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 KCSA081513Spar · corrodedCORROSION ON FITTING AT WS 530 ON AFT SPAR WEB. (K)SDR DL757081276Rib · damagedRT WING RIB STA 18 HAS 1 EA ELONGATED HOLE AT STR 9.5 FWD OUTBOARD HOLE ON FWD LEG OF STR CHANNEL. REWORKED DAMAGED HOLE TO A FINAL SIZE OF .250, EDGE MARGIN OF .450 IAW 757 SRM 51-40-05 FIG 2. INSTALLED 1 EA FASTENER ON STRINGER CLIP U9.5 RT WING RIB 18 PERSDR DL757081249Spar · gougedDURING WINGLET MOD, THE LT WING REAR SPAR LOWER CHORD WAS DAMAGED BY TOOLING. A GOUGE WAS BLENDED SMOOTH AND TREATED FOR CORROSION PROTECTION. THE BLEND AND TREATMENT WAS APPROVED BY BOEING.SDR 08FDEA04121Spar · corrodedRIGHT WING INBD T/E AT THE MAIN LANDING GEAR SUPPORT, LOWER FWD AUX SPAR SPLICE HAS CORROSION. REPLACED SPLICES IAW DWG ARB 0621 AT THE RIGHT WING INBD TRAILING EDGE AT THE MLG LOWER FWD & AFT SPAR SPLICES.SDR 08FDEA04071Spar Cap · damagedRIGHT WING REAR SPAR UPPER CAP AT STA XORS 676, 875, AND 887 FOUND HOLE ELONGATED. CARRIED OUT REPAIR AS PER EA NR 1-5710-123124. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 08FDEA04038Frame · crackedRT WING, I/B AILERON LOWER T/E PANEL FRAME CRACKED WITH MISSING ATTACH FASTENER AT AFT END OF FRAME 10 INCH O/B FROM I/B END OF AILERON REMOVED DAMAGED PANEL FRAME REF SRM 51-30-2. VERIFIED MATERIAL OF FRAME TO BE BAC1506-1625 7075-T6. FABRICATED REPLACEMESDR ABXA200810160251Spar · corrodedLEFT WING LOWER L/E WING SPAR WAS CORRODED I/B OF TAI DUCT, APPROXIMATELY WS 433. WING SPAR WAS REPAIRED IAW REA B657-57753.SDR 08FDEA04407Spar · crackedRT WING RIB 5 NEXT CENTER SPAR FWD ZONE FOUND WITH CRACK (RIB 5 TO TOP SKIN). RIB 5 REPAIRED IAW EA 6-5710-121705.SDR DHLA2008745609Spar · corrodedRT WING SPAR AT WBL 164.5 LOWER CHORD WITH CORROSION. REPAIRED RIGHT WING FRONT SPAR LOWER CHORD IAW B727 SRM 57-10-6 FIG 2 DETAIL II.SDR 2008UALA05667Stiffener · crackedSTIFFENER IN NOSE WHEEL WELL LEFT SIDE IS CRACKED ON THE RISER. REPAIRED STIFFENER PER SRM 57-11-16.SDR DL757081261Spar · damagedLT WING REAR SPAR LWR T-CAP HAS TOOLING MARK AT RIB STA 23. COMPLETED REPAIR PER ERA 470321-14 REV O.SDR 08FDEA03753Spar · crackedRIGHT WING, TRAILING EDGE REAR SPAR AT STA XORS = 197.20 LANDING GEAR BRACE SUPPORT ROD LOWER FITTING 02 EACH CRACK FOUND NEAR FASTENER. RIGHT WING TRAILING EDGE REAR SPAR AT STA XORS = 197.20 LANDING GEAR BRACE SUPPORT ROD LOWER FITTING REMOVED AND REPLASDR 2008FA0000658Spar · crackedLT WING SPAR CRACKED IN THE AREA OF WHERE THE PIVOT BLOCK IS INSTALLED. (K)SDR 08FDEA03588Spar Cap · damagedRIGHT WING, TRAILING EDGE SPAR UPPER CAP AT STA XORS 675 FOUND 01 EACH FASTENER HOLE ELONGATED. REPAIR