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 = 'A310' 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 = 'A310' 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 07FDEA01454Fairing · crackedCRACK FOUND AT INNER SKIN OF NR 4 LT FLAP MOVABLE FAIRING. REPAIR PERFORMED BY BONDING IAW SRM 57-20-35 AND EA 6-5720-99236 AND RAS/FOK/126/2006 ISSUE (A).SDR 07FDEA01441Skin · corrodedCORROSION FOUND IN CWB UPPER SURFACE BETWEEN FR46/47 AND FR48 BETWEEN Y1555 AND Y1850. PERFORM NDT INSPECTION NTM 51-10-08, 51-10-01 AND 51-10-04. REPAIRED PER SRM 57-10-12 PG. 201. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.SDR 07FDEA01440Skin · corrodedLT WING OUTER SKIN SURFACE WITH CORROSION ON T/E AREA 591 RIB 27 REPAIRED PER FEDEX EA 6-5710-106708. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS " MAJOR.SDR 07FDEA01439Door Frame · wornFWD CARGO COMPARTMENT DOOR AFT FRAME FOUND WORN AT FRAME 25 REPAIRED PER FEDEX EA 6-5330-106703. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS " MAJOR.SDR 07FDEA01438Door Frame · wornFWD CARGO COMPARTMENT DOOR FWD FRAME WORN ON FRAME 20 STR 42 REPAIRED PER FEDEX EA 6-5330-106703. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS " MAJOR "SDR 07FDEA01445Skin · damagedFUSELAGE LOWER FWD LOBE, REPAIR AT LT SIDE OF FUSELAGE BETWEEN FRAME 25 & 26/32 BETWEEN STR. 42 & 43 REPAIRED PER SRM 53-10-12 FIG. 229 (SHEET 1) PG. 406 TO 410 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS " MAJOR "SDR 07FDEA01443Panel · cracked(N0535) CRACK FOUND ON NR 1 PYLON AFT FAIRING. REPAIR ON GOING AS SRM. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. FAIRING TO PYLON COWL OF RT CORE W/ TWO CRACKS REPAIRED IAW SRM 54-56-10 CONFIG 2 FIG 201.SDR 07FDEA01442Fairing · crackedCRACK FOUND ON NR 1 PYLON LOWER FAIRING. REPAIR ON GOING AS SRM REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.SDR 07FDEA01433Fairing · crackedFAIRING PANEL TO PYLON COWL OF RT CORE WITH 2 CRACKS REPAIRED THE CRACKS IAW SRM 54-56-10 CONFIG. 2 FIG 201. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED MINOR.SDR 07FDEA00604Lock · unknownDURING LANDING AT KBUR, THRUST REVERSER LEVERS EXTREMELY STIFF, F/O LOWERED REVERSER OR ATTEMPTED TO STOW AND LEVERS WERE SO STIFF COULD NOT STOW REVERSERS. ALL BETWEEN 80-60 KTS, AT ABOUT 65 KTS CAPT COMMANDED F/O TO MOVE HAND FROM THROTTLE AND POUNDED ANDSDR 07FDEA00070Transmitter · leakingAT TOGA FOR TAKEOFF, LOST BLUE HYD SYSTEM. QTY WENT TO ZERO. REJECTED TAKEOFF,CLEARED RWY WORKED QRH. FOUND LEAK COMMING FROM BLUE SYSTEM PRESSURE TRANSMITTER AREA ON BLUE SYSTEM MODULE. LEAK IS OBVIOUS. R & R BLUE SYSTEM PRIORITY VALVE REF. A310-200SDR 06FDEA04357Frame · crackedDURING ACCESS OPENING ON MAIN CARGO DECK SOME CROSS TRACKS OF FRAME 43 P/N R538D1048-200-00 WAS FOUND CRACK AND NEED TO BE REPLACED. TRACKS REPLACED PER SRM 51-40-00 ON FR43 Y1456/Y1956. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".SDR 06FDEA04352Crossbeam · misrepairedPREVIOUS REPAIR FOUND LOCATED ON LT CROSSBEAM FS 3249, FR 60 AND Y120- Y197. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAISDR 06FDEA04351Crossbeam · misrepairedPREVIOUS REPAIR FOUND LOCATED ON LT CROSSBEAM FS 3143, FR 55/58 AND Y120- Y197. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM RESDR 06FDEA04322Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON AFT CARGO DOOR SKIN FWD LWR SIDE, FS 3249, AND FR 60. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT CONFORM TO AN SDR 06FDEA04321Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON LOWER SECTION OF FWD CARGO DOOR SKIN, FS 1605, AND FR 23-23A. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT TO SDR 06FDEA04040Spar · corroded33 AREAS OF CORROSION AROUND FASTENERS ALONG FS 40 AT CTR WING TANK LOWER SPAR CHORD BETWEEN STRINGER 1 AND 5R (EXTERNAL OF TANK) C/W FEDEX EA6-5730-105024.SDR 06FDEA03882Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON R1 DOOR LOWER AFT END FS 1260 AND FR 16 EXTERNAL DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORMSDR 06FDEA03881Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON R1 DOOR LOWER FWD END FS 1187 AND FR 14A EXTERNAL DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFOSDR CA061101001Valve · broken(CAN) WHILE PERFORMING A GENERAL VISUAL INSPECTION INSIDE THE RIGHT HAND/OUTER FUEL TANK, THE OUTBOARD FUEL PUMP SEQUENCE VALVE WAS FOUND BROKEN. DEBRIS OF THE SEQUENCE VALVE WHERE FOUND NEARS THE RESPECTIVE FUEL PUMP CANISTER. AREA WAS CLEAN OUT. SEQUENCE VALSDR 06FDEA3045None · noneFOUND REPAIR LOCATED ON RT WING T/E WS 1625, RIB 26-27 BETWEEN OB FLAP AND WING TIP. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR CA060822002Wheel · cracked(CAN) DURING THE AIRCRAFT PUSHBACK, IT WAS NOTED ON THE ECAM THAT NR 8 MAIN WHEEL WAS LOOSING PRESSURE. AFTER RETURNING TO THE GATE, IT WAS CONFIRMED USING A REGULAR TIRE PRESSURE GAUGE THAT THE PRESSURE WAS DROPPING. USING LEAK DETECTOR FLUID, IT WAS DETERMINSDR CA060822003Line · chafed(CAN) DURING ROUTINE MAINTENANCE INSPECTION, FOUND NR 1 ENGINE DRIVEN PUMP OUTLET PRESSURE TUBE OF GREEN HYDRAULIC SYSTEM CHAFED BY THE AILERON TRIM INPUT CABLE AT REAR SPAR OB OF RIB 5A. HYDRAULIC TUBE REPLACED. CAMPAIGN INITIALIZED TO VERIFY THE REST OF THE SDR 06FDEA2991Landing Gear · malfunctionedLOUD BANG AND PRONOUNCED VIBRATION WAS FELT FROM THE NOSE WHEEL WELL AREA. UPON GEAR RETRACTION, UNSAFE GEAR DOOR ( NOSE WHEEL ) AMBER LIGHT REMAINED ON BOTH PANELS, QRH WAS FOLLOWED. GEAR HANDLE WAS NOT SELECT ED TO NEUTRAL. ONCE DECIDED TO EXTEND GEAR FOR SDR 06FDEA2725Floor Support · corrodedMDCC AT FR 12 TO 14 HAS CORROSION AROUND SCREW HOLES TOP AND BOTTOM REF N00373. REPLACED FLOOR SUPPORT IAW A310-200 SRM 51-40-21.SDR 06FDEA2724Seat Track · corrodedFOUND FRAME 19 TRACK 4 RT HAS CORROSION IN TRACK. REMOVED AND REPLACED SEAT TRACK A310-200 SRM 51-40-21 AND 51-72-10.SDR 06FDEA2723Structure · corrodedMDCC AT FR 13 TO 14 LT YB HAS CORROSION AROUND FASTENER HOLES TOP AND BOTTOM, SURFACE REF N00390. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW A310-200 SRM 53-10-00.SDR 06FDEA2720Power Cable · faultyPDIS 426 30-40 0008213 28JUL06 MEM, SMOKE IN COCKPIT DUE TO OVERHEAT OF RT WINDOW HEAT COILED POWER CORD. RAM AIR VALVE OPENED AND COURIER 02 MAN OVERRIDE SELECTED ON. COURIER 02 SYSTEM RESET AND RAM AIR DOOR CLOSED. ACN RELEASED FOR SERVICE IAW MEL/CDSDR 06FDEA2718Controller · malfunctionedPDIS 417, 21-30, 0009646, 28JUL06 SIN, AFTER TAKEOFF RECEIVED ECAM ALERT (EXCESS CAB ALT) WENT TO RED TABS AND COULD NOT CONTROL CABIN PRESSURE. ON ECAM NR1 OUTFLOW VALUE OPEN , NR2 OUTFLOW CLOSED FACT, 28JUL06 09:49 SIN R R/I NR1 CABIN PRESSURE CONTROLSDR 06FDEA2663Pitot Tube · dirtyRIGHT AFTER ROTATION BOTH ATS LEVERS DROPPED OFF. ADC FAILED ON CAPT SIDE SWITCHED OVER TO OTHER SYSTEM REENGAGED ATS LEVERS AS PER ECAM THROTTLE RETARDED TO IDLE AS SOON AS ATHR BUTTON PUSHED. NO ECAM FOR ADC. ALSO NR 1 FLT DIRECTOR FAILED. CAPTS ALTIMETESDR 06FDEA2659Adc · failedJUST AFTER ROTATION BOTH ATS LEVERS DROPPED OFFLINE AND WOULD NOT RESET. YAW DAMP DROPPED OFF, WOULD NOT RESET. CAPTS PFD, ADC FAILED. SWITCHED OVER TO F/O SYSTEM. HAD NUMEROUS AIRSPEED WINDSHEAR VMO MMO WARNINGS EVEN THOUGH USING STBY SYSTEMS. AT THAT POSDR 06FDEA2656Seat Track · corrodedMDCC FS 19 LT TRACK NR 4 HAS CORROSION INSIDE AND OUTSIDE OF TRACK REF N00201. REMOVED AND REPLACED SEAT TRACK AT FS 19 IAW A310 SRM 51-72-10.SDR 06FDEA2655Floor Support · corrodedMDCC FS 14 TO 14B AT YD FLOOR SUPPORT HAS CORROSION TOP AND BOTTOM SURFACE REF N00385. REMOVED AND REPLACED FLOOR SUPPORT IAW A310 SRM 51-40-00.SDR 06FDEA2654Floor Support · corrodedMDCC AT FS 13B LT YA FLOOR BOARD SUPPORT HAS CORR AROUND FAST HOLE TOP AND BOTTOM SURFACE REF N00389. REMOVED CORROSION IAW A310 SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW A310 SRM 53-10-00, FIG 102 TABLE 102.SDR 06FDEA2653Rib · corrodedLT HORIZ STAB TE RIB AND WEBS IB OF SERVO ACTUATORS, UPPER SURFACE HAVE CORROSION AROUND FASTENER HOLES REF N00292. REMOVED CORROSION IAW A310 SRM 51-74-10, FOUND TO BE WITHIN LIMITS IAW A310 SRM 55-10-00.SDR 06FDEA2652Rib · corrodedLT PYLON IB SIDE RIB 16A HAS CORROSION AROUND FAST HOLES REF N00174. REMOVED CORROSION ON RIB 16A GUSSET IAW A310 SRM 51-72-10 FOUND TO BE OUT OF LIMITS. REPLACED RIB 16A GUSSET IAW A310 SRM 51-40-21.SDR 06FDEA2651Cargo Track · corrodedMDCC AT FS 11A TO 14 LT YD HAS CORROSION ON TOP AND BOTTOM SURFACE AROUND FAST HOLES REF N00397. REMOVED CORROSION IAW A310 SRM 51-74-10 FOUND TO BE