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 05FDEA00750Frame · corrodedAREA BEHIND AFT CARGO COMPARTMENT FRAME 77 LEFT SIDE APPROX STR 49L STR HAS 5 SQ INCHES OF CORROSION. REMOVED CORROSION AT FRAME 77 FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00 FIG 104 TABLE 102. REMOVED AND REPLACED STRINGER SECTION WITH NEW 48L FR SDR 05FDEA00749Door Frame · corrodedAREA BEHIND BULK CARGO BETWEEN FRAMES 72-74 LEFT SIDE AT STRINGER 49 HAS 15 SQ" OF CORROSION. REMOVED CORROSION FR 72-74 FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00 FIG 104. REMOVED AND REPLACED STRINGER SECTION 49L FR 72 TO 78 IAW A310-200 SRM 53-SDR 05FDEA00748Stringer · corrodedAFT OF BULK CARGO BILGE AREA STGR 53 LT HAS 2 AREAS OF CORROSION BETWEEN FR 70-71. REMOVED REQUIRED FASTENERS AND REMOVED CORROSION IAW A310-200 SRM 51-40-21 AND SRM 51-74-10. MATERIAL LOSS AFTER CORROSION REMOVAL WENT OUT OF LIMITS IAW A310-200 SRM 53-10-00SDR 05FDEA00747Stringer · corrodedAFT OF BULK CARGO AT BILGE AREA, STRINGER 56 LT HAS NUMEROUS CORROSION ON STRINGER'S. RUNS THROUGH FRAME 70-71 AND FRAME 72, AS MARKED. REMOVED FASTENERS ON STR 56 LT AT FR 70-71 AND 72 IAW A310-200 SRM 51-40-21. REMOVED CORROSION IAW A310-200 SRM 51-74-10SDR 05FDEA00746Bracket · wornNR 2 ENGINE RT CORE COWL DOOR HOLD OPEN ROD SUPPORT BRACKET ON ENGINE IS WORN. REMOVED AND REPLACED BRACKET, INSTALLING IAW A310-200 AMM 20-21-12.SDR 05FDEA00745Bracket · crackedNR 1 PYLON AFT END AT APPROX RIB 18 1 BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET IAW A310-200 SRM 51-72-10.SDR 05FDEA00744Beam · corrodedMAIN DECK CARGO CLS ADAPTER BETWEEN R1 AND R2 AT FRAME 50 IS CORRODED. REMOVED AND REPLACED BEAM IAW A310-200 SRM 51-72-10.SDR 05FDEA00743Seat Track · corrodedMAIN CABIN FRAME 61/62, SCALLOPS ARE WORN ON TRACK '0'. REMOVED FLOOR PANELS FOR ACCESS IAW A310-200 SRM 51-40-21. REMOVED AND REPLACED SEAT TRACK SECTION IAW A310-200 SRM 51-72-10 AND 53-10-16. REINSTALLED FLOOR PANELS IAW A310-200 SRM 51-40-21.SDR 05FDEA00742Seat Track · corrodedMAIN CABIN FRAME 62 TO 73 SEAT TRACK '0' HAS SEVERAL AREAS OF CORROSION IN ZONE 250. REMOVED AND REPLACED SEAT TRACK FROM FRAME 62 TO FRAME73 IAW A310-200 SRM 51-72-10.SDR 05FDEA00741Strap · crackedNR 1 PYLON OUTBD SIDE FWD OF PRECOOLER STRAP IS CRACKED. REMOVED AND REPLACED ANGLE IAW A310-200 SRM 51-72-10.SDR 05FDEA00740Gusset · corrodedNR 1 PYLON OUTBD SIDE AT RIB 15 ANGLE HAS 3 SQ INCHES OF CORROSION. REMOVED AND REPLACED GUSSET IAW A310200 SRM 51-72-10.SDR 05FDEA00739Gusset · corrodedNR 1 PYLON OUTBD SIDE AT RIB 16 ANGLE HAS 3 SQ INCHES OF CORROSION. REMOVED AND REPLACED GUSSET IAW A310-200 SRM 51-72-10.SDR 05FDEA00738Gusset · corrodedNR 1 PYLON OUTBD SIDE AT RIB 17 ANGLE HAS CORROSION AROUND 4 HOLES. REMOVED AND REPLACED GUSSET IAW A310-200 SRM 51-72-10.SDR 05FDEA00737Access Panel · corrodedNR 2 PYLON ACCESS PANEL NR 423EL HAS MODERATE CORROSION AROUND INTERIOR SIDE OF ALL FASTENER HOLES. REMOVED CORROSION IAW A310-200 SRM 51-74-10, VERIFIED THREE AREAS OUT OF LIMITS. VERIFIED REPAIR MATERIAL, FABBED THREE EA. REPAIR DOUBLERS AND FILLERS IAW SDR 05FDEA00627Frame · crackedREF. SNRM# N00525 MAIN CABIN FRAME 37 CLS ADAPTER -Y040 IS GOUGED AND CRACKED (BETWEEN SEAT TRACK 2 AND 3 LT). REMOVED AND REPLACED CLS ADAPTER PER A310 SRM 51-72-10 TREATED, PRIMED AND TOP COATED AREA AND FASTENERS PER A310-200 SRM 51-75-10.SDR 05FDEA00626Floorbeam · damagedFR 38 MDCC FLOORBEAM LT OF CTR AT 38 INCHES, AFTER REMOVAL OF CLS ADAPTER TO FACILITATE FRAME REPAIR, FASTENER HOLES FOUND TO BE OUT OF ROUND, FWD INBOARD HOLE ON CLS ADAPTOR AFT OUTBD, AND ALSO 2 DRILL STARTS. BLENDED OUT DRILL STARTS PER A310 SRM 51-73-10, SDR 05FDEA00625Longeron · corrodedMAIN DECK CARGO FR 14 LONGERON 4TH FROM CENTERLINE CORRODED OUT OF LIMITS. REMOVED AND REPLACED LONGERON A53610797234 WITH NEW PART IAW A310 SRM 51-72-10.SDR 05FDEA00623Seat Track · gougedMDCC SONE 241, RT NR 2 SEATRACK, FR54.2 HAS 1-EA GOUGES AREA ON SCALOPE HOLE. REMOVED DAMAGED SEAT TRACK FITTING AT MDCC ZONE 241 RT NR 2 FR54.2 AND REPLACED WITH NEW SEAT TRACK FITTING P/N A5381114620000 IAW A310 SRM 51-40-21.SDR 05FDEA00622Seat Track · corrodedMAIN DECK CARGO ZONE 240 LT NR4 SEAT TRACK, FR 54 AND FR 54.1 CORROSION PROPAGATED ON SEAT TRACK FLANGE SCREW HOLES 2-AREAS. BLENDED CORROSION IAW A310-200 SRM 51-74-10, 53-10-16, CHECKED LIMITS AND NOTED FOR MATERIAL LOSS, DUE TO CORROISION OUT OF LIMITS RESDR 05FDEA00574Skin · corrodedCORR B/T STR 34-35 FROM FS 39 AFT APPROX 8 IN LT REF N00850. COMPLIED WITH EA 6-5315-86078.SDR 05FDEA00526Skin · damagedREPAIR AT STN 2135 FS 38.1 STN 2188 FS 38.2 STR 49 LT, AIR CONDITION ACCESS DOOR. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-72-10 AND 51-40-21.SDR 05FDEA00523Skin · damagedMOD TYPE Y MOD NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR). COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FUSELAGE - REPAIR AT FR 15/16 BELOW R1 DOOR (PLEASE EVALUATE). REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIRSDR 05FDEA00572Access Panel · damagedLOWER FUSELAGE FWD CARGO DOOR ACCESS PANEL NR 811BR HAS (2EA) CRACKS AT FASTENER HOLE. REPLACED WITH NEW ACCESS PANEL DUE TO EXCESSIVE REPAIRS AND PANEL DEFORMATION IAW A310-200 SRM 51-71-30. PAINTED IAW A310 SRM 51-75-10.SDR 05FDEA00568Rib · corrodedNR 2 PYLON OTBD SIDE RIB 16A UPPER AREA BRACKET LWR AREA HAS AN AREA OF CORROSION EXTENDING UNDER FASTENERS. REMOVED AND REPLACED BRACKET IAW A310-200 SRM 51-72-10. REINSTALLED 3 NUTPLATES IAW A310 SRM 51-40-21. (SEE JPF)SDR 05FDEA00566Skin · damagedREPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. ITEM NR 27 OF LIST FUSELAGE DOUBLER TOP RT SIDE AT FR 78. FUSELAGE DOUBLER ON TOP RT SIDE AT FRAME 78 FOUND TO BE IN CONFORMANCE WITH A310-200 SRM 53-10-12 FIG 216 THIS REPAIR SDR 05FDEA00565Skin · damagedREPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. ITEM NR 20 OF LIST FUSELAGE DOUBLER LOWER LT SIDE AFT OF LT MLG DOOR OPENING. FUSELAGE DOUBLER FOUND TO BE IN CONFORMANCE WITH AIRBUS DWG A538-12568 LOWER LT SIDE AFT OF LT MLGSDR 05FDEA00563Angle · corrodedFRAME 86 JUST ABOVE THS JACKSCREW 1 AREA OF CORROSION BETWEEN 2EA FASTENERS ON L-ANGLE. REMOVED CORROSION IAW A310 SRM 51-73-10. EVALUATED AREA AND FOUND IT TO BE OUT OF LIMITS IAW A310 SRM 53010-00. REMOVED AND REPLACED L-ANGLE IAW A310 SRM 51-40-21. TREASDR 05FDEA00550Door · crackedAFTER REMOVAL OF PANEL 143GL ON SNRM N00035, FOUND RAM AIR EXHAUST DOOR SURROUND BOX TO HAVE A 10 INCH CRACK ON INBD SIDE UPPER RADIUS. REMOVED AND REPLACED LT RAM AIR EXHAUST.SDR 05FDEA00549Seat Track · gougedRT NR 2 SEATRACK FR 54.2, HAS 1 GOUGED AREA ON SCALOPE HOLE. REMOVED DAMAGED SEAT TRACK FITTING AT MDCC SONE 241 RT NR 2 FR 54.2 AND REPLACED WITH NEWS SEAT TRACK FITTING P/N A5381114620000 IAW A310-200 SRM 51-40-21.SDR 05FDEA00514Regulator Valve · malfunctionedAPPROX 80-90 KNOTS GOT ECAM RED LIGHT FOR "HIGH OIL PRESS" NR 1 ENG DID RTO LIGHT WENT OUT. AT IDLE NR 1 ENG = 54 PSI, NR 2 ENG = 44 PSI. REMOVED AND REPLACED NR 1 OIL PRESS REGULATOR VALVE PER AMM 79-21-04-4. PERFORMED ENG RUN PER JRH. ALL PARAMETERS NOSDR 05FDEA00513Transmitter · malfunctionedRTO RPLB RWY 25 AT 95 KTS WITH A OIL PRESSURE HIGH INDICATION ON LOWER FORWARD INSTRUMENT PANEL. LIGHT OUT AFTER SEVERAL SECONDS. DRAINED ENG NR 1 OIL TANK PERFORMED SNIFF CHECK, NO FUEL CONTAMINATION NOTED. REMOVED AND REPLACED OIL PRESS TRANSMITTER PER SDR 05FDEA00480Seat Track · corrodedM DECK ZONE 240, LEFT NR 2 SEAT TRACK, FR47, FR51, FR51.5, FR52.5, FR53 AND FR54, CORROSION INSIDE SCALLOPED HOLES, 6-AREAS. BLENDED CORROSION PER A310 SRM 51-74-10 MEASURED MATERIAL LOSS AND FOUND ALL AREAS WITHIN LIMITS EXCEPT FOR AREAS AT FRS 51.5 AND 52.5SDR 05FDEA00479Adapter · crackedMDCC ZONE 241, BETWEEN RT SEAT TRACK 2-3 FR 43, 1-EA. CLS ADAPTER HAS CRACKED UNDERNEATH. REMOVED AND REPLACED CLS ADAPTER IAW A310 SRM 51-72-10.SDR 05FDEA00478Seat Track · corrodedM DECK CARGO COMPT LT NR 4 SEAT TRACK, FR 48, FR 49, FR 50, FR 52.5, FR 53.5 CORROSION INSIDE SCALOPE HOLES 5-AREAS AS MARKED. REMOVED CORROSION IAW SRM 51-74-10. OUT OF LIMITS IAW A310 SRM 53-10-16 FIG 101. CUT AND REMOVED BAD SECTION OF SEAT TRACK FROM FRSDR 05FDEA00476Seat Track · corrodedMDCC ZONE 241, RT SEAT TRACK NR 5, FR39.5, HAS 1-AREA OF CORROSION INSIDE SCALLOPED HOLE. REMOVED DAMAGED SEAT TRACK AND REPLACED WITH NEW SEAT TRACK P/N A53810820000IAW A310-200 SRM 51-72-10.SDR 05FDEA00475Intercostal · bentBETWEEN FR 84 AND FR 85 STG 34L INTERCOSTAL IS BENT. INTERCOSTAL ANGLE HAS BEEN REMOVED AND REPLACED IAW A310-200 SRM 51-40-21.SDR 05FDEA00474Seat Track · corrodedREF SNRM# N00536 MDCC ZONE 241 RT SEAT TRACK NR 5 FR 5.5 FR50 FR50.5 FR53 FR54 CORROSION INSIDE SCALLOPED HOLES 5-AREAS. REMOVED CORROSION IAW SRM 51-74-10 OUT OF LIMITS IAW SRM 53-10-16 FIG 101. REMOVED BAD SECTION OF TRACK FABBED REPAIR SPLICES AND TRACK ISDR 05FDEA00473Strap · crackedREF. SNRM NR N00844 BETWEEN FR 86 AND FR 87 STG 34L (LT) INTERCOSTAL IS BENT ANGLE STRAP FOUND TO BE CRACKED