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 engine_model_key = 'V2500A1' 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 engine_model_key = 'V2500A1' 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 AWXA200400731Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 BETWEEN FR 64 AND FR 66. MAINTENANCE REMOVED AND REPLACED BEAM Y765 FROM FR 64 TO FR 66 IAW A319 SRM 51-42-11 PG. 39 AND 41 FIG. 18.SDR AWXA200400746Floor Panel · crackedMAJOR REPAIR, DURING B-04 CHECK FOUND 2 EACH 1INCH CRACKS IN FLOOR PANEL 221EF. MAINTENANCE CUTOUT DAMAGE IN FLOOR PANEL 221EF, AND PERFORMED BOND REPAIR IAW A319 SRM 53-02-00, FIG. 202.SDR AWXA200400727Floorbeam · corrodedDURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 AT FR 66. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 AT FR 66 IAW A319 SRM 51-42-11 PG. 6, 7, & 41, FIG. 18. REGISTRATION NR WAS CHANGED TO REFLECT THE CORRECT AIRCRAFT, THIS EVENT DID NOT OCCUR SDR AWXA200400745Floor Panel · corrodedDURING B-04 CHECK FOUND CORROSION ON AFT SIDE CORNER OF FLOOR PANEL 261FF FROM FR 66 TO FR 68, AND Y1292 LT TO 1732 LT. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 261FF IAW AWA T/C C1D25310.SDR YENA200437Electrical Box · malfunctioned3O MINS INTO FLIGHT FA NR 1 REPORTED AN ODOR EMITTING FROM ROW 1-4, TURNED LIVE TV MASTER SWITCH TO OFF, SMELL WAS GONE AFTER 3 MIN. TV'S WERE WORKING PRIOR TO TURNING THE MASTER SWITCH OFF. COMPLIED WITH INFO NOTICE 2003-T050TR A. NO ABNORMALITIES WERE FOUSDR AWXA200400583Proximity Sensor · faultyEMERGENCY LANDING - FLT 0280 - ON APPROACH, EN ROUTE WITH LANDING GEAR SELECTED DOWN GEAR DID NOT EXTEND, MANUALLY SELECTED GEAR DOWN AND DECLARED EMERGENCY. MAINTENANCE PERFORMED WIRING CHECK AND FOUND RESISTANCE ON LT MAIN LANDING GEAR (MLG) DOOR OPEN PROXISDR AWXA200400563Plate · corrodedMCN - MAJOR REPAIR - DURING B-03 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF LT AFT SHEAR PLATE AT THE AFT END OF Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED LT AFT SHEAR PLATE Y1292 FROM FR 69 TO FR 70; FABRICATED A NEWSDR YENA200417Housing · defectiveLT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. FOUND RECEPTACLE AT FAULT. REPLACED LIGHT HOUSING ASSY.SDR AWXA200400277Blade · crackedAFTER TAKEOFF, EN ROUTE. NR 2 ENG STALLED WITH EGT OVERTEMP OF 843 DEGREE, FOLLOWED ECAM & DECLARED EMERGENCY. MX R / R NR 2 ENG IAW T/C. BORESCOPE OF HPC REVEALED 1, 7TH STAGE BLADE FRACTURED ROOT, & A SECTION OF 7TH STAGE REAR DAMPER WIRE MISSING OVER A SPASDR CA040319003Valve · malfunctioned(CAN) CREW REPORTED SEVERAL INCIDENTS OF UNEXPLAINED FUEL LOSS FROM RT FUEL SYS RESULTING IN INCONSISTENT FUEL IMBALANCES ON VARIOUS OCCASIONS. NO VISIBLE SIGNS OF FUEL SYS LEAKAGES WITHIN ACRFT NOR ON GROUND. FUEL QTYS CLOSELY MONITORED BY CREW WHILE TROUBLESDR RYNA54233Transducer · faultyDURING CRUISE FLIGHT, ECAM DISPLAYED (LEFT WING AIR LEAK) MESSAGE. PERFORMED ECAM ACTION. RETURNED, AS A HEAVY WEIGHT LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE BLEED PRESSURE TRANSDUCER.SDR AWXA200400233Bleed Valve · failedON CLIMBOUT AT APPROX 1500 FT HEARD A LOUD BANG & AC SHUTTERED, ECAM INDICATED NR 2 ENG STALL, AFTER ECAM MESSAGE ENG OPERATED NORMALLY. TURNED BACK & LANDED WITHOUT FURTHER EVENT. MX BORESCOPED HPC 3 & 6 STAGE, NO DEFECTS NOTED. PERFORMED PRESSURE BURNER SESDR AWXA200400178Epsu · dischargedEMERGENCY LIGHT SYSTEM TEST FAILED AT PUSH BUTTON ON FLIGHT ATTENDANT FORWARD PANEL. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD.SDR AWXA200400189Seat Track · corrodedDURING B-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR BEAM TEE CAP (SEAT TRACK) AT CLIP NUT LOCATIONS BETWEEN FR 17 AND FR 20, Y1292 RT. MAINTENANCE REMOVED DAMAGED SEAT TRACK BETWEEN BS 7830 AND BS 8000, Y1292 RT; FABRICATED 6 EACH REPASDR AWXA200400190Floorbeam · corrodedDURING B-04 CHECK CORROSION WAS FOUND ON FLOORBEAM BETWEEN FR 66 AND FR 68, Y1292 RT. MAINTENANCE REMOVED DAMAGED FLOORBEAM BETWEEN FR 66 AND FR 68, Y1292 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM IAW DWG D53472172; INSTALLED REPAIR PART IAW A320 SRM 51-4SDR AWXA200400191Floorbeam · corrodedDURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM AT FR 68, Y1292 RT. MAINTENANCE REMOVED DAMAGED FLOORBEAM AT FR 68, Y1292 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM IAW DWG D53472189; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 9-14, 16 SDR AWXA200400055Fuel Control · malfunctionedPHX - ABORTED TAKEOFF - FLT 0820 - ON TAKEOFF AT PHX EN ROUTE FOR BOS THE NR 1 ENGINE FAILED TO ACCELERATE, REJECTED TAKEOFF AT 60 KTS. TAXIED CLEAR OF RUNWAY AND RAN UP NR 1 ENGINE, ENGINE AGAIN FAILED TO ACCELERATE ABOVE 1.1 EPR, RETURNED TO GATE. MAINTENASDR AWXA200301607Windshield · delaminatedAIR TURN BACK, AFTER TAKEOFF, EN ROUTE FOR SLC THE FIRST OFFICERS WINDSHIELD DELAMINATED, TURNED BACK AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD IAW AMM 56-11-11. VENDOR DID NOT PERFORM FAILURE ANALYSIS OF SDR AWXA200301340Overheat Loop · faultyPHX - ABORTED TAKEOFF - FLT 0567 - ON APPLICATION OF TOGA POWER FOR BLEEDS OFF TAKEOFF AT PHX EN ROUTE FOR MCO, RECEIVED ECAM MESSAGES FOR ENGINE NR 1 BLEED LEAK FOLLOWED BY APU BLEED FAULT & AIR PACK NR 1 FAULT. REJECTED TAKEOFF AND RETURNED TO GATE. MAINTESDR RYN2004F00011Floor Support · corrodedAT (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 34 ABOVE STRINGER 34 IN FORWARD CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 34 JUST ABOVE 34L IN FORWARD CARGO COMPARTMENT.SDR DLM90030893Switch · unserviceableRIGHT FUEL PRESSURE LIGHT ILLUMINATED ON TAKEOFF ROLL. REPLACED FUEL FILTER AND PRESSURE SWITCH PER MAINT MANUAL.SDR AWXA200301085Packing · rupturedPHX - FLIGHT CONTROL - FLT 0261 - EN ROUTE FROM YYZ TO PHX RECEIVED ECAM (YELLOW) NR 2 ENGINE HYDRAULIC PUMP LOW PRESSURE INDICATION. LANDED AT PHX WITHOUT INCIDENT, EMERGENCY EQUIPMENT CALLED TO STANDBY AS PRECAUTION. MAINTENANCE DISCOVERED A BLOWN SEAL AT POSDR 23431924Sill · corrodedAT (C) CHECK, FOUND L2 DOOR SILL HAS RIVET HEADS THAT HAVE EXFOLIATED CORROSION BETWEEN FR 66 AND FR 68. REMOVED AND REPLACED L2 DOOR SILL, LOWER FORWARD CORNER FITTING, DRAINS AND ANGLE AT FRAME 67, LT LOWER UNDER SILL. (SDR NR 23431924)SDR RYN2004F00025Control Panel · faultyAFTER TAKE OFF FROM ATL, NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED WITH NO ECAM MESSAGE. AIRCRAFT RETURNED TO DEPARTURE AIRPORT AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ANNUNCIATOR LIGHT TEST AND INTERFACE BOARD. OPERATIONAL CHECKED NORMAL. NO FASDR RYN2004F00008Attach Fitting · corrodedAT (C) CHECK FOUND AFT CABIN NR 2 RT DOORWAY AFT GIRT BAR ATTACH FITTING PLATE WITH CORROSION. REMOVED AND REPLACED AFT GIRT BAR ATTACH FITTING PLATE ON AFT CABIN NR 2 RT DOORWAY.SDR AWXA200301082Floor Support · corrodedMCN - MAJOR REPAIR - DURING C-07 CHECK CORROSION WAS FOUND AT FASTENER HOLE ON MAIN CABIN FLOOR SUPPORT AT Y558 (LBL 22), JUST FORWARD OF FR 66. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED FLOOR SUPPORT FROM SDR AWXA200301096Floorbeam · corrodedDURING C-07 CHECK CORROSION WAS FOUND ON Y1292 FLOORBEAM AFT SIDE OF FR 66. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED Y1292 FLOORBEAM FROM FR 64 TO FR 67; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PARTS IAW A3SDR AWXA200301097Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-07 CHECK CORROSION WAS FOUND ON Y765 FLOORBEAM FR 67-69. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED Y765 FLOOR BEAM FROM FR 67 TO FR 69; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPSDR RYN2004F00007Floor Panel · corrodedAT (C) CHECK FOUND AFT LAV FLOOR PANEL WITH CORROSION AT NUMEROUS LOCATIONS AT ATTACHMENT POINTS FOR BLOW OUT DOOR FRAME. REPAIRED AFT LAV FLOOR PANEL, CORROSION AT ATTACHMENT POINTS FOR BLOW OUT DOOR FRAME. REMOVED AND REPLACED INSERTS.SDR DLM90030844Bleed Valve · failedNR 2 ENG COMPRESSOR STALLS LESS THAN 1.2 EPR. REPLACED 7TH STAGE BLEED VALVE.SDR RYN2004F00010Threshold · corrodedAT (C) CHECK FOUND R2 DOOR THRESHOLD HAS 5 CORRODED RIVETS. REMOVED AND REPLACED CORRODED RIVETS AT R2 DOOR THRESHOLD.SDR AWXA200301008Connector · damagedEN ROUTE, AFTER TAKEOFF BLEEDS OFF RECEIVED ECAM MESSAGE NR 2 ENG BLEED ABNORMAL PRESS. TURNED OFF APU BLEED SWITCH NR 2 ENG BLEED ONLY AT 24 PSI, DIVERTED FOR REPAIR. MAINT REMOVED AND REPLACED BLEED PRESS REG VALVE CTRL SOLENOID (10HA2), DUE TO CLASS 3 FAULTSDR AWXA200300971Actuator · malfunctionedON TAKEOFF ROLL AT SMF EN ROUTE FOR PHX RECEIVED NR 2 ENGINE COMPRESSOR VANE FAULT, REJECTED TAKEOFF AT 60 KTS. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75306, OPERATIONAL AND LEAK CHECK WERE GOOD PER T/C F5MSDR CA030805006Control Unit · failed(CAN) ON APPROACH, AC APPROACH STATUS REVERTED TO CAT III SINGLE WITH WHEEL PAGE SHOWING AMBER STEERING. N/W STEERING SWITCH CYCLED OFF THEN ON WITH INDICATIONS RETURNING TO NORMAL AND CAT III DUAL. UPON LANDING, IDLE REVERSE WAS SELECTED(NOISE ABATEMENT) BUTSDR AWXA200300869Bleed Valve · malfunctionedON TAKEOFF AT PHX EN ROUTE FOR BOS OVER TEMP OCCURRED ON THE NR 2 ENG, REJECTED T/O AT 100 KTS. MAINT COMPLIED WITH STEP 4C OF AMM FORCE CK OF VSV MECH, FORCE REQUIRED LESS THAN 350 INCH POUNDS. R & R NR 2 ENG MASTER BLEED VALVE ACT, OPERATIONAL CHECK WAS GOSDR AWXA200300866Pump · defectiveON TAKEOFF, RECEIVED ECAM WARNING FOR NR 1 ENG COMPRESSOR VANE FAULT ALONG WITH N1/N2 OVERSPEED, REJECTED TAKEOFF AT 60 KTS, RETURNED TO BLOCK. MX R & R NR 1 ENG VSV ACTUATOR, FAULT STILL PRESENT DURING ENG RUN. R & R NR 1 ENG FUEL METERING UNIT. REPLACED LOSDR AWXA200300840Odor · detectedAFTER TAKEOFF FROM LAS EN ROUTE FOR PDX NOTICED AIRCRAFT VIBRATION, CLIMBING THROUGH FL 180 NR 2 ENGINE VIBRATION AT 2.2, VIBRATION BECAME STRONGER AND AFT CABIN FLIGHT ATTENDANT REPORTED A BURNING ODOR COMING FROM AFT GALLEY AREA. ODOR BECAME STRONGER AS FLISDR AWXA200300811Power Supply · dischargedLAS - EEL - DURING EMERGENCY LIGHT TEST THE SYSTEM INDICATED OK, BUT FAILED TO ILLUMINATE THE EMERGENCY ESCAPE PATH LIGHTS. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL TEST WAS GOOD IAW AMM 33-51-00.SDR AWXA200300805Eec · failedDURING TAKEOFF AT PHX EN ROUTE FOR DEN THE CREW PUSHED POWER UP FOR TAKEOFF AND THE NR 2 ENGINE DID NOT RESPOND, POWER REMAINED AT IDLE, REJECTED TAKEOFF. FLIGHT CREW NOTED THAT THE NR 1 ENGINE DID RESPOND NORMALLY. APPROXIMATELY 5 MINUTES LATER; RECEIVED ECSDR AWXA200300776Bleed Actuator · faultyON TAKE OFF ROLL AT PHX EN ROUTE TO YYC, EGT LIMIT EXCEEDED (645) DEGREES. ABORTED TAKEOFF AND RETURNED TO GATE. MECHANIC REMOVED AND REPLACED THE 2.5 BLEED (LPC MASTER) ACTUATOR IAW AWA T/C R5M75307 AND PERFORMED POWER ASSURANCE TESTS IAW AWA T/C F5M71312 ASSDR AWXA200300736Actuator · faultyAT CRUISE FL 360, NR 2 ENG COMPRESSOR VANE ECAM MSG, AT FL 290 NR 2 ENG STALLED. SHUTDOWN ENG, EMERGENCY EQUIP TO STANDBY. LANDED, TAXIED TO GATE. REPORT INDICATED NR 2 ENG OVERTEMP 663'C APPX 7 SEC. MX INSPECTED INTERMEDIATE PRESSURE CHECK VALVE, FAULT ISSDR AWXA200300708Shear Pin · defectiveDURING 8-DAY CHECK FOUND THE R-1 DOOR ASSIST BOTTLE WOULD NOT HOLD PRESSURE. MAINTENANCE REMOVED AND REPLACED THE R-1 DOOR DAMPER CYLINDER SHEAR PIN AND PUNCTURE DISK IAW 52-11-14-401, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300698Actuator · looseTEARDOWN REPORT OF ENG IDENTIFIED HIGH INTERNAL LEAKAGE AT VSV ACT ALONG WITH SLOW PISTON VELOCITY. TEARDOWN REVEALED THAT CONTROL SERVO VALVE & SEAL WERE WORN BEYOND LIMITS & CAUSED INTERNAL LEAKAGE AT VSV ACT. FAILURE MODE & EFFECTS ANALYSIS CONSIDER THIS A SDR 2003FA0000760Seal · corrodedPART RECEIVED FROM REPAIR STATION FOR FPI IAW IAE V2500A1A5 (REV 53) AND V2500D5 (REV 35), ATA 72-43-20, TASK 70-23-02-230-501. PART REJECTED AT FPI FOR HOLES AND PITS ON INNER GROVE.SDR AWXA200300370Engine · malfunctionedDURING TOGA POWER APPLICATION NR 2 ENGINE SPOOLED UP SLOWER THAN NR 1 ENGINE CAUSING AN ISSUE ON WET RUNWAY, REJECTED TAKEOFF APPROX 15 KTS. INITIAL SPOOL DIFFERENCE WAS ATTRIBUTED TO ENGINES NOT BEING EXACTLY MATCHED AT 1.05 EPR. ON 2ND ATTEMPT ENGINES MATCSDR AWXA200300416Thermocouple · defectiveON DESCENT WITH AUTO THROTTLE ON 11,000 FT, NR 2 ENGINE SPOOLED NORMALLY TO MAINTAIN MANAGED SPEED, NR 1 ENGINE DID NOT SPOOL FOR 3 TO 4 SECONDS. NR 1 ENGINE WENT TO CLIMB THRUST RESULTING IN SUBSTANTIAL YAW (3 TO 5 DEG) ROLL OF 2 TO 3. ON IDLE DESCENT 6000 SDR AWXA200300125Snubber · weakMCN - EMERGENCY EVACUATION - DURING C-04 CHECK, THE L-1 DOOR SNUBBER WAS FOUND TO BE WEAK DURING OPERATION. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR SNUBBER CYLINDER PER AIRBUS AMM TASK'S 52-13-14-020-057, AND 52-13-14-220-053. OPERATIONAL CHECK WAS PERFSDR CA030117006Hose · chafedHYDRAULIC HOSE FOUND CHAFFED THROUGH ON ENGINE 1 GREEN HYDRAULIC SYSTEM PUMP PRESSURE TRANSDUCER. REF. 29-11-49-80A TUBES INSTL-HYDRAULIC, V2500, ENGINE 1, ZONE 400/ITEM 310.SDR AWXA200300014Actuator · inoperativeFLT 0660, ON TAKEOFF ROLL EN ROUTE RECEIVED ECAM MESSAGE (ENG 1 COMPRESSOR VANE); REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75306. LUBRICATED VSV, PERFORMED MAINTENANCSDR AWXA200201208Apu · malfunctionedTAILPIPE FIRE, AFTER (APU) SHUT DOWN, A TAILPIPE FIRE WAS NOTICED BY GROUND CREW. MAINTENANCE INSPECTED THE APU AND FOUND NO DAMAGE TO TAILPIPE OR SURROUNDING AREA. PLACED SYSTEM ON MEL, COND. 1.
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