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 jasc_code = '5751' 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 jasc_code = '5751' 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 2010F00132Bushing · misinstalled((EBVR)) DURING THE REMOVAL OF THE RT AILERON FOR PAINT, IT WAS FOUND THAT THE OTBD HINGE BUSHING WAS NOT FULLY INSTALLED (PN 6724012-1). THE BUSHING WAS NOT INSTALLED ENOUGH WHERE THE RETAINING CLIP COULD ENGAGE IN THE GROOVE. AFTER REMOVING THE AILERON IT SDR HNAA2010063000165Stud · looseRIGHT AILERON INBD BONDING STUD SPINS. REPAIRED BONDING STUD IAW EO8-57-10-0263.SDR IPXA0660660Skin · damagedRT OTBD AILERON HAS 4 OTHER AREAS OF LIGHTNING STRIKE DAMAGE ON UPPER SURFACE OF WEDGE MARKED. STARTED SANDING AREA, FWD LIMITS TO ENGR. FINISHED DAMAGE REMOVAL REF SRM 57-60-02-2R. STARTED NR 346819. REPAIR COMPLETE SEE NRC 346819 AND ECA 020462. THIS REPAISDR IPXA0660654Wedge · damagedRT OTBD AILERON T/E WEDGE LIGHTNING DAMAGE. REPAIRED IAW EO B767-5750-38137-B.SDR A6WA201040458Skin · chafedLT AILERON L/E SKIN CHAFED FROM OTBD CTR HINGE BUT COTTER KEY. REPAIRED LT AILERON L/E SKIN FROM OTBD CTR HINGE NUT COTTER KEY IAW B/A REO 601R-57-60-078, REV A.SDR A6WA201040437Skin · unserviceableRT AILERON BOTTOM L/E INBD SKIN PN CC670-13052-2. R & R NEW SERVICEABLE SKIN.SDR FDEA201006142009Skin · dentedDENTED LOWER SURFACE INBOARD EDGE OF RT INBOARD AILERON ASSY. DENT AREA MEASURED 0.008" TO 0.060" DEEP, FOUND ACCEPTABLE AS PER SRM 51-80-01 VOLUME II REVISION 96. HFEC INSPECTION CARRIED OUT AS PER DAC NDT SPM REVISION 13 06-10-01.001 ON DENT AREA AND FOUNSDR 2010FA0000535Hinge · misinstalled((EBVR)) DURING THE REMOVAL OF THE RT AILERON FOR PAINT, IT WAS FOUND THAT THE OTBD HINGE BUSHING WAS NOT FULLY INSTALLED (PN 67240121). THE BUSHING WAS NOT INSTALLED ENOUGH WHERE THE RETAINING CLIP COULD ENGAGE IN THE GROOVE. AFTER REMOVING THE AILERON IT WSDR A6WA201040423Panel · chafedRT AILERON L/E PANEL 699BB HAS MINOR CHAFE DAMAGE BLENDED IAW SRM 57-60-00 WITH .002" MATERIAL LOSS.SDR A6WA201040422Panel · chafedRT AILERON L/E 699CB HAS MINOR CHAFE DAMAGE. REPAIRED IAW 200-57-60-06 WITH 0.0003 MATERIAL LOSS.SDR A6WA201040424Panel · chafedRT AILERON PANEL 699AB HAS MINOR CHAFE DAMAGE. REAPIRE IAW REO 601R-57-60-020 WITHIN .013 MATERIAL LOSS.SDR FDEA201006031807Skin · bentRT WING OTBD AILERON LOWER SKIN INBD EDGE IS BENT. REMOVED FASTENERS AND REMOVED DAMAGE BY CUTOUT IAW SRM 57-10-00, FIG 56, VOL I. FABRICATED DOUBLER AND FILLER IAW SRM 57-10-00, FIG 56, VOL I. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II. INSTALLED DOUBLESDR WRLA20100601362Wedge · damagedPUNCH - LEFT OUTBOARD AILERON TRAILING EDGE WEDGE ON INBOARD SIDE WAS DAMAGE DURING CARGO UNLOADING IN AFGHANISTAN. NRC U07011 ISSUED. PER SRM 57-60-01 REPAIR 1 & SRM 51-70-07 FIG 6 TO REPAIR THE DAMAGE WEDGE. PER SRM 51-60-01 PFM OUTBOARD AILERON BALANCINGSDR FDEA201006011751Wedge · crackedRT WING OTBD AILERON T/E WEDGE IS CRACKED AND PAINT IS CHIPPED FROM XW 760 TO XW 890. REMOVED T/E WEDGE SEC IAW SRM 57-20-00, FIG 10, VOL I. FABRICATED NEW T/E WEDGE AND "Z" ANGLE IAW SRM 57-20-00, FIG 10, VOL I. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II.SDR CA100809019Skin · cracked(CAN) UPON A WALK AROUND INSP, IT WAS NOTED THAT THE LT AND RT AILERONS HAD 8 IN CRACKS SPAN WAYS JUST IN FRONT OF THE STIFFNER ON THE UPPER SKIN. THE AILERONS WERE REPLACED.SDR SIMA201015805Fitting · damagedDURING MBV INSPECTION FOUND OUTBOARD AILERON FITTING HAS WORN AND OVERSIZED HOLES CAUSING HAT BUSHING TO STAY IN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE OUTBOARD ATTACH FITTING ON THE RIGHT AILERON IAW EO EM-27MR-112. THE AIRCRAFT WASDR FDEA201005291729Skin · bulgedRT WING - OTBD AILERON UPPER SURFACE AT APPROX XOA 870, FOUND BULGING. RT OTBD AILERON R & R IAW AMM 27-10-02-4 REV 10.SDR FDEA201005291724Skin · bulgedLT WING - INBD AILERON LOWER SURFACE FWD SIDE APPROX XIA 295 TO XIA 325 FOUND SKIN BULGING. REPAIRED IAW EA NR 8-5750-140484. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201005291723Skin · bulgedLT WING - OTBD AILERON LOWER SKIN FWD SIDE APPROX XOA 1006 TO XOA 1025 FOUND BULGING. REPAIR CARRIED OUT IAW EA8-5750-140483, REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 110.SDR USAA2010061691141Hinge Pin · corrodedSAL - S4 - MAJOR REPAIR - CORROSION ON LEFT AILERON NR 2 HINGE PIN BETWEEN WS 12277 TO WS 12870. REPLACED LEFT AILERON NR 2 HINGE PIN BETWEEN WS 12277 TO WS 12870 IAW A319 AMM 27-14-41.SDR USAA2010061691140Hinge Pin · corrodedSAL - S4 - MAJOR REPAIR - CORROSION ON LEFT AILERON NR 1 HINGE PIN BETWEEN WS 11664 TO WS 12277. REPLACED LEFT AILERON NR 1 HINGE PIN BETWEEN WS 11664 TO WS 12277 IAW A319 AMM 27-14-41.SDR FDEA201005261679Skin · bulgedRT OTBD AILERON UPPER SURFACE AT APPROX XOA870 FOUND BULGING. RT OTBD AILERON R & R IAW AMM 27-10-02-4, REV 10.SDR FDEA201005261678Skin · bulgedLT OTBD AILERON LOWER SKIN AT FWD SIDE APPROX XOA 910 TO XOA 945 FOUND WITH BULGING. REPAIR CARRIED OUT IAW EA NR 8-5750-140483, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 -110.SDR FDEA201005261677Skin · bulgedLT OTBD AILERON LOWER SKIN AT FWD SIDE APPROX XOA 1000 FOUND WITH BULGING. REPAIR CARRIED OUT IAW EA NR 8-5750-140483, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100-110.SDR FDEA201005261667Skin · bulgedRT OTBD AILERON UPPER SURFACE AT APPROX XOA 940 FOUND BULGING. RT OTBD AILERON R & R IAW AMM 27-10-02-4 REV 10.SDR FDEA201005261666Skin · bulgedRT OTBD AILERON UPPER SURFACE AT APPROX XOA 895 FOUND BULGING. RT OTBD AILERON R & R IAW AMM 27-10-02-4, REV 10.SDR USAA2010061691142Hinge Pin · corrodedSAL - S4 - MAJOR REPAIR - CORROSION ON LEFT AILERON NR 5 HINGE PIN BETWEEN WS 14057 TO WS 14459. REPLACED LEFT AILERON NR 5 HINGE PIN BETWEEN WS 14057 TO WS 14459 IAW A319 AMM 27-14-41.SDR C2XA10SH180Attach Bracket · wornSHV - DURING C-CHECK THE RT AILERON PCA ATTACHMENT BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA201014404Fitting · gougedDURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT AILERON PCA FITTING LUGS ON AILERON TO BE GOUGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201014403Attach Fitting · wornDURING MAINTENANCE BASE INSPECTION FOUND LEFT AILERON PCA OUTBOARD ATTACH FITTING ON AILERON HAT BUSHING MIGRATING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR USAA2010062191190Hinge Pin · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON AILERON HINGE PIN NR 5 RIGHT WING. REPLACED AILERON HINGE PIN NR 5 IAW A319 AMM 27-14-41.SDR 2010FA0000481Spar · corrodedSEVERE CORROSION ON SPAR BETWEEN HINGES AND SPAR. AIRCRAFT WAS NOT HANGARED. WATER SEEPAGE BETWEEN STEEL HINGE BRACKET AND ALUMINUM SPAR DEVELOPED TO CAUSE CORROSION TO BLISTER AROUND RIVETS FASTENING HINGE TO SPAR. THIS CONDITION WAS FOUND DURING THE FABRIC RSDR IPXA10560343Skin · puncturedINSPECTION TYPE:C4, RT WING AILERON LWR SURFACE PUNCTURED JUST INBD OF 2ND FROM OTBD STATIC WICK. RT WING AILERON LWR SURFACE WAS REPLACED IAW SRM 51-70-04 AND SRM 51-60-01-OG.SDR C2XA10SH167Attach Bracket · wornSHV - DURING C-CHECK THE LT AILERON PCA ATTACHMENT BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR UALA2010051401646Skin · damagedLIGHTNING STRIKE TO LT AILERON. INSP COMPLETE, WORKING REPAIRS, DAMAGE TO LT AILERON ACCOMPLISHING DOUBLER-SANDWICH REPAIR. WORKING WITH L/E FOR EVA. REPAIR COVERED BY SRM REPAIR. ACP REPAIR OF T/E DAMAGE ONLY. BLENDED DAMAGE IAW MT. REPAIR IS WITHIN LIMITS.SDR A6WA201040350Skin · chafedRT AILERON LOWER L/E PANEL 699CB IS CHAFED. REPAIRED CHAFED RT AILERON LOWER L/E PANEL 699CB.SDR A6WA201040349Skin · chafedRT AILERON LOWER L/E PANEL 699AB IS CHAFED. REPAIRED RT AILERON LOWER L/E PANEL 699AB IAW SRM 57-60-00, FIG 101, SHEET 1, VIEW B.SDR SIMA201013305AFitting · wornDURING MAINTENANCE BASE VISIT FOUND THE LEFT AILERON POWER CONTROL UNIT ATTACHMENT FITTING ON AILERON HAS WORN AND HAD MIGRATING HAT BUSHINGS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED POWER CONTROL UNIT FITTING IAW EO EM-27MR-112. THE AIRSDR JGVR2010F00103Attach Bracket · corroded( JGVR ) DURING A SCHEDULED A-CHECK INSPECTION, CORROSION WAS FOUND ON THE LT AILERON ACTUATOR ATTACH BRACKET. STARTED REMOVING CORROSION AND FOUND CORROSION MIGRATING BENEATH COMPOSITE LAYERS. CUSTOMER ELECTED TO REPLACE LT AILERON.SDR SWAA102564Skin · peelingDURING SCHEDULED 20Y CHECK, FOUND RT WING AILERON UPPER SURFACE OUTER PLY SKIN PEELED. REPAIRED AILERON PER SRM.SDR SIMA201011902Attach Fitting · damagedDURING MAINTENANCE BASE VISIT FOUND THE LEFT AILERON, PCA ATTACH FITTING HAS DAMAGE FROM BOLT REMOVAL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED PCA ATTACH FITTING IAW ENGINEERING ORDER EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR C2XA10SH150Bracket · damagedSHV - DURING C-CHECK LT AILERON PCA BRACKET I/B FLANGE HAT BUSHINGS MISSING AND HOUSING IS DAMAGED. MAINTENANCE REMOVED AND REPLACED LT AILERON PCA BRACKET IAW EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SWIA201024220Skin · chafedRIGHT AILERON UPPER LEADING EDGE CHAFED. (C CHECK)REPLACED AILERON UPPER SKIN.SDR A6WA201040382Skin · chafedRT AILERON L/E UPPER SURFACE IS CHAFED. REPAIR DAMAGE ON RT AILERON L/E UPPER SURFACE IAW REO 601R-57-60-013, REV NC 2000-11-20 AND REO 601R-57-60-073, REV A 2010-4-22.SDR UALA2010041601279Frame · delaminatedLEFT WING AILERON, OTBD MOST, LOWER TRAILING EDGE, HAS SKIN DELAMINATING. CONDUCTIVE FRAME IS DELAMINATING FROM LOWER SURFACE OF AILERON, REMOVED ENTIRE CONDUCTIVE FRAME. MFG NEW FRAME REF UA-EVA. ACCOMPLISHED ITEM 2 AND 3 IAW EVA 73687. REPLACED FRAME ATSDR FDEA201004121165Skin · gougedRT WING INBD AILERON, UPPER INBD EDGE IS WORN AND GOUGED. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS (ORIGINAL 0.040; REMAINING 0.022 IAW SRM 57-00-01, VOL I. REMOVED SKIN PANEL IAW SRM 51-35-01, VOL II. FABRICATED SKIN PANEL IAW DWG ARC 1316, REV "C". PESDR SIMA201010203Hinge · gougedDURING MAINTENANCE BASE VISIT FOUND THE LEFT AILERON HINGE POINT NR 2 TO BE GOUGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AILERON HINGE NR 2 IAW ENGINEERING ORDER EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR A6WA201040347Skin · chafedTOP SIDE OF LT AILERON L/T IS CHAFED. REPAIRED LT AILERON UPPER L/E SKIN IAW REO 601R-57-60-013 AND REO 601R-57-60-071.SDR SIMA201010201Bushing · missingDURING MAINTENANCE BASE VISIT FOUND THE RIGHT AILERON PCA FITTING INBOARD LUG MISSING HAT BUSHING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED AILERON PCA FITTING IAW ENGINEERING ORDER EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR ASAA1047659Panel · damagedRIGHT WING AILERON HAS MULTIPLE AREAS OF DAMAGE ON COVE PANEL LANDINGS. REPAIRED DAMAGED AREAS IAW EA 400 57EA 03176.
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