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 = '7377' 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 = '7377' 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 SWAA2016071153678Attach Angle · corrodedFORWARD GALLEY DOOR THRESHOLD INBOARD ATTACH ANGLE CORRODED BETWEEN BS 298 TO 330, RBL 57. R & R THE ATTACH ANGLE IAW SRM.SDR SWAA2016071153677Angle · corrodedAFT GALLEY DOOR CUTOUT CREASE BEAM INBOARD ANGLE CORRODED BETWEEN BS 880 TO 1016, RBL 56. R & R THE ANGLE IAW SRM.SDR SWAA2016070753580Support · corrodedFORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 420 - 440, RBL 24. R & R THE SUPPORT IAW SRM.SDR SWAA2016070753579Support · corrodedFORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 396 - 420, RBL 23. R & R THE SUPPORT IAW SRM.SDR SWAA2016070553464Strap · corrodedFORWARD CARGO BAY ON CARGO DOOR SILL INNER STRAP CORRODED BETWEEN BS 480 TO 500, RBL 22. R & R THE STRAP IAW SRM.SDR SWAA2016062353177Intercostal · crackedFLOOR SUPPORT INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 12. R & R INTERCOSTAL IAW SRM.SDR CALA2016020400085Structure · wornSTRIKE PLATE WORN THROUGH STRUCTURE ON HP PNEU DOOR 192DR, OTBD FWD LATCH. FABRICATED & INSTALLED REPAIR IAW ECRA 5710-02515.SDR ASCB20160225001Frame · corrodedEXFOLIATION CORROSION FOUND ON THE AFT FACE OF THE FUSELAGE FRAME AT BS 303.9, IN THE AREA OF THE FORWARD LT PASSENGER DOOR LOWER HINGE FITTING.SDR CALA2016010800038Seat Track · crackedIAW AD 2013-23-04 AT STATION 727B, LBL 45.5. FOUR EACH CRACKS NOTED, TWO EACH OTBD FLANGE, TWO EACH INBD FLANGE. INSTALLED FLANGE REPAIRS IAW RES 2009911-11 REV 1R & ECRA 5320-02663. COPY ATTACHED.SDR CALA2016010800037Seat Track · crackedIAW AD 2013-23-04 AT STATION 727B, RBL 45.5, TWO EACH CRACKS NOTED, ONE EACH INBD FLANGE, ONE EACH OTBD. INSTALLED FLANGE REPAIRS IAW RES 2009911-14 REV 1R & ECRA5320-02663. SEE ATTACHED COPY.SDR CALA2016010800036Seat Track · crackedIAW AD 2013-23-04 STATION 727B AT RBL 24.75, ONE EACH CRACK NOTED ON INBD SIDE OF FLANGE. INSTALLED FLANGE REPAIRS IAW RES 2009911-13 IR & ECRA 5320-02663. SEE ATTACHED COPY.SDR CALA2016010800035Seat Track · crackedIAW AD 2013-23-04 AT STATION 727B ON LBL 24.75, FOUR EACH CRACKS NOTED, TWO EACH INBD FLANGE, TWO EACH OTBD FLANGE. INSTALLED FLANGE REPAIRS AT RBL 24.75, FOUR EACH SEAT TRACK STATION 727B IAW RES 2009911-12 REV 1R & ECRA 5320 - 02663, SEE ATTACHED COPY.SDR CALA2015122801034Seat Track · crackedCRACKS FOUND AT SEAT TRACK FASTENER HOLES, 4 EACH AT STATION 727B, LBL 45.5. COMPLIED WITH REPAIR AT SEAT TRACK STATION 727B, LBL 45.5 IAW RES WI 2009650-2 REV IR & ECRA 5320-02660.SDR CALA2015122801033Seat Track · crackedCRACKS FOUND AT SEAT TRACK FASTENER HOLES, 2 EACH AT STATION 727B, LBL 24.75. COMPLIED WITH REPAIR AT SEAT TRACK STATION 727B, LBL 24.75 IAW RES WI 2009650-3 REV IR & ECRA 5320-02660.SDR CALA2015122401029Seat Track · crackedCRACKS FOUND AT SEAT TRACK FASTENER HOLES, 3 EACH AT STATION 727B, RBL 45.5. COMPLIED WITH REPAIR AT SEAT TRACK STATION 727, RBL 45.5 IAW RES WI 2009650-5 REV IR & ECRA 5320-02660.SDR CALA2015122401028Seat Track · crackedCRACKS FOUND AT SEAT TRACK FASTENER HOLES, 3 EACH AT STATION 727B, RBL 24.75. COMPLIED WITH REPAIR AT SEAT TRACK STATION 727B, RBL 24.75 IAW RES WI 2009650 4 REV IR & ECRA 5320-02660.SDR Z6WR20151222013Panel · burnedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2101-177 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 45B, REVEALS 7 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION CT -177 BONDED PANEL ASSEMBLSDR Z6WR20151222012Panel · burnedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2101-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 40B, REVEALS 9 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION CT -174 BONDED PANEL ASSEMBLSDR Z6WR20151222011Panel · burnedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2102-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 45B, REVEALS 8 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION CT-174 BONDED PANEL ASSEMBLYSDR Z6WR20151222010Panel · burnedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2101-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 40B, REVEALS 13 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION CT -174 BONDED PANEL ASSEMBSDR CALA2015111300922Structure · crackedHFEC INSPECTION DETECTED A CRACK INDICATION AT STATION 727B, RBL45.50, TWO HOLES EACH, AFT INBD & AFT OTBD. ACCOMPLISHED STRAP REPAIRS IAW RES-WI 2009633-4 & ECRA 5320-02627.SDR CALA2015111300921Strap · crackedHFEC DETECTED CRACK INDICATIONS AT STATION 727B AT LBL 45.50, SPLICE STRAP, THREE HOLES EACH, FWD INBD, AFT INBD & AFT OTBD. ACCOMPLISHED STRAP REPAIRS IAW RES-WI 2009633-2 & ECRA 5320-02627, IND & OTBD.SDR CALA2015111300920Strap · crackedHFEC DETECTED CRACK INDICATIONS AT STATION 727B AT LBL 45.50, SPLICE STRAP, THREE HOLES EACH, FWD INBD, AFT INBD, AFT OTBD. ACCOMPLISHED STRAP REPAIRS IAW RES-WI 2009633-2 & ECRA 5320-02627 INBD & OTBD.SDR CALA2015111300919Structure · crackedHFEC DETECTED A CRACK INDICATION AT STATION 727B, LBL 24.75, INBD AFT HOLE, ONE EACH. ACCOMPLISHED STRAP REPAIRS IAW RES-WI 2009633-1 & ECRA 5320-02627.SDR SWAA2015062641185Stringer Clip · corrodedSTRINGER CLIP CORRODED AT STATION 787, STRINGER 26L. R & R CLIP IAW SM.SDR SWAA2015062641184Stringer Clip · corrodedSTRINGER CLIP CORRODED AT STATION 787, STRINGER 26R. R & R CLIP IAW SRM.SDR SWAA2015062641183Stringer Clip · corrodedSTRINGER CLIP CORRODED AT STATION 747, STRINGER 26L. R & R CLIP IAW SRM.SDR SWAA2015061140599Frame · crackedFOUND A FUSELAGE FRAME CRACKED AT BS 400, STRINGER 8R. REPAIRED THE FRAME IAW EA.SDR CA141023010Brake Assy · failed(CAN) DURING PUSHBACK, NOTICED A VIBRATION COMING FROM THE LANDING GEAR. GND CREW THEN NOTICED SEVERAL PIECES OF METAL ON THE RAMP, NEAR THE LEFT INBOARD MAIN WHEEL. PIECES SEEM TO COME FROM LEFT INBOARD SIDE. BOTH THE NR 2 BRAKE ASSEMBLY WAS REPLACED DUE TSDR COZA20140724044Adc · failedON APPROACH, THE FIRST OFFICERS AIRSPEED INDICATOR & ALTIMETER FAILED WITH ALL FLAGS SHOWN. DURING TROUBLESHOOTING THE AIR DATA COMPUTER WOULD NOT TEST. THE AIR DATA COMPUTER WAS REPLACED. LEAK & OPERATIONAL CHECKS WERE ACCOMPLISHED WITH NO WARNING INDICATISDR EE4Y2011041900105Pan · crackedDURING INSPECTION PROCESS WE FOUND IN THE PAX CABIN TOURIST CLASS, POSITION 14A-C SEATS WITH BACK PAN CRACKED.SDR CA140123009Line · leaking(CAN) DURING TAKEOFF AFTER ROTATION THE FLIGHT CREW REPORTED AN AUTO FAIL LIGHT ILLUMINATE ON THE PRESSURIZATION PANEL. FOLLOWING PROCEDURES, THE FLIGHT CREW SWITCHED TO ALTERNATE MODE WHICH ALSO FAILED. THE FLIGHT CREW THEN SWITCHED TO MM & WERE SUCCESSFUL SDR COZA20130124023Actuator · leakingRIGHT INBOARD GROUND SPOILER, OUTBOARD ACTUATOR FOUND WEEPING FLUID. REPLACED ACTUATOR. OPS AND LEAK CHECKED NORMAL.SDR COZA20120703010Actuator · slowDURING OPS CHECKS, RAM AIR INLET DOOR ACTUATOR WAS SLOW WHEN MOVING DOOR. REPLACED ACTUATOR AND OPS CHECKED NORMAL.SDR DALA1214863603Mechanism · out of limits08MAR12; WHILE WORKING PSV4, OPN 59086 FOUND THE RT ELEV CONTROL TAB MECHANISM, "GAP CHECK BETWEEN OUTER FACE OF THE AFT LUG AND THE SWAGE RING" BEYOND LIMITS. NR 58 WAS WRITTEN FOR MECHANISM REPLACEMENT, PART NBR 251A2430-18. FCF TO BE COMPLIED WITH DUE TO SDR DALA1212063602Frame · damagedWORKING ERA 484067-14 REV B HAD TO REMOVE DOUBLERS FROM PREVIOUS REPAIR INSTALLED ON SAME ERA WHICH FAILED DTA. REMOVED DOUBLES AND FOLLOWED INSTRUCTION REF AS PRI 484067-14 REV C. INSTALL AND SIGNED OFF A FOLLOWED INSTRUCTIONS AS OUTLINED IN ERA 484067-14 RSDR ASMF201111121001Switch · damagedDURING CLIMB, MAIN LANDING GEAR DID NOT RETRACT. AIR RETURN. CREW ACCOMPLISHED QRH 14.16 PROCEDURE, CONFIRMING FAILURE. DURING MX REVISION, MANUAL EXTENSION ACCESS DOOR SWITCH AND ACTUATOR DETECTED DAMAGED. MANUAL EXTENSION ACCESS DOOR SWITCH AND ACTUATOR SDR CA111004005Starter · damaged(CAN) ENROUTE, THE CREW NOTICED A LOW OIL QTY INDICATION OF 2 QT FOR THE NR 1 ENGINE. OIL PRESSURE AND TEMP WERE REPORTED TO BE NORMAL FOR THE NEXT 40 MINUTES WHEN THE QTY DROPPED TO ZERO AND PRESSURE DROPPED AS WELL TO MINIMUM VALUES. SUBSEQUENTLY, THE LOW SDR CA110727007Motor · unserviceableDURING CLIMB OUT THE FLIGHT CREW HAD A STAB OUT OF TRIM LIGHT ILLUMINATE. THE FLIGHT CREW EXECUTED THE APPROPRIATE CHECKLIST AND FOUND THE STABILIZER ELECTRIC TRIM TO BE INOPERATIVE BUT MANUAL TRIM SERVICEABLE. THE FLIGHT CREW DECIDED TO TURN BACK DUE TO THESDR P7UR201126001B-Nut · leakingWHEN PERFORMING AN INSPECTION OF