WITHIN LIMITS IAW A310 SRM 53-10-00 FIG 102 TABLE 102.SDR 06FDEA1888Spar Cap · corrodedPREVIOUS REPAIR FOUND LOCATED ON THE LT HORIZONTAL STABILIZER FRONT SPAR CAP HS 225-267, RIB 8-9. EXISTING REPAIR EVALUATED FOUND PER SRM ,BUT CORROSION WAS FOUND ON THE SURROUNDING AREA OF REPAIR AND NEW REPAIR ACCOMPLISHED PER E.A. 6-5510-97877 REPAIR ESDR 06FDEA1085Repair · unknownPREVIOUS REPAIR INSTALLED ON RIGHT HAND NUMBER TWO SPOILER UPPER OUTBOARD END AT WS 339 TO WS 359. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED ASDR 06FDEA1083Repair · unknownPREVIOUS REPAIR INSTALLED ON LT OUTBOARD FLAP LOWER SURFACE BETWEEN FLAP RIB 4 AND 5 AT WS 1010 TO WS 1030. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. SDR 06FDEA1081Repair · nonePREVIOUS REPAIR INSTALLED ON LEFT HAND INBOARD FLAP UPPER TRAILING EDGE WEDGE, WS 145 TO WS 177. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. TRAILING EDGSDR 06FDEA1080Repair · unknownPREVIOUS REPAIR INSTALLED ON LEFT HAND INBOARD FLAP UPPER TRAILING EDGE WEDGE, WS 40 TO WS 86. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. TRAILING EDGE SDR 06FDEA1079Repair · unknownPREVIOUS REPAIR INSTALLED ON LEFT HAND INBOARD FLAP LOWER TRAILING EDGE WEDGE, WS 140 TO WS 185. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. TRAILING EDGSDR 06FDEA1074Repair · unknownPREVIOUS REPAIR INSTALLED AT FUSELAGE CROWN LEFT HAND SIDE AT FR 40/41 TO FR 40/41, FS 2294 TO FS 2294, STR 2 TO STR 3. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPSDR CA060220001Wire Harness · burnedAIRCRAFT ARRIVED AT STATION WITH A DEFECT LOG REPORT OF THE FORWARD LAVATORY NOT FLUSHING. TROUBLESHOOTING FOUND THAT 4 WIRES BETWEEN THE FLUSH MOTOR AND THE TIMER UNIT WERE BROKEN. IT WAS NOTED THAT MINOR ARCH/BURNING OF THE WIRES HAD OCCURRED. ALL 4 WIRESSDR 06FDEA0649Failsafe · corrodedFWD PASS CREW DOOR RING RT FAILSAFE RING CORRODED AT UPPER FWD CORNER AT CENTRAL UPPER AREA AND AT AFT LOWER CORNER. REPLACED FAILSAFE RING PER DWG. R53610899 AND FEDEX EA 6-5340-95697 AND AIRBUS T.D. REF. 942-042678/03/2006 AND SRM 51-72-10 AND SRM 51-40-21 SDR 06FDEA0647Fitting · crackedFWD MDCC UTILITY AREA SUSPECT A CRACK AT FLOORBEAM CONNECTION FITTING AT FRAME 12A LT.SDR 06FDEA0642Repair · noneFOUND REPAIR LOCATED LT PAX DOOR L1. EXTERNAL DOUBLER LWR AFT CORNER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF REPAIR ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR WAS PREVIOUSLY ACCOMPLISHED RAS/AS/027/2006 REPAIR EVALUATED SDR 06FDEA0641Skin Panel · unknownFOUND REPAIR LOCATED LT AILERON WS 513-538. LOWER SURFACE. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA0534Repair · misinstalledFOUND REPAIR LOCATED ON RT OUTBD FLAP, RT WS 935-950. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR ACCOMP
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