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 UPS98226848Spar · corrodedINSPECTION TYPE:C R/W FRONT SPAR LOWER CHORD IS CORRODED AT FSS 438 AND FS 446. REMOVED CORROSION OUT OF LIMITS AND REPAIRED IAW ER NR 98-2449.SDR UPS98226847Spar Chord · corrosionINSPECTION TYPE:C R/W UPPER F/SPAR CHORD SHOW SIGNS OF CORROSION AT FSS 398.0, 497.0, 513.5, 521.5, 730.02, 737.0. REMOVE CORROSION FOUND OUT OF LIMITS AND REPLACE SPAR CHORD IAW 98-2421.SDR DLL13981076Spar Cap · crackedOVERSIZED FASTENER HOLES WERE FOUND IN THE VERTICAL FLANGE OF THE LT WING LWR REAR SPAR CAP AT APPROX IWS 258. THE FASTENER FINAL DIAMETER WAS 0.3428. REPAIRED PER ERA 331709-14AD.SDR CALA9800893Spar · crackedINSPECTION FOUND A 1.5 INCH CRACK ON OUTBOARD SIDE AND A 1.5 INCH CRACK ON INBOARD DOUBLER OF NR 8 SLAT INBOARD ACTUATOR MOUNT AREA OF FRONT SPAR. THE INBOARD DOUBLER WAS REMOVED AND REPLACED AND THE OUTBOARD CRACK WAS STOP DRILLED IAW SRM 51-10-1.SDR AU980548Spar · cracked(AUS) WING MAIN SPAR CRACKED IN TWO PLACES. OUTBOARD CRACK LENGTH 82.55 MM (3.25 INCH). INBOARD CRACK LENGTH 57.15 MM (2.25 INCH). FOUND DURING INSPECTION IAW SA226 MANUAL ST-UN-M002.SDR 98ZZZM479Spar Web · corrodedDURING C-CHECK INSPECTION DISCOVERED CORROSION ON THE CENTER TANK REAR SPAR WEB AT STATION 1241, BL 0.0. REPAIRED BY CUTTING OUT A SECTION OF PRESSURE WEB ANGLE BETWEEN LBL 5 AND RBL 15, BLENDING OUT CORROSION COMMON TO THE REAR SPAR WEB, HFEC INSPECTING AREASDR DHL9870627CSpar · crackedAT C-CHECK, LEFT WING FRONT SPAR WS 115 LOWER END OF VERTICAL ANGLE CRACKED. STOP DRILLED END OF CRACK, HFEC, FABRICATED ANGLE REPAIR, 6 X 2 PER SRM 51-40-3. N/R 1648.SDR 98ZZZX2143Spar · crackedDURING ANNUAL INSPECTION, A CRACK OF APPROXIMATELY .50 INCH WAS FOUND ON THE FORWARD VERTICAL FACE OF THE TOP HAT SECTION FORMING THE SPAR ASSY 1 INCH INBOARD OF THE OUTER EDGE AND ADJACENT BUT NOT RUNNING TO THE LT MAIN PLANE REAR ATTACH BOLT. CAUSE UNKNOWN SDR UPS98226733Spar Chord · crackedINSPECTION TYPE:C, CRACK INDICATION NOTED ON RT WING UPPER REAR CHORD FROM WS 462 TO WS 464 (APPROX). CRACK INDICATION WAS CORROSION WS 457-470. REPAIRED PER SRM 57-10-6 FIG 3 AND DWG 65C19647 CAT II REPAIR.SDR TSAA9857263Spar · corrodedFOUND CORROSION AT WBL 318 ON RT WING FRONT SPAR LOWER CHORD HORIZONTAL FLANGE LOWER SURFACE. REPAIRED CORROSION PER ECO 1803 R4. AIRCRAFT RETURNED TO SERVICE. (M)SDR CALA9800847Spar Cap · crackedLEFT WING LOWER SPAR CAP CRACKED 2.35 AT STA XRS 161.7. PERFORMED REPAIR PER TASK CARD 08-5700-1-0025 OP 12.SDR CALA9800846Spar Cap · crackedA 1 INCH CRACK AROUND I/B HOLE ON RIGHT WING LOWER SPAR CAP. REPAIRED PER TASK CARD 08-5710-1-0020 OP 7.SDR 98ZZZX2051Spar · crackedINSPECTION FOUND CRACKED REAR STUB SPAR. NEEDS C/W MOONEY SB M20-217.SDR MWEA98592Spar Cap · corrosionFOUND CORROSION ON RIGHT WING FRONT SPAR TEE CAP SPLICE PLATE INBOARD OF NUMBER 1 SLAT DRIVE TRACK. MAINTENANCE FABRICATED AND INSTALLED NEW STRAP.SDR HALA9800112Spar Cap · crackedLAX - FLT 09 - RIGHT WING CRACKED N THE REAR SPAR CAP WEB NEAR XORS 433/402. INSTALLED FUEL TANK REPAIR DOUBLER PER ES07349, DATED 5-7-98. (X)SDR UPS98426920Spar · corrodedINSPECTION TYPE-C, CORROSION ON INNER SPAR SKIN EXTENSION RT WING STATION 1320 JUST O/B OF JACKING POINT. REMOVED CORROSION.SDR SWAA980754Spar Chord · crackedDURING SCHEDULED D-CHECK, FOUND CRACK INDICATION ON TOP MOST INBOARD FASTENER HOLE COMMON TO MAIN LANDING GEAR BEAM FITTING (RIGHT SIDE) RSS 224 (CRACK ON SPAR CHORD UPPER). REPAIRED PER BOEING SRM.SDR 98FDEA00328Spar Chord · corrodedCORROSION ON RT WING REAR SPAR LOWER CHORD, WS 207. CORROSION WAS REMOVED AREA APPROX 7 WIDE, HEIGHT .625, .25 DEPTH. REPAIRED PER SRM 57-10-6, FIG 2, SHEET 4 AREA WAS NOT CHECKED AND NO CRACKS FOUND.SDR P5CA9800931Spar Web · corrodedLEVEL 1 CORROSION FOUND ON AFT SPAR LWR WEB AT ATTACHMENT OF BONDING LEAD OF NR 2 AFT BOOST PUMP. REPAIRED CORROSION PER SRM 51-10-01 AND SRM 51-10-02.SDR P5CA9800970Spar Chord · corrodedLEVEL 1 CORROSION ON RT WING LOWER CHORD SURFACE AT FSS 822-840. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.SDR DLL10980896Spar Web · crackedWING LT, REAR SPAR WEB, OWS 77 LOWER CAP ATTACHMENT, REPAIR FOR WEB CRACK. THE LT WING REAR SPAR WEB WAS FOUND WITH A .50 LONG CRACK EMANATING FROM A FASTENER HOLE ATTACHING THE WEB TO THE LOWER SPAR CAP AT OWS 77. THE WEB CRACK WAS ROUTED OUT AND AN ALUMINSDR MWEA98497Spar Cap · corrodedRIGHT WING LEADING EDGE STATION 330 FORWARD LOWER SPAR HAS CORROSION. MTC REMOVED CORROSION AND INSTALLED REPAIR STRAP USING APPROVED DATA.SDR MWEA98496Spar Cap · corrodedRIGHT WING LEADING EDGE STATION 200 FORWARD SPAR LOWER CAP HAS A PREVIOUS REPAIR ON THE FORWARD SIDE OF THE CAP. REMOVED PREVIOUS REPAIR BLENDED CORROSION INSTALLED REPAIR STRAPS USING APPROVED DATA.SDR MWEA98492Spar · corrosionLT WING STATION XRS 360 LOWER AFT SPAR HAS INTERGRANULAR CORROSION ON UPPER SIDE OF LOWER SPAR CAP. MTC REMOVED CORROSION AND REPAIRED SPAR USING APPROVED DATA.SDR CA980421011Web · cracked(CAN) FAIRCHILD RECENTLY REVISED ITS AIRFRAME INSPECTION MANUAL TO INCLUDE A DETAILED INSPECTION OF THE WING CENTER SPAR INNER WEB. CRACKS FOUND ON THE WEB. TWO OTHER AIRCRAFT WITH SIMILAR PROBLEM.SDR CA980421010Web · cracked(CAN) FAIRCHILD RECENTLY REVISED ITS AIRFRAME INSPECTION MANUAL TO INCLUDE A DETAILED INSPECTION OF THE WING CENTER SPAR INNER WEB. CRACKS HAVE BEEN FOUND ON THE WEB. TWO OTHER AIRCRAFT WITH SIMILAR FINDINGS.SDR CA980421009Spar Web · cracked(CAN) FAIRCHILD RECENTLY REVISED ITS AIRFRAME INSPECTION MANUAL TO INCLUDE A DETAILED INSPECTION OF THE WING CENTER SPAR INNER WEB. INSPECTION FOUND CRACKING ON THREE DIFFERENT AIRCRAFT. PART TC: 39,582. ACFT TT: 25,974 HOURS.SDR MWEA98433Spar · damagedTHE RIGHT WING FORWARD LOWER SPAR CAP HAS AN UNDOCUMENTED REPAIR. MTC REPAIRED SPAR CAP USING APPROVED DATA.SDR EIAA980164Spar · corrodedMZJ - DURING 'C4' CHECK INSPECTION, LEFT WING OLES 1481, FRONT SPAR LOWER RABBET STRUCTURE HAS EXFOLIATION PROGRESS UNDER FRONT SPAR STIFFENER FITTING. REMOVED CORROSION AND REPAIRED FRONT SPAR LOWER CHORD PER ECRA 481-54-121-2. (M)SDR 9806296608Spar Chord · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON LOWER CHORD OF FRONT SPAR FS 1471. REPAIRED PER EA 66-153315.SDR RRXA98173Spar Cap · crackedDURING A MAINTENANCE VISIT FOUND RIGHT WING, FORWARD SPAR CAP LOWER CRACKED AT XFS=519. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04464.SDR TWAA9809309Spar · crackedMCI - DURING OP 16 MAINTENANCE CHECK FOUND ON RT WING HOLE 43 INDICATING CRACK WITH HFEC, RT WING LOWER REAR SPAR STA XRS 154. REPAIRED PER SERVICE REWORK DRAWING J060173 AND TWA STD PRACTICES. (X)SDR TWAA9809308Spar · crackedMCI - DURING OP 16 MAINTENANCE CHECK FOUND ON RT WING HOLE 71 INDICATING CRACKED, LOWER REAR SPAR RT XRS 200. REPAIRED PER SERVICE REWORK DRAWING J060173 AND TWA STD PRACTICES. (X)SDR TWAA9807305Spar · crackedMCI - DURING OP16 MAINTENANCE CHECK, FOUND HOLE 104 INDICATING CRACK RT WING LOWER SPAR STATION XRS 268. REPAIRED PER SERVICE REWORK DRAWING J060173 AND TWA STD PRACTICES. (M)SDR TWAA9807304Spar Cap · crackedMCI - DURING OP15 MAINTENANCE CHECK, FOUND STATION XRS 164 INSIDE TANK FWD FACE OF LOWER SPAR CAP, VERTICAL LEG WITH CRACK EXTENDING INTO LOWER RADIUS, BELOW INBOARD FLAP BARREL NUT ATTACH POINT. INSTALLED NEW SPAR CAP AND SPLICE PER DWG J060165 AND STD PROCESDR TWAA9806915Spar Cap · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LEFT WING STATION XRS 164 INSIDE TANK, FWD FACE OF LOWER SPAR CAP, VERTICAL LEG HAD CRACK EXTENDING INTO LOWER RADIUS BELOW INBOARD FLAP BARREL NUT ATTACH POINT. INSTALLED NEW SPAR CAP AND SPLICE PER DWG JO60165 ANDSDR AU980327Spar · corroded(AUS) LT AND RT WING SPARS P/N 68-1.4001 AND P/N 68-1.4002 CONTAINED INTERGRANULAR AND EXFOLIATION CORROSION IN THE WEBS LOCATED BEHIND THE ENGINE FIREWALLS.SDR 9806249974Spar · corrodedDURING M-CHECK, FOUND CORROSION ON REAR SPAR UPPER CAP AND ADJOINING WING SKIN AT WS 691. REPAIRED PER EA 99-154768.SDR AU980353Spar · corroded(AUS) WING SPAR ASSEMBLY CONTAINED DEEP PITTING CORROSION ON THE LOWER WING ATTACHMENT LUG. CAUSED BY A BROKEN AND RUSTY SCAT HOSE WIRE RESTING ON THE SPAR.SDR 98ZZZX2501Spar Cap · misdrilledDURING C-CHECK, INSPECTION, DISCOVERED