CARRIED OUT AS PER E.A. 1-5710-122430, THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA03587Spar Cap · damagedRIGHT WING, TRAILING EDGE REAR SPAR UPPER CAP AT STA XORS 746 FOUND 01 EACH FOUND FASTENER HOLE ELONGATED. REPAIRED AS PER E.A. 1-5710-122430, THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA03586Spar Cap · damagedRIGHT WING, TRAILING EDGE REAR SPAR UPPER CAP AT STA XORS 897 FOUND 01 EACH FASTENER HOLE ELONGATED. FASTENER HOLE REPAIR CARRIED OUT AS PER EA 1-5710-122430, THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA03577Spar · corrodedCORROSION ON RIGHT WING FRONT LOWER SPAR CHORD AT FSS 514. REMOVED CORROSION, VERIFIED REMAINING MATERIAL TO BE 0.123", HFEC INSPECTED ALL OPEN HOLES WITH NO DEFECTS NOTED, PERFORMED ULTRASONIC INSPECTION OF BLENDED AREAS, NO DEFECTS NOTED, SPOT FACED FASTENESDR 08FDEA03561Spar · corrodedLT AFT MAIN TANK BOOST PUMP HEAVY CORROSION ON SPAR. CORROSION REMOVED AND AREA TREATED IAW FEDEX EA NR F-5710-124306. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.SDR 08FDEA03483Spar · corrodedFOUND CORROSION ON LT MLG FWD PICK UP FITTING AREA ON REAR SPAR (HOLE NR 8, NR 13). REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW RAS/BAE/1006539/2008 ISS A, APPROVED BY EA 6-5751-1210094.SDR COEA0804703Spar · puncturedMAJOR REPAIR: LT WING FRONT SPAR WEB HAS A PUNCTURE HOLE AT WS 11560. DISCOVERED DURING MAINTENANCE AFTER TAXI INCIDENT. (S) CUT OUT THE DAMAGED AREA ON THE WING FRONT SPAR WEB PLATE. FABRICATED AND INSTALLED A REPAIR PLATE WITH FILLERS. ISSUED FIELD ENGSDR FDEA200808073298Former · crackedLT WING L/E INT FOUND CRACK ON FORMER. REPAIRED AREA IAW SRM 57-00-01 FIG 10 VOL I.SDR 08FDEA03298Former · crackedLT WING L/E INT FOUND CRACK ON FORMER.SDR COEA0806816Spar · corrodedRT WING FRONT SPAR UPPER FLANGE ANGLE IS SHOWING WEAR MARKS. RT WING FRONT SPAR TOP FLANGE HAS FRETTING DAMAGE WHERE THE ANTI CHAFE STRIP IS WORN THROUGH. REPAIRED BY BLENDING DAMAGED AREA AND LEAVING AS IS. (S)SDR 08FDEA03215Spar · corrodedUNDOCUMENTED BLEND REPAIR FOUND ON THE AFT SIDE OF THE LT WING REAR SPAR WEB AT RSS 183. EVALUATE AND RECTIFY. LEFT WING REAR SPAR WEB CORROSION BLEND REPAIR CARRIED OUT IAW EA F-5710-118827 DATED MAY 24 2008. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-02-100.SDR UPS08552955Plate · crackedINSPECTION TYPE-C2, LT WING T/E AFT LOWER SPAR WIGGLE PLATE BROKEN FWD OF NR 5 SPOILER AT RSS342. REMOVED AND REPLACED WIGGLE PLATE IAW SRM 51-40-02.SDR 08FDEA03188Spar · damagedRIGHT WING, DURING ACCOMPLISHMENT OF EA NR 1-5710-105596C PART 2, REAR SPAR LOWER CHORD FORWARD AND AFT TENSION TIES AT STA XORS 1088 FOUND