THE ACFT, A HYD LEAK WAS NOTED ABOVE THE PYLON ON NR1 ENGINE. UPON FURTHER INVESTIGATION, A LOOSE B-NUT WAS FOUND ON THE HYD A SYSTEM PRESSURE LINE. SKYDROL WAS FOUND LAYING IN THE ENGINE STRUT TORQUE BOX AREA BETWEEN NAC STA 2SDR CA110630005Control Lever · brokenACFT TAKING OFF REPORTS GEAR WILL NOT RETRACT. FLIGHT CREW CARRIED OUT NON NORMAL CHECKLIST AND CONCLUDED THAT THE GEAR LEVER LOCK SOLENOID IS AT FAULT AND AN OVERRIDE WOULD BE REQUIRED. NON NORMAL CHECKLIST CARRIED OUT WITH OUT INCIDENT. ACFT DIVERTED WHERSDR CA110606018Probe · failedMADE AIR TURN BACK TO STATION DUE TO CREW EXPERIENCING MULTIPLE FMC, A/P AND ENGINE DISPLAY FAULTS AND THE LACK OF AVAILABLE PARTS AND MX. PROBLEM ISOLATED TO TAT PROBE FAILURE. PROBE REPLACED ON SNAG G021767. AUTO THROTTLE ENGAGED FAILED TO CONTROL SPEED, ASDR CA110530004Idg · failedACFT ABORTED TAKEOFF BELOW 65 KNOTS DUE TO MASTER CAUTION ELEC LIGHT CAUSED BY DRIVE LIGHT ILLUMINATED ON P5-5. ENGINE NR 2 DRIVE LIGHT ILLUMINATED. NR 2 IDG R & R IAW AMM 24-11-11. OPS TESTED NR 2 IDG IAW AMM 24-11-00-700-803. FUNCTIONAL CHECKED SERVICESDR DALA1134023607Power Supply · inoperativeINTERMITTENT EMERGENCY EGRESS LIGHTING AISLES AND EXIT HATCHES. REPLACED POWER SUPPLY M1672 CHECKS OK.SDR CA110512003Snubber · unserviceableAFTER FLIGHT, L2 DOOR WAS JAMMING DURING OPENING. THE DOOR WAS INSPECTED, THE L2 DOOR SNUBBER WAS FOUND UNSERVICEABLE AND WAS REPLACED.SDR DALA1122693608Light · inoperativeEXTERIOR EMERGENCY EGRESS LIGHTS ARE INOPERATIVE AT DOORS L1, L2, AND R2. MAINTENANCE RE-LAMPED EACH POSITION AND SYSTEM NOW CHECKS GOOD.SDR CA110128008Connector · dirty(CAN) JUST PRIOR TO TOP OF DESCENT, NR 1 ENGINE FUEL FILTER BYPASS LIGHT CAME ON. FUEL FILTER BYPASS CONNECTOR CLEANED AND REINSATLLED IAW AMM 73-34-01. ENGINE RUN C/O IAW 71-00-00 AND NR 1 EEC BITE C/O IAW AMM 73-21-00. NO CURRENT FAULTS AT THIS TIME. ON TASDR CA110126005Warning System · out of adjust(CAN) AIRCRAFT ABANDONED TAKEOFF DUE TO SPEEDBRAKE DO NOT ARM INDICATION. DO NOT ARM ILLUMINATED AT 50 KTS. TAKEOFF ROLL ABANDONED, NO HIGH ENERGY STOP INSPECTION REQUIRED BUT WILL BE ADDRESSED AS SUCH IN LOG BOOK. FIM BEING CARRIED OUT. ALSO HAD REVERSER LIGHSDR CA110119003Check Valve · failedON DESCENT WITH A/T ENGAGED, FELT/HEARD ENGINE SURGE/STALL. DISENGAGED A/T AND UPON MANUAL APPLICATION FWD AND AFT OF THRUST LEVERS, HEARD FELT SURGE/STALL. ENGINE PARAMETERS REMAINED NORMAL AND WERE BEING MONITORED ON DESCENT. THE FLIGHT MADE AN UNEVENTFUL LASDR CA110107011Thermal Switch · failedNR 2 ELEC HYD PMP OVERHEAT LIGHT ON DURING CLIMB. ELEC NR 2 OVERHEAT WARNING SW. FOUND FAULTY, SWITCH REPLACED IAW AMM 29-32-12. EMDP CASE DRAIN FILTER FOUND NO CONTAMINATION, LEAK CHECK CARRIED-OUT IAW AMM 29-11-41. OPS TESTED SERVICEABLE. P/N OFF: G37-1J
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