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 = '5700' 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 = '5700' 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 JJBA20230908002Unknown · unknownLH WING FFS5 CASING ALUMINUM FERRULE CORRODED AND FFS 1 INNER SHAFT BENDED AND RH WING FFS 1 CASING ALUMINUM FERRULE CORRODED. LH WING FFS 5 REPLACED AND TESTED SERVICEABLESDR DALA2023082806943Unknown · unknownSHIP 3278 SLAT 3 LEADING EDGE AREA RH WING DAMAGE. CORRECTIVE ACTION: INSPECTED OK FOR SERVICE. PUT ON REPEAT MONITOR. (2936615)SDR CALA2023082802641Screw · missingPDA 2 2 SCREWS MISSING DURING #2 SERVICE CHECK. LEFT WING PANEL SCREWS MISSING PICTURE ADDED REPLACED MISSING SCREWS AS REQUIRED. OK TO CONTINUE.SDR FDEA202308241486Skin · noneAGING AIRCRAFT - EXISTING REPAIR DOUBLER FOUND ON RIGHT HAND WING FIXED LEADING EDGE UPPER SURFACE AT STATION XIS 247. EXISTING REPAIR DOUBLER ON RIGHT HAND WING FIXED LEADING EDGE UPPER SURFACE AT STATION XIS 247 EVALUATED AND FOUND REPAIR DOUBLER NOT IN SDR IPXA202308230001Unknown · unknown*** SDR FILED OPEN *** FAULT: LEFT WING FIXED LEADING EDGE HAS CRACK BEHIND SLAT#4 OUTBOARD ENDSDR BAGA202308210005Support Bracket · crackedRUDDER PEDAL DAMPER BRACKET CRACKED. PERMANENT REPAIR (BY REPLACEMENT) OF RUDDER PEDAL DAMPER SUPPORT (P/N 170-08554-401)SDR P5CA2023072200037Unknown · unknownREFER EO 1957A593 PART 1 SB 747-57-2369 REV 1 NO.1 FLAP TRACK ACTUATOR FRAME EXISTING REPAIR MODIFICATION(<P>ACTUATOR FRAME MODIFICATION CARRIED OUT AS PER ATLAS AIR EO 1957A593 REV 3 PART 1 AND REPAIRED AS PER RI NO: RI-57-50-16381 REV A</P>)SDR P5CA2023072200038Unknown · unknownLHW NO. 1E VC FLAP FWD BULKHEAD FOUND DEFORMED ( FWD L/E D BEAM AFT B/HEAD WEB STIFFENER DEFORMED )(<P>B/HEAD STIFFENER DEFORM AREA REPAIRED AS PER RI NO. RI-57-41-16375 REV A</P>)SDR P5CA2023072200039Unknown · unknownRHW FIXED L/E D BEAM AFT B/HEAD FOUND BROKEN(<P>B/HEAD BROKEN AREA REPAIRED AS PER RI NO : RI-57-41-16382 REV A</P>)SDR P5CA2023072200040Stiffener · unknownRHW WING FRONT SPAR ILES 487 ( AFT OF 14 K / FLAP ) STIFFENER FOUND CRACK(<P>CRACK STIFFENER REPLACED AS PER SRM 51-10-02, NEW STIFFENER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW STIFFENER INSTALLED AS PER SRM 51-40-02 ( REV 40 DATE 2 JUN 2023 )</P>)SDR P5CA2023072200041Stiffener · unknownLHW L/E FRONT SPAR ILES 470 ( AFT OF 12 K/FLAP ) STIFFENER LWR FOUND BROKEN.(<P>BROKEN STIFFENER REPLACED AS PER SRM 51-10-02, NEW STIFFENER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW STIFFENER INSTALLED AS PER SRM 51-40-02 ( SRM REV 40 DATE 20 JUN 2023 )</SDR P5CA2023072200042Unknown · unknownLHW L/E CAVITY ILES 540 D BEAM AFT BULKHEAD FOUND CRACK(<P>B/HEAD CRACK AREA REPAIRED AS PER RI NO : RI-57-41-16383 REV A</P>)SDR P5CA2023072200043Unknown · unknownLHW WING TIP I/B UPPER AFT EDGE STRAP FOUND BURN MARK(<P>BURN MARK AREA REPAIRED AS PER RI NO: RI-57-30-16423 REV A</P>)SDR P5CA2023072200044Unknown · unknownLHW I/B L/E ILES 410 'V' SUPPORT ROD UPPER ATT. BRACKET FOUND ELONGATED ( NO.5 AND 6 ).