NUMEROUS OVERSIZE FASTENER HOLES IN THE REAR LOWER RIGHT HAND SPAR CAP FORWARD LOWER FLANGE AT XRS111.5 (PN 5911305-502) AND LOWER AFT WING SKIN/STRINGERS (P/N 3919224-2). REPAIRED BY OVERSIZE FASTENER HOLES, FABRICATINGSDR 98ZZZX2500Spar Cap · crackedDURING C-CHECK INSPECTION, DISCOVERED A CRACK ON THE FRONT SPAR UPPER CAP (PN 5912124-1) OF THE LEFT HAND WING FLAP LOCATED BETWEEN XF229.00 AND SF235.00. REPAIRED BY TRIMMING OUT THE CRACK, NDT INSPECTED, FABRICATED AND INSTALLED NESTED STEEL ANGLE WITH HILOSDR TWAA9807318Spar Cap · crackedMCI - DURING OP 16 MAINTENANCE CEHCK, FOUND RT WING TE UPPER REAR SPAR CAP CRACKED AT INBOARD FLAP HINGE UPPER ATTACH HOLES. STOP DRILLED CRACK, REPAIRED PER DAC DWG J060271 AND STD PRACTICES. (M)SDR TWAA9807204Spar Cap · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND RT WING TE UPPER REAR SPAR CAP CRACKED AT INBOARD FLAP HINGE UPPER ATTACH HOLES. STOP DRILLED CRACK. REPAIRED PER DAC DWG J060271 AND STANDARD PRACTICES. (M)SDR AU981213Spar · corroded(AUS) SUBMITTER STATED INCORRECT STEEL WASHERS (CORRECT TYPE ALUMINIUM) USED UNDER THE LEFT WING ATTACHMENT NUTS CAUSED CORROSION OF THE WING SPAR. AIRCRAFT IS AN AMPHIBIAN AND OPERATES IN A SALT LADEN ENVIRONMENT. 1,301.SDR TWAA9809406Spar · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND RT WING TRAILING EDGE INBD FLAP REAR SPAR, INBD FLAP CASTING MOUNT HOLE LOWER INBD HOLE, WITH CRACK EXTENDING INTO RADIUS ON FWD SIDE OF FUEL TANK. SPLICED SECTION OF LOWER SPAR FROM STA XRS 111.510 TO XRS 195.210, SDR CALA9800542Spar Web · crackedINSPECTION FOUND A 4 INCH CRACK IN CENTER WING SECTION AT REAR SPAR WEB UPPER RADIUS ABOVE PRODUCTION PANEL FROM RBL 0 TO RBL 4. THE AREA WAS REPAIRED IAW EA SA004-5710-01843, DRAWING 65C37620, AND SERVICE BULLETIN 727-57A0182.SDR RRXA98198Spar · gougedDURING A MAINTENANCE VISIT, FOUND LEFT WING, UPPER AFT SPAR GOUGED AT XRS=373, DAMAGED BEYOND LIMITATIONS IAW DC-8 SRM. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E04-R11. UNDER ACMI WO EO47 NR N0004.SDR 98ZZZX1293Spar · corrodedDURING C/W AD 96-24-17R (AMEND NR 39-10229 EFF 1-27-97), INTERGRANULAR CORROSION WAS FOUND ON THE LOWER WEB OF THE RT REAR SPAR AFT FACE APPROXIMATELY 17 INCHES FROM THE WING ATTACH POINT. THE CORROSION HAD CAUSED A BULGE IN THE MATERIAL AND WAS APPROXIMATELYSDR 98ZZZX1172Spar Cap · corrodedDURING WING INSPECTION, FOUND EVERY WHERE THAT SOUNDPROOF INSULATION COMES IN CONTACT WITH THE FERROUS AFT SPAR CAP, THAT CORROSION SETS IN DUE TO THE MOISTURE THAT THE INSULATION HOLDS.SDR AU980332Plate · corroded(AUS) WING SPAR PLATE CONTAINED EXFOLIATION CORROSION BETWEEN SPAR FLANGE AND SPAR PLATE. LENGTH OF CORROSION 35MM (1.37 INCH).
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