REMOVED AND REPLACED WITH NEW ANGLE IAW A310 SRM 51-40-21.SDR 05FDEA00472Skin · dentedREPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. ITEM NR 8 ON LIST FUSELAGE, LT SIDE FR77 AT 3 O'CLOCK POSITION. REPAIRED DENT AREA IAW A310 SRM 53-10-12 FIG 112 AND 51-73-10 PARA. 7 FIG 4. TREATED BARE METAL IAW A310 SRM 51-SDR 05FDEA00471Bracket · lightning strikeLIGHTNING STRIKE TO BRACKET TOP OF RUDDER RIGHT SIDE FOUND AFTER REMOVAL OF PANEL 326AT FOR STATIC WICK REPAIR NOO238. REMOVED AND REPLACED COUPLING IAW A310-200 SRM 51-40-21, TOPCOATED COUPLING IAW A310-200 SRM 51-75-10.SDR 05FDEA00470Seat Track · corrodedMDCC ZONE 252 RT NR 4 SEAT TRACK HAS AREA OF CORROSION INSIDE SCALLOPED HOLE (1- AREA ONLY) AT FRAME 64.5. REMOVED CORROSION IAW A310-200 SRM 51-74-10 FOUND CRACK, FABBED REPAIR SECTION AND SPLICED IAW A310-200 SRM 51-10-16 FIG 208 AND SRM 51-40-40. REMOVEDSDR 05FDEA00469Bracket · corrodedNR 1 PYLON OTBD SIDE UPPER AREA RIB 15A BRACKET ON LWR AREA HAS CORROSION EXTENDING UNDER FASTENERS FOR NUT PLATE. CORROSION REMOVED IAW A310 SRM 51-74-10, NDT MATERIAL THICKNESS AFTER THICKNESS IS OUT OF LIMITS. REMOVED AND REPLACED BRACKET AND 3EA NUTPLASDR 05FDEA00468Seat Track · corrodedMDCC SONE 252 RT NR 4 SEAT TRACK FS 68 FS 69.5 FS 70.5 HAS 3 AREAS OF CORROSION INSIDE SCALLOPED HOLES. REMOVED DAMAGED SEAT TRACK SECTION AND REPLACED WITH NEW SEAT TRACK SECTION FROM FRAME 69.5 TO FRAME 71.5 IAW A31-200 SRM 51-10-16 FIG 208 RT NR 4 RESTOREDSDR 05FDEA00467Seat Track · corrodedMDCC RT NR 5 SEATRACK, FS 78 FS 78.5 HAS 2 AREAS OF CORROSION INSIDE SCALLOPED HOLES. REPLACED SEAT TRACK IAW A310-200 SRM51-72-10, FABRICATED NEW SEAT TRACK IAW DRAWING A53279232, REMOVED REINSTALLED FLOORBOARDS IAW A310 AMM 53-10-21. REMOVED, REINSTALLED GSDR 05FDEA00466Panel · corrodedCORROSION AROUND FASTERNER HOLES, LEFT AND RIGHT SIDE TOP OF RUDDER, PANEL 326AT REMOVED TO REPAIR STATIC WICK BASE N00238.SDR 05FDEA00465Adapter · corrodedMAIN CABIN AT FRAME 38 CLS ADAPTOR, -YE15 HAS 1EA AREA OF CORROSION (BETWEEN SEAT TRACK LAND 2 LT)SDR 05FDEA00462Outflow Valve · fluctuatesA/C WOULD NOT PRESSURIZE ON CLIMB-OUT OF MEM. LEVELED OFF AT 9000. CABIN VSI CLIMBING AT SAME RATE AS A/C CLIMB. NR 2 FWD AND AFT VALVES DISPLAYED FULL OPEN AND AMBER IN COLOR. NR 1 FWD AND AFT OUTFLOW VALVES OSCILLATED VIOLENTLEY OPEN AND CLOSED THROUGH FSDR 05FDEA00461Uplock Hook · damagedNOSE LANDING GEAR DOOR AMBER LIGHT ILLUMINATE ON BOTH PANELS FOLLOWED ECAM. QRH DECLARED EMERGENCY FOR OVERWEIGHT LANDING. LANDING WEIGHT 289.0 AND 250 FPM RATE OF DESCENT. NOTICEABLE VIBRATION FROM NOSE GEAR DOOR. FURTHER T/S FOUND RT UPLOCK ASSY-NLG DOOSDR 05FDEA00439Panel · damagedRT WING PANEL 650JB HAS 4 EA ELONGATED REF N00522. REPAIRED PANEL 650JB IAW EA 6-5710-86051.SDR 05FDEA00425Rib · crackedRT WING 4 IN IB OF RIB 30 L/E AREA AFT PANEL LANDING IS CRACKED REF N00636. REMOVED AND REPLACED LANDING IAW SRM 51-40-21 AND 51-72-10 AND DRW A57243955.
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