(<P>NO.6 BRACE UPPER (2EA) FASTENER HOLES AND UPPER ATT BRACKET O/B (2EA) FASTENER HOLES REPAIRED AS PER RI NO : RI-57-41-16380 REV A</P>)SDR P5CA2023072200045Unknown · unknownLHW FIXED L/E OLES 530 'D' BEAM FOUND CRACK(<P>D BEAM B/HEAD CRACK AREA REPAIRED AS PER RI NO: RI-57-41-16369 REV A</P>)SDR P5CA2023072200046Unknown · unknownLHW L/E D BEAM FWD EXTERNAL SKIN FOUND DENT ( AFT OF NO.6 V/C FLAP )(<P>SKIN DENT ARAE REPAIRED AS PER RI NO : RI-57-41-16394 REV A</P>)SDR P5CA2023080100055Unknown · unknownRHW NO.20 V/C FLAP LSA FOUND DAMAGE(<P>PERFORMED REPAIR AT LSA DAMAGE AREA PER CMM 57-55-42 REPAIR 17-1</P>)SDR P5CA2023080100056Unknown · unknownRHW NO.19 V/C FLAP LSA FOUND DAMAGE(<P>PERFORMED REPAIR AT LSA DAMAGE AREA PER CMM 57-55-42 REPAIR 17-1</P>)SDR P5CA2023080100057Unknown · unknownRHW NO.20 V/C FLAP LSA FOUND DAMAGE(<P>PERFORMED REPAIR AT LSA DAMAGE AREA PER CMM 57-55-42 REPAIR 17-1</P>)SDR P5CA2023080300065Unknown · unknownLHW L/E LOWER PANEL UNDER #1E V/C FLAP FOUND CRACK(<P>PERFORMED REPAIR AT CRACK AREA PER RI-57-41-16401 REV.A</P>)SDR HNAA2023091800327Unknown · unknownE990709 DENT ON RH #1LEADING EDGE APPROXIMATELY 22 INCHES FROM INBD EDGE AND 19 INCHES FROM LOWER TRAILING EDGE. : PERFORMED REPAIR TO RH #1 LEADING EDGE APPROXIMATELY 22 INCHES FROM INBD EDGE AND 19 INCHES FROM LOWER TRAILING EDGE. IAW EMB 145 SRM 57-40-00 SDR SWAA2023083090508Plate · crackedOUTBD. WIGGLE PLATE UNDER RIGHT WING PANEL #661AB PHENOLIC FILLER CRACKED.<[01] REPLACED OTBD WIGGLE PLATE UNDER RIGHT WING PANEL #661AB IAW SRM 51-40-02.;[02] PART UPDATEDSDR DALA2023081806755Unknown · unknownSHIP 5642 RH HORIZONTAL STABILIZER / UPPER SKIN / AT REAR SPAR / CORROSION. CORRECTIVE ACTION: REF ERA 594728-14. (2919483)SDR DALA2023081806734Unknown · unknownSHIP 1705 RT WING THERMAL ANTI ICE DOOE ASSY MISSING. CORRECTIVE ACTION: FWD TO B767-300 CDL 57-41-02 .RT WING THERMAL ANTI-ICE DOOR ASSY . DISPATCH APPROVED , PLACARD INSTALLED (4571503)SDR UIEA2023063000674Unknown · unknownLH WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT RBL 7 WITH CRACK (FOUND DURING ACCESS PROCESS TO THE W/O A1N080-7-522)(<P>PERFORMED PERMANENT REPAIR ON REAR SPAR VAPOR BARRIER ATTACH ANGLE BETWEEN LBL 5 TO LBL 18.5 DUE TO CRACKS IAW B737-800 BCFSDR UIEA2023072800763Unknown · unknownRT WING FUEL TANK STIFFENER WITH CRACK, BETWEEN RIB 21 & RIB 22 (OBSERVED WHILE PERFORMING THE 20 YEARS INSPECTION)(<P>PERFORMED PERMANENT REPAIR ON RH OUTBOARD WING UPPER STRINGER U-9 DUE TO CRACK IAW COOPESA EO #: COO-EO-17861-R01 (JUL/15/23) DOCUMENTED AND SDR 2024FA0000024Stiffener · crackedFOUND RIGHT WING LOWER, INBOARD, FORWARD SKIN, FORWARD STIFFENER CRACKED. REPLACED