FASTENER HOLE ELONGATED. ELONGATED HOLE AT REAR SPAR LOWER CHORD FORWARD AND AFT TENSION TIES AT STA XORS 1088. REPAIRSDR 08FDEA03107Spar Cap · damagedLEFT WING, UPPER SPAR CAP FASTENER HOLE AT STA XORS 878 FOUND ELONGATED. LEFT WING UPPER SPAR CAP STA XORS 878 ELONGATED HOLE REPAIRED AS PER FEDEX EA NR 1-5710-124328, TITLE: WINGS BASIC WING STRUCTURE, LEFT WING UPPER SPAR STA XORS = 878, ELONGATED HOLE REPSDR UPS08852998Spar · crackedINSPECTION TYPE-C2, POSSIBLE CRACK AT CENTER SPAR WEB FLANGE JUST IB XRS 358 NR 4 MAIN. REMOVED DAMAGE AND FABBED AND INSTALLED REPAIR IAW SRM., 57-2-0, 51-1- 8, 51-1-21.SDR UPS08852903Spar Cap · crackedINSPECTION TYPE-C2, CRACK AT CENTER SPAR CAP WEB FLANGE JUST IB XRS255 NR MAIN. STOP DRILLED CRACK , FABBED AND INSTALLED REPAIR DOUBLER IAW. SRM., 51 -1-8, 57-2-0 FIG. 2, 51-1-20D.SDR KCSA081308Frame · damagedFOUND FRAME WEB DAMAGED APPROX.20" FWD OF I/B AILERON @WBL-455 (B)SDR KCSA081306Spar Cap · corrodedR/H WING REAR SPAR TOP CHORD IS CORRODED ON UPPER SURFACE AT WBL 460 (B)SDR UPS08852792Spar · damagedINSPECTION TYPE-C2, RT WING FRONT SPAR T CAP HAS DOUBLE DRILLED HOLE XFS 92.5. CLEANED HOLE AND INSTALLED BUSHING IAW SRM, EO DC8-5710-29984-A, 51-1- 8, 51-1-24.SDR UPS08M52957Spar Cap · corrodedINSPECTION TYPE-1C, LT WING LWR FWD SPAR CAP XORS 799 HAS EXFOLIATED CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS, CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM VOL 1 57-10-00 FIG.45.SDR CA080806017Spar · corroded(CAN) PART FOUND CORODED AT SPAR ATTACHMENT BOLT HOLE.SDR CA080806016Spar · corroded(CAN) PART FOUND CORRODED AT SPAR ATTACHMENT BOLT HOLE.SDR 08FDEA02428Spar · corrodedPANEL JUST AFT OF RT WING AFT SPAR LOWER CHORD IS CORRODED FABRICATED NEW PANEL FROM JUST AFT OF RT WING SPAR LOWER CHORD REF. BOEING DWG 65-26797-3, TREATED AND PRIMED AND PAINTED REF SRM 51-10-2 PG 1-7, MM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAISDR 08FDEA02322Spar · crackedFOUND CRACKED FASTENER HOLE IN CENTER SPAR WEB C 44. REPAIR PERFORMED BY CUT OUT THE DOUBLER, ROTOTEST FOR CRACK FREE CONDITION AND REAM UP UNTIL CRACK REMOVAL IAW RAS 70507029/021/2008 ISS A, APPROVED BY EA 6-5710-120043.SDR IXX2008F00038Stiffener · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING AUXILIARY SPARS STIFFENER CORRODED AT STATION XW 33.