALSO, 4 RIVETS INSTALLED IN CHEM-MILLED POCKET. DAMAGE DETERMINED TO BE BEYOND 340 SRM LIMITS. DAMAGE INSPECTED AND SUBMITTED TO MFG FOR EVALUATION. DENTS AND RIVET LOCATIOSDR 2013FA0000651Skin · puncturedCARGO DOOR OUTER SKIN LOWER EDGE PUNCTURED FROM FOREIGN OBJECT CONTACT. DAMAGE INSPECTED FOR CRACKS, FILLED AND SEALED IAW 340 SRM, CH 51-20-56; ACCEPTED FOR CONTINUED OPERATION IAW REPAIR STATEMENT 340SDS034488.SDR TSAA20131031007Structure · crackedRT UPPER SHROUD CRACKED AT FWD CIRCUMFERENTIAL FLANGE BEYOND LIMITS. REPAIRED IAW REPAIR STATEMENT 340SDS034475.SDR TSAA20131031006Skin · dentedFUSELAGE LT AFT SKIN DENTED BETWEEN FS 739 AND 749, ABOVE LT VENTRAL FIN. DAMAGE DETERMINED TO BE BEYOND LIMITS. DAMAGE INSPECTED, FOUND TO BE ACCEPTABLE FOR CONINTUED SERVICE IAW REPAIR STATEMENT 340SDS034517.SDR TSAA20131031005Skin · gougedFUSELAGE SKIN GOUGED AT FS 258, WL 80. DAMAGE DETERMINED TO BE BEYOND LIMITS. DAMAGE REPAIRED BY TRIMMING, INSPECTING AND RESTORING PROTECTIVE FINISH IAW SRM 51-20.SDR TSAA20131031003Structure · delaminatedCOMPOSITE DAMAGE NOTED ON FUESLAGE RT VENTRAL FIN OTBD FACE, SEVERAL LOCATIONS BETWEEN FS 756 AND 768.5. DAMAGE DETERMINED TO BE BEYOND LIMITS. DAMAGE REPAIRED IAW SRM CH 53-90-10 IAW REPAIR STATEMENT 340SDS034517.SDR TSAA20131031002Skin · corrodedCORROSION NOTED ON FUSELAGE RT LOWER SKIN AT FS 339 DAMAGE DETERMINED TO BE BEYOND MFG LIMITS AFTER BLENDING TO REMOVE CORROSION. REPLACED DAMAGED FASTENERS AND INSPECTED TO ENSURE ALL DAMAGE WAS REMOVED. RESTORED PROTECTION FINISH IAW SRM 51-20.SDR PNSA2013092604Generator · failedRT AC GENERATOR FAILED, R & R GENERATOR.SDR TSAA20130923008Skin · corrodedDURING CHECK, CORROSION FOUND ON FUSELAGE SKIN, FORWARD AND BELOW RT SIDE WINDOW.SDR OZCA20130905001Smoke Detector · defectiveDURING A TURNBACK FOR AN OIL TEMP PROBLEM ON THE LT ENGINE, THE CARGO SMOKE LIGHT ILLUMINATED INTERMITTENTLY. NO SMOKE WAS DETECTED OR NOTICED. AN EMERGENCY WAS DECLARED. MX REPLACED CARGO ZONE B1 AND C2 SMOKE DETECTORS AND RELEASED. AFCF PERFORMED AND SESDR CA130816007Cable · failed(CAN) CREW WENT TO PULL THE HANDLE TO SET THE PARKING BRAKE AND THE HANDLE SHEARED OFF THE CABLE.SDR CA130627009O-Ring · deteriorated(CAN) WE HAD A IN-FLIGHT SHUTDOWN DUE TO HIGH OIL CONSUMPTION ON THE RT ENGINE ON ACFT. IT WAS CAUSE BY A LOW OIL PRESSURE LIGHT ILLUMINATING SHORTLY AFTER TAKEOFF AND A DROP IN OIL PRESSURE TO THE RED LINE. THE ACFT RETURNED TO BASE SAFELY. IT WAS FOUND THASDR TSAA20130528006Skin · corrodedDURING ROUTINE VISUAL INSPECTION, CORROSION DAMAGE FOUND ON FUSELAGE SKIN LOCATED AT BS 435, SL1504. DAMAGE LENGTH IS 1.375", WIDTH IS .5", AND DEPTH IS .02".SDR PNSA2013051805Panel · faultyON TAKEOFF ROLL ENGAGED CTOT, LEFT ENGINE SET POWER AS NORMAL, RIGHT ENGINE DID NOT SET POWER RIGHT ENGINE STAYED AT 80% TORQUE PUSHED RIGHT PL UP A LITTLE TO ENSURE 64 SWITCH ENGAGED, TORQUE WENT FROM 80% TO 120% FOR APPROX 1 SECOND NO OVER TEMP OIL PRESSURE SDR CA130409014Tube · leaking(CAN) DURING CRUISE FLIGHT THE FLIGHT CREW NOTICED A LOW OIL PRESSURE INDICATION ON THE NR 2 ENGINE. THE CHECKLIST WAS FOLLOWED AND THE NR 2 ENGINE WAS SHUTDOWN. THE FLIGHT CREW ADVISED MAINTENANCE AND FLIGHT OPERATIONS AND RETURNED. AN INSPECTION WAS COMPLSDR CA130222008Terminal Block · overheated(CAN) UPON SWITCHING ON THE AVIONICS MASTER PRIOR TO TAXIING OUT FOR TAKEOFF, A BURNING ODOR WAS NOTICED IN THE COCKPIT. THE AVIONICS SWITCH WAS TURNED OFF AND THE PASSENGER DISSEMBARKED. MAINTENANCE INSPECTED THE ACFT AND FOUND THE ODOR TO BE COMING FROM TSDR CA130114004Sensor · malfunctioned(CAN) DURING THE CLIMBOUT, THE CREW NOTED THAT THE NR 2 ENGINE OIL TEMPERATURE BEGAN TO INCREASE AND WAS READING HIGHER THAN NORMAL. IT CONTINUED TO INCREASE INTO THE YELLOW ARC AND SHORTLY THEREAFTER TO THE REDLINE. ALL OTHER ENGINE PARAMETERS INCLUDING THESDR CA121130011Recorder · failed(CAN) THE FDR WAS SENT OUT TO OBTAIN THE RECORDING FOR AN UNRELATED SYS FAILURE. WHEN THE AVIONICS SHOP ATTEMPTED TO READ THE FDR THEY FOUND THE FDR WAS NOT WORKING FOR ABOUT THE LAST 10HRS OF FLIGHT. THE LAST SCHEDULED MAINTENANCE THERE WAS A CORRELATION CHESDR TSAA20121003006Engine · surgesACFT HAD A LOW SPEED TAKEOFF ABORT (LESS THAN 80 KNOTS) DUE TO ENGINE SURGE.SDR TSAA20120507002Generator · failedLT AC GENERATOR LIGHT ILLUMINATED AT TAKEOFF. ACFT ABORTED AND RETURNED TO GATE.SDR CA120419001Bearing · failed(CAN) DURING HEAVY INSPECTION, WITH THE AILERON CABLE TENSION SLACKED OFF, IT WAS NOTICED THAT THE RT AILERON BELLCRANK, IN THE WING, MOVEMENT WAS ROUGH AND NOISY. UPON REMOVAL FOR FURTHER INSPECTION, IT WAS DISCOVERED THAT THE 2 BEARINGS, PN MS27641-5 THAT SUSDR 2012F00061Line · crackedON APPROACH THE NR 2 ENGINE EXPERIENCED AN AUTOCOARSON PROBLEM AND A PERCAUTIONARY SHUTDOWN WAS PERFORMED.
SDR TSAA201201001Accumulator · leakingAFTER COMPLETION OF ENGINE TREND MONITORING, HYD CAUTION LIGHT ILLUMINATED ON CENTRAL WARNING PANEL. BOTH MAIN AND EMERGENCY ACCUMULATOR PRESSURE LOW. AUTO FUNCTION DID NOT WORK. EMERGENCY DECLARED. ACFT RETURNED TO AIRPORT WITH NO FURTHER INCIDENT. R & RSDR TSAA1132014Lock Ring · brokenLANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION AFTER TAKEOFF. FLIGHT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. REPLACED BROKEN ROLLER GUIDE LOCK RING ON LT MLG INBD AND OTBD ROLLER GUIDE SWITCH. ADJUSTED/TESTED LANDING GEARS (EXTENSSDR TSAA2011112372013Oil System · lowON TAKEOFF ROLL, THE RT ENGINE OIL WARNING LIGHT ILLUMINATED AT APPROX 90 KTS. ABORTED TAKEOFF ROLL AND RETURNED TO GATE WITHOUT FURTHER INCIDENT. SERVICED NR2 ENGINE OIL QUANTITY. ACFT RETURNED TO SERVICE.SDR TSAA2011112372012Oil System · lowON TAKEOFF ROLL, THE LT ENGINE OIL WARNING LIGHT ILLUMINATED AT APPROX 90 KTS, ABORTED TAKEOFF ROLL AND RETURNED TO GATE WITHOUT FURTHER INCIDENCE. SERVICED NR1 ENGINE OIL QUANTITY. ACFT RETURNED TO SERVICE.SDR CA111116004Acm · seized(CAN) APPROXIMATELY 10 MINUTES AFTER DEPARTURE THE CREW NOTED AN ABNORMAL SMELL IN THE COCKPIT. THE RECIRC FANS WERE SUSPECT & WERE SELECTED TO OFF IAW THE CHECKLIST. THE SMELL DISSIPATED & THE FLIGHT CONTINUED. WITHIN 10 TO 15 MINUTES THE SMELL RETURNED INSDR CA111116005Pump · intermittent(CAN) ON APPROACH THE CREW RECEIVED A HYD PRESS INDICATION ADVISORY WHEN THE LG WAS SELECTED. IAW CHECKLIST, THE LG WAS EXTENDED USING THE ALTERNATE SYS & ALL 3 GEAR INDICATED DOWN & LOCKED. THE ACFT HYD PRESS & QTY WAS VERIFIED & THE ACFT LANDED WITHOUT INCSDR CA111116007Ice Shield · loose(CAN) ON APPROACH THE FLIGHT CREW COULD HEAR AN ABNORMAL NOISE FROM THE EXTERIOR OF THE ACFT. ALL PARAMETERS & OPERATION OF THE ACFT WAS NORMAL & THE ACFT COMPLETED A NORMAL LANDING. A VISUAL INSPECTION BY THE CREW AFTER LANDING REVEALED A LIFTED SECTION OF SDR TSAA2011101132011Control Valve · misrepairedLANDING GEAR CONTROL VALVE, WAS OPS CHECKED AFTER INSTALLATION. DURING OPS CHECK, LANDING GEAR DID OPPOSITE OF WHAT IT WAS ASKED. WHEN THE GEAR HANDLE WENT UP, THE GEAR WENT DOWN. WHEN THE GEAR HANDLE WENT DOWN, THE GEAR WENT UP. UPON FURTHER INVESTIGATIONSDR OWFR20110921001Rib · crackedDURING A ROUTINE INSPECTION IAW JOB CARD 0600-541-01I, A CRACK HAS BEEN FOUND IN THE LOWER BEND RADIUS OF THE RT FLAP RIB NR5 LOCATED APPROX AT STA WS202.
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