STIFFENERSDR NACA2023081100006Unknown · unknownRH WING NO.5 SLAT T/E WEDGE DELAMINATION AT SS.248~SS.254. REMOVED THE DELAMINATION SKIN AT RH WING NO5 SLAT T/E WEDGE SS248~SS254 MADE THE SKIN FILLER AND DOUBLER INSTALLED THE REPAIR PARTS AND PERFORMED 250°F METAL BOND REPAIR I.A.W B737-00 SRM 51-70-10 REPASDR NACA2023081100005Unknown · unknownRH WING NO.4 SLAT T/E WEDGE EDGE DEFORM AT SS.12.25. REMOVE THE INITIAL REPAIR DOUBLER AND DAMAGED CORE AT RH WING NO.4 SLAT T/E WEDGE EDGE SS12.25 MADE THE REPAIR CORE AND DOUBLER AND INSTALLED PERFORMED PERMANENT 250°F METEL METAL BOND REPAIR I.A.W B737-300SDR NACA2023081000002Unknown · unknownLH WING L/E PNL SUPPORT WAS CORRODED AT FSS 339 . REPLACED PNL SUPPORT AT LH WING L/E FSS 339 FROM PN 69-76227-1 I.A.W B737-300 SRM 51-40-2 PAGE 10~PAGE 12(REV 130)SDR SWAA2023092088284Plate · damagedCHECK LH WING DEFLECTOR RIB TO DEFLECTOR PANEL ATTACH SERRATED PLATES FOR CONDITION AND ELONGATED HOLES<[01] REMOVED AND INSTALLED NEW FASTENERS AT LH WING DEFLECTOR RIB PER SRM 51-40-02-0G-0;[02] VERIFIED FASTENERS REPLACEDSDR P5CA2023080300061Unknown · unknownLEFT WING, OUTBOARD FLAP, LOWER SURFACE, WS 764.2, WITH PERFORATION(<P>LEFT WING, OUTBOARD FLAP, LOWER SURFACE WAS REPAIRED IAW 57-00-00.</P>)SDR V0XD20230831001Unknown · unknownLIGHTNING STRIGKE DAMAGE TO LH SLAT #3 OUTER SKIN. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR IAW OLIVER WYMAN CAVOK EA 23-C7-57-0690 REV. A PART III. DTE TO BE ACCOMPLISHED WITHIN 12 MONTHS OF THE RETURN TO SERVICE DATE FOR THE SECTION III REPAIR IAW ACSDR FDEA202308081559Rib · gougedR/H WING SPOILER 5 BEAM I/B JACK RIB LWR BORE INNER FACE GOUGE ACCOMPLISHED THE REINFORCING REPAIR AT RH #5 SPOILER I/B JACK RIB I.A.W FEDEX EA NO:T6- 5740-T0375737 P1,SEQ NO:865, TITLE:WINGS - ATTACH FITTINGS - RH WING #5 SPOILER JACK RIB AT STA ABX 175.8SDR DALA2023080906493Unknown · unknownSHIP 3118 CORROSION TRAILING EDGE UPPER SKIN LOWER SURFACE AT LEVEL OF RIB11 ON LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 610039-14AD. (2908086)SDR SWIA202310270805Unknown · crackedLEFT WING BATT RIB WS48.30 ANGLE ON THE FORWARD END OF THE CAP IS CRACKED. (C-CHECK RO 10/29/2023) REMOVED AND REPLACED LH WING BATT RIB ANGLE AT W.S. 48.30 WITH NEW, REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21 AND DWG 600-10204 REV -L. COMPLIED WITHSDR SWIA202310805Unknown · corrodedLEFT WING BATT RIB WS53.60 ANGLE ON THE FORWARD END INBOARD SIDE IS CORRODED. (C-CHECK RO 10/29/2023) WET INSTALLED NEW LH BATT RIB ASSY AT WS53.60 REF CRJ-200 SRM 51-42-21, CRJ-200 SRM 51-42-06 AND DRAWING NO: 601R10203 REV-G. COMPLIED WITH SKYWEST TSDR YENA2023080800920Unknown · unknownDURING HEAVY MAINTENANCE: DEBONDED UPPER EXTERNAL SKIN I/B FLAP LOCATED AT 6.5 INCHES FROM INBOARD EDGE ON R/H WING; REF AEROMAN N/R 2023- 403383, REPAIRED UPPER SKIN I/B FLAP ON RH WING IAW EC# A23-652-01, EA# 57-0258-23, REV O, AND EA # 57-0258-23 PART 1. MASDR YENA2023080800918Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE OVERHANG RIB 18 TO RIB 19 ON RH WING; REF AEROMAN WO2023 132/1 NR2023-403107 -- REF JB NR 00013 FOR THE FUR CREATION.