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 = '5711' 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 = '5711' 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 ABXA9701762Spar · crackedFOUND CRACKS INSIDE UPPER/LOWER FLAP SUPPORT ATTACH HOLES IN WING REAR SPAR AND BULKHEAD INSTALLATION STRUCTURE AT XRS=428. REPAIRED IAW ABX REA D857-20371MR.SDR ABXA9701746Spar Cap · crackedLEFT L/E AUX TANK IS CRACKED AT OUTBOARD AFT UPPER CORNER ON ANGLE. INSTALLED REPLACEMENT SPAR CAP IAW DC-8 SRM 53-1-0, 51-1-21 AND 51-3D.SDR AALA972012Spar · crackedTUL - FOUND CRACK IN WING CENTER SECTION REAR SPAR WEB NEAR MILL CUT FROM RBL 3 TO RBL 5, WL 187 APPROX. REPAIRED PER ESO 11697. (M)SDR 97FDEA00768Spar Chord · corrodedCORROSION (C53-224-05) WING CENTER SECTION FRONT SPAR LOWER CHORD RBL 25, BS 740. *S/D* FOUND CORROSION OUT OF LIMITS. REMOVED WING CENTER SECTION FRONT SPAR LOWER CHORD. INSTALLED NEW CHORD IAW FED-EX EA- 7-5710-36858.SDR 9721316601Spar Web · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON LEADING EDGE FORWARD SPAR WEB AT FS 1521 AT LOWER SPAR CHORD. REPAIRED PER EA 66-152528.SDR UPS97824869Rear Spar · crackedINSPECTION TYPE-C, RT WHEEL WELL SPAR AT STA 860 RBL 39 TO RBL 61 CRACKED. REPAIRED IAW DOUGLAS SERVICE REWORK DWG SRO8570009.SDR IXXA9800020Spar Cap · crackedDURING ROUTINE D-CHECK INSPECTION, A CRACK WAS FOUND ON THE LOWER SPAR CAP STRAP AT STATION XW 475. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL REPAIR FILLER AND A REPAIR ANGLE IN ACCORDANCE WITH SERVICE REWORK DRASDR 97ZZZX4754Fitting · corrodedDURING INSPECTION PER SB 977 FOUND REAR SPAR CARRY THRU LOWER FITTING (LEFT) BADLY CORRODED. REPLACED PART.SDR 97ZZZX4500Spar · crackedDURING ANNUAL INSPECTION, PERFORMED WING SPAR INSPECTION PER AMERICAN CHAMPION SL 406 FOR WOOD SPARS: AC-43-16 ALERT NR 226 MAY97: FOUND EXTENSIVE COMPRESSION CRACKS AT FRONT, REAR AT BOTTOM OF BOTH WING SPARS. AIRCRAFT USED FOR AEROBATIC FLIGHT. AD 87-18SDR 97FDEA00748Spar Chord · corrodedNR 0323 005, CORROSION (C53-224-05) WING CENTER SECTION UPPER FWD SPAR CHORD, BS 740, LBL 38-44 AND 53-57, WL 202.SDR 97FDEA00747Spar Chord · corrodedCORROSION (C53-132-02-1/2) WING CENTER SECTION LWR SPAR CHORD BS 740, LBL 32 TO 42, WL 169. *S/D* ACCESSED AREA REMOVED LOWER BS 740 CENTER TANK SPAR CHORD RBL 70.5 TO LBL 70.5, WL 169. INSPECTED FASTENER HOLES, COLD WORKED FASTENER HOLES, FLAP PEENED SKIN,SDR CALA9701437Spar Tang · crackedAFT SPAR LEFT SIDE AFT TANG CRACKED (.250) FROM BUTE DOOR ATTACH HOLE APPROXIMATELY 5 OUTBOARD OF STATION 164. CUT OUT 2 CRACK AREA. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH EC/RA 5710-01844 AND DRAWING J060271-503.SDR CALA9701428Spar Web · crackedCRACKS (.75 AND .3125) AT RT SPAR DOUBLER AND WEB VERTICAL FITTING AT TRAP PANEL. REMOVED AND INSTALLED FITTING AFTER CRACK REWORK IN ACCORDANCE WITH EA 5761-01003 AND DOUGLAS DRAWING NR 5935248.SDR CALA9701429Spar Web · crackedLEFT SPAR DOUBLER WEB CRACKED (1.25) AT TRAP PANEL VERTICAL FITTING. REPAIRED PER DOUGLAS DRAWING 5935248.SDR CALA9701426Spar Web · crackedLEFT SPAR DOUBLER WEB CRACKED AT TRAP PANEL VERTICAL FITTING. REPAIRED PER DOUGLAS DRAWING 5935248.SDR ABXA9701568Spar Cap · crackedCRACK FOUND BETWEEN TWO L/E ATTACH HOLES ON THE FWD TANG. REPAIR ACCOMPLISHED IAW SB 5775119-509 AMD ABX REA D857-20498MR.SDR TWAA9805701Spar · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK INDICATION IN RT WING REAR SPAR AT INBD FLAP HINGE CASTING LOWER INBOARD HOLE. REPAIRED PER DOUGLAS DRAWING JO60271. (M)SDR CALA9701563Spar Chord · corrodedINSPECTION FOUND RT WING REAR SPAR LOWER CHORD CORRODED ON BOTH SIDES OF NR 2 SPOILER ACTUATOR INBOARD SUPPORT LEG. THE FASTENERS WERE REMOVED, THE CORROSION WAS REMOVED AND THE FASTENERS WERE REINSTALLED IAW ECRA 5710-01849.SDR CALA9701562Spar · corrodedINSPECTION FOUND CORROSION ON LT WING REAR SPAR IN NR 3 SPOILER AREA TEN INCHES OUTBOARD OF SPOILER INBOARD MOUNT FITTING. THE FASTENERS WERE REMOVED, THE CORROSION WAS REMOVED, AND THE FASTENERS WERE REINSTALLED IAW SRM 51-21-01.SDR DHL9780773CSpar · crackedLEFT WING UPPER SURFACE REAR SPAR PREVIOUS SHEET METAL REPAIR LOCATED FORWARD OF NR 1 SPOILER PANEL ON THE OUTBOARD HINGE INBOARD SIDE IS CRACKED, BROKEN OFF BELOW THE REPAIR, THE SKIN IS ALSO CRACKED. REMOVED DAMAGED REPAIR DOUBLER AND DAMAGED REPAIR FILLER SDR CALA9701564Spar Cap · corrodedINSPECTION FOUND CORROSION ON LOWER SIDE OF LT WING UPPER SPAR CAP, AFT SPAR TWELVE INCHES OUTBOARD OF NR 2 SPOILER ACTUATOR MOUNT CASTING. THE UPPER WING PANEL WAS REMOVED, THE CORROSION WAS REMOVED AND THE PANEL WAS REINSTALLED IAW SRM 51-30-02 AND 51-10-03SDR 98ZZZX34Spar · corrodedCORROSION FOUND ON FRONT SPAR, LT WING STATIONS 32, 46, 57, 60, 62, 64, AND 81, AND RT WING STATION 32. REF: AD75-27-09 R2 AND AMDT 39-3878.SDR 98ZZZX33Spar · corrodedCORROSION FOUND ON FRONT SPART, LT WING STATIONS 32, 46, 57, 60, 62, 64, AND 81, AND RT WING STATION 32. REF: AD75-27-09 R2 AND AMDT 39-3878.SDR 98ZZZX30Spar · corrodedCORROSION REVEALED ON FRONT SPAR LT WS 32, WS 46, AND WS 81 AND RT WS 32.SDR 98ZZZX29Spar · corrodedCORROSION REVEALED ON FRONT SPAR LT WS 32, WS 46, AND WS 81 AND RT WS 32. REF: AD 75-27-09 R2 AND AMDT 39-3878.SDR ASAA9740067Spar · gougedSEA - DURING C-CHECK, GOUGES WERE FOUND ON THE FORWARD CHORD FLANGE AT RIGHT AND LEFT OUTER WING FRONT SPAR WING STATION 796.846. REPAIRED PER EA 5720-01131 AND BOEING TELEX M-7272-974829. (M)SDR ABXA9701541Spar Cap · delaminatedLEFT LEADING EDGE AUX TANK UPPER SPAR CAP DELAMINATED AND CORRODED XFS 20 AND XFS 40. INSTALLED NEW L/E UPPER SPAR CAP IAW DC-I SRM 51-1-21 AND 51-1-20D.SDR UPS97825304Spar · crackedINSPECTION TYPE-C, L/W LOWER AFT SPAR CRACKED AT STA XW 120. REMOVED 4 HYDRAULIC LINES FOM. REMOVED 2 AUX SPAR FITTINGS, INSTALLED 05, -7 AND -3 FITTINGS AND FILLER IAW DC8 SRM 57-2-6 AND REO 03831 REV A, DC8 SRM 51-1-20A, 51-3-0. REINSTALLED HYD LINES IAW SDR 97ZZZX4793Carry Thru Spar · corrodedINSPECTION FOUND CABIN OVERHEAD CARRY-THROUGH SPAR CORRODED WHERE FRESH AIR DUCT PASSES THROUGH. SUSPECT DISSIMILAR METAL CONTACT.SDR 97ZZZX4508Shims · missingDURING REPLACEMENT OF PAN UNDER WING WALK IN THE GEAR WELL, RIB WAS FOUND CRACKED. THE WING WAS REMOVED AND FOUND SEVERAL WING ATTACHMENT BOLTS CORRODED. BOLTS AND SPECIAL WASHERS NOT IN PROPER LOCATIONS PER PA28 MM. (WING ATTACH). NO SHIMS AT EITHER WING SSDR RRXA97276Spar · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO TENSION HOLES ON RIGHT UPPER WING SPAR. *S/D* THE RIGHT UPPER AUX SPAR TWO TENSION HOLES WERE SLIGHTLY CORRODED. HOLES WERE REAMED FOR CLEAN-UP AS DOCUMENTED. THESE HOLES ARE WITHIN THE BLUEPRINT TOLERASDR DL72S971953Rear Spar Web · crackedTHE WING CENTER SECTION REAR SPAR WEB IS CRACKED AT LBL 20.5. THE CRACK IS APPROX 2.5 LONG IN A CHEMMILL RADIUS JUST BELOW THE SPAR UPPER CHORD. AN ACCESS HOLE WILL BE CUT OUT AS REQUIRED TO GAIN ACCESS TO THE REAR SPAR WEB IN THE WING SECTION. THE CUTOUT ISDR 9725139616Spar Web · corrodedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LEFT WING REAR SPAR WEB LOWER CHORD AND SPLICE ANGLES AT XRS 111. REPAIRED PER EA 99-112846.SDR 97ZZZX4257Spar Cap · corrodedSEVERE CORROSION ON LOWER CENTER SECTION SPAR CAP. CORROSION WAS FOUND AFTER RT WING WAS REMOVED FOR REPAIR DURING ANNUAL INSPECTION. CORROSION CANNOT BE DETECTED WITH WING INSTALLED. SUBMITTER RECOMMENDED PANEL BE INSTALLED ON BOTTOM SKIN PANEL TO CHECK FOSDR 97FDEA00668Spar Chord · corrodedNR 0245 001 CORROSION (C53-132-02-1/2) WING CENTER SECTION UPPER REAR SPAR CHORD BS 870, RBL 70-LBL 70, WL 188. REMOVED AND REPLACED DAMAGED 870 UPPER CHORD PER FED-EX EA 7-5710-36196.SDR 9725119616Spar Web · crackedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CRACK IN RIGHT WING AFT SPAR WEB AT XRS 91. REPAIRED PER EA 99-151849.SDR 9725109616Spar Chord · corrodedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT WING SPAR LOWER CHORD AT XRS 58-189. REPAIRED PER EA 99-112839.SDR GAIA9745Rear Spar · corrodedDURING C-CHECK, INSPECTION CORROSION WAS FOUND AT LEFT WING UPPER REAR SPAR RAIL. REPAIRED IAW TRACOR COMJET FAX NR 505-97-WLD-169 DATED 9-9-97. THIS REPAIR TFSI/ASD FAA DER APPROVED. AIRCRAFT RETURNED TO SERVICE. (M)SDR UPS97824634Spar Plate · crackedINSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND REINFORCEMENT PLATE ON BOTTOM OF LOWER FRONT SPAR CRACKED AT STA XW408. FABRICATED REPAIR DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DACO SERVICE REWORK DRAWING SR08570014 AND DC8 SRM 57-1-8, 51-1-21SDR 97ZZZX4250Bolts · looseDURING 100-HOUR INSPECTION, THE CENTER SECTION WING BOLTS THAT ATTACH THE LOWER WING SPAR PLATE TO THE WING SPAR (I.E., 20 WING BOLTS) WERE ALL FOUND UNDERTORQUED BY ONE-HALF TO ONE FULL TURN. THE NAS464P5 BOLTS SHOULD BE TORQUED 100-140 INCH/POUND.SDR DHL9780706CSpar · bulgedAT C-CHECK, LT UPPER T/E REAR SPAR XRS 172.00 HAS BULGE IN T/E PANEL. REMOVED REPAIR, INSPECTED AREA, NO CORROSION AND REINSTALLED REPAIR PER SRM 51-1-21.SDR 9717076623Spar Web · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON FRONT SPAR WEB AT LOWER CHORD BETWEEN FSSI 600 AND 610. REPAIRED PER EA 66-151501.SDR 97FDEA00606Spar Chord · corrodedCORROSION (C53-132-02- 1/2) WING CENTER SECTION LOWER FRONT SPAR CHORD BS 740, RBL 10 AND RBL 26 TO 30, WL 164.SDR 97FDEA00619Spar Chord · corrodedNR 0748 027 STA-PAE - CORROSION (C57-174-01) ON BS 870 REAR SPAR UPPER CHORD RBL 20-60, LBL 10-40, WL 178. BLENDED, REMOVED CORROSION ON UPPER REAR SPAR CHORD, BS 870, RBL 20-60, LBL 10-40, WL 178. CHORD FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. RESDR 97FDEA00611Spar · corrodedCORROSION (C57-174-01) ON BS 870 REAR SPAR LOWER CHORD, LBL 40 TO 45, WL 138. *S/D* REMOVED CORROSION, BLENDED ON BS 870 REAR SPAR LOWER CHORD. FOUND CHORD TO BE OUT OF LIMITS PER FED SRM 53-10-1. REMOVED AND REPLACED SPAR CHORD PER EA NR 7-5710-36144.SDR DLL10971748Rear Spar · corrosionCORROSION WAS FOUND ON THE WING CENTER SECTION REAR SPAR WEB AT BOTH LBL AND RBL 102. THE CORROSION IS LOCATED ON THE AFT SIDE OF THE WEB AT THE SPAR UPPER CHORD ATTACHMENTS, AND JUST INBOARD OF THE AFT UPPER CENTER SECTION WING JOINT FITTINGS. THE MAX DEPTHSDR TSAA9757216Spar Chord · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION NOTED ON RT WING FRONT SPAR LOWER CHORD FORWARD HORIZONTAL FLANGE LOWER SURFACE AT FSS 317, 36S, 461, 550, 417, BY NR 4 SLAT ACTUATOR, AND BY NR 5 SLAT ACTUATOR. REPAIRED PER ECO 1803R4. AIRCRAFT RETURNED TO SERVICE.SDR AALA971631Spar Chord · corrodedTUL - FRONT SPAR LOWER CHORD ANGLE CORRODED BELOW NR 6 SLAT ACTUATOR 2.50 INCH BY 6 INCH AREA. REMOVED CORRODED SECTION OF SPAR, REPAIRED IAW BSRM 57-10-6, FIGURE 2. TST: 67,059. CYCLES, 43,852. (X)SDR DL72K971679Spar Web · crackedTHE WING CENTER SECTION REAR SPAR WEB WAS CRACKED AT APPROX RBL 20.5 AND LBL 11.5. THE CRACK AT RBL 20 IS 2.0 LONG AND A CHEM-MILLED RADIUS JUST BELOW THE SPAR UPPER CHORD. THE CRACK AT LBL 11.5 IS 1.13 LONG ALSO IN THE CHEM-MILLED RADIUS JUST BELOW THE SPARSDR CALA9701242Spar Chord · corrodedINSPECTION FOUND RT WING FORWARD SPAR LOWER CHORD PLATE CORRODED ON INNER SURFACE BETWEEN FS 672 AND 685. THE CORRODED AREA WAS CUT OUT AND A NEW SECTION WAS SPLICED IN IAW ECRA 5710-01836.
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