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED STIFFENER. FABRICATED STIFFENER. CLEANED, TREATED AND PRIMED AREA AND STIFFENER. INSTALLED SDR USAA920081306Stiffener · crackedCLT - C22 - MAJOR REPAIR - CENTER WING REAR SPAR VERTICAL STIFFENER CRACKED. REPLACED CENTER WING REAR SPAR VERTICAL STIFFENER IAW B737 SRM 51-40-03. (S)SDR DHL2008764532Spar · crackedWHILE AT C CHECK, RT WING REAR SPAR J BEAM CRACKED WBL 126. FABRICATED AND REMOVED AND REPLACED IAW BOEING DWG 65-21655 AND ASTAR EC-00911-001.SDR DHL2008764531Spar · crackedWHILE AT C CHECK, LT WING REAR SPAR J BEAM CRACKED INDICATION WBL126. FABRICATED AND REMOVED AND REPLACED IAW BOEING DWG 65-21655 AND ASTAR EC-00910-001 MATERIAL BAC 1506-860 7075T6 DIM 81 INCH BY 5 1/2 INCH PO NR 815922.SDR ASAA0843140Spar · crackedBS 663.75 WING CENTER SECTION REAR SPAR LOWER RIGHT WEB (COMPOSITE PANEL) CRACKED. WING CENTER SECTION REAR SPAR AT BS 663.75 LOWER RIGHT WEB CRACK REPAIRED PER SRM 51 70 04 REPAIR NR 10.SDR UPS08652337Stiffener · crackedINSPECTION TYPE:N/A LEFT WING LES 665 FRONT SPAR STIFFENER UPPER AREA FOUND CRACK. CRACK LENGTH .5 INCH APPROX . LEFT WING LES 665 FRONT SPAR STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.SDR UPS08652336Stiffener · crackedINSPECTION TYPE:N/A RIGHT WING LES 665 FRONT SPAR STIFFENER UPPER AREA FOUND CRACK. CRACK LENGTH .5 INCH APPROX. RIGHT WING LES 665 FRONT SPAR STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.SDR 2008FA0000321Spar Cap · crackedTHE CRACK EMANATES FROM THE 5TH RIVET OUTBOARD OF THE LOWER FORWARD WING BOLT FITTING, (4TH RIVET FROM END OF SPAR CAP)IN THE REAR ROW OF RIVETS, & EXTENDS TO THE TRAILING EDGE OF CAP. THE A/C PASSED 2-400 HR WING SIRM INSPECTIONS. THE CRACK WAS DETECTED AT THSDR 2008FA0000326Spar Cap · crackedTHE CRACK EMANATES FROM THE 5TH RIVET OUTBOARD OF THE LOWER FORWARD WING BOLT FITTING, 4TH RIVET FROM END OF SPAR CAP, IN THE FRONT ROW OF RIVETS, AND EXTENDS TO THE LEADING EDGE OF CAP. THE A/C PASSED 2-400 HOUR WING SIRM INSPECTIONS. 181 HRS INTO NEXT INTESDR DHL2008807506Frame · crackedLT WING CTR L/E FORMER CRACKED 0.500" STA XW 454.000. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLERS (AL7075T6 0.040") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER AND AREA IAW SRM 51-1-8B. INSTALLSDR UPS08852252Frame · crackedINSPECTION TYPE:C3 RT WING UPPER SURFACE NR 4 STUBWING INBD UPPER FRAME CRACKED, GOUGED AND CHAFED. REPAIRED RT NR 4 STUBWING INBD UPPER FRAME IAW SRM 51-01-20D, SRM 51-01 -21, SRM 57-02-00-0 FIG 002 AND DWG 5769525.SDR FE5F200800001Spar · corrodedFOUND LT WING REAR SPAR HAS CORROSION MARKS AT STA 367-361 C (EO) (L-5.875 IN,W-0.875 IN,D-0.125 IN).SDR UPS08852253Frame · crackedINSPECTION TYPE:C3 LT WING CENTER LE 3 INCH CRACK IN FRAME ABOVE PNEUMATIC DUCT XFS 410. REPAIRED LT WING CENTER LE AND FABRICATED INTERCOSTAL AND INSTALLED AT XFS 410 IAW DWG 57-69-589, SRM 51-01-21 AND SRM 51-01-20D.
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