--REMOVED CORROSION LOCATED RIB 18 PLUS 15.163 INCHES TRAILING EDGE TSDR YENA2023080800911Unknown · unknownDURING HEAVY MAINTENANCE: CPCP FINDING: CORROSION ON RIB 3 IN ALL CONNECTORS SETTLEMENT AREA, BTW SPAR 2-3 WING LH AND RH; (RESOLVED ON W/O: 1241004 TASKCARD: NR-00017 )REF: TOMX W/O 2268 N/R 00204 CORROSION ON RIB 3 IN ALL CONNECTORS SETTLEMENT AREA, BTW SPARSDR SWAA2023083192860Access Panel · bulgedL/H WING LOWER MID T/E ACCESS PANEL # 561CB HAS BULGING/CRACKED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGED AREA FASTENER HOLES AS MARKED AT PANEL #561CB AS PER B737 SRM 51-70-04-2R-9 AND 51-70-04-2R-0 PARAGRAPH 4-L-M-N ; MATERIAL USED PO#1791128 ASDR CALA2023080402423Panel · missingPDA 1 PDA PANEL 652 MISSING FROM ACFT, ALONG WITH SECTIONS OF PANELS AND FARINGS SURROUNDING GEAR STRUCTURE. ADDING IMAGES ADDITIONAL IMAGESDR ENHA20230801003Unknown · unknownDURING SCHEDULED INSPECTION PER CESSNA TASK # 57-10-01-250, CRACKS WERE NOTED ON LH&RH ,FWD AND AFT LOWER STRUT FITTINGS.SDR FDEA202307301334Doubler · unknownEXISTING REPAIR FOUND AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 657. EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 657 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH MD-11 SRM 57-40-02-2R REPAIR 15SDR COEA2023101212816Landing · corrodedWO 247829 NR 600027 HEAVY CHECK COE/MAJOR REPAIR: R/H WING PANEL 622CT LANDING HAS FRETTING. CORRECTIVE ACTION: REPAIRED PER SRAS DO/TS-3018/09...5261 ISSUE G, DATED 9/29/2023.SDR SWI2023F00398Unknown · chafed*R/H WING T/E RIB CHAFFED ADJACENT TO OTBD GRND SPOILER ACTUATOR (MARKED), MX#26956335 (C-CHECK RO 10/4/2023) BLENDED AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ REO 670-57-51-509 REV -- DATE 2023-08-14. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITHSDR DALA2023072906145Unknown · unknownAIRCRAFT 678, LH OUTBOARD FLAP, OUTBOARD FLAP TRACK, FORWARD FUSE BOLT HAS CORROSION AND BOTH FORWARD INBOARD AND OUTBOARD BUSHINGS ARE CORRODED AND GOUGED. CORRECTIVE ACTION: REPLACED FORWARD FUSE BOLT AND BUSHINGS PER B757 AMM 27-51-03. (LP 2888019)SDR DALA2023072906144Unknown · unknownAIRCRAFT 678, LT WING - #3 FLAP TRACK FWD FUSE PIN AND 2EA BUSHINGS ARE CORRODED. CORRECTIVE ACTION: REPLACED #3 LEFT WING FLAP TRACK FWD FUSE PIN AND BUSHINGS. (LP 2887833)SDR SWAA2023072882803Panel · out of adjustRH WING INBOARD FIXED TRAILING EDGE UPPER PANEL IS OUT OF ADJUSTMENT.<[01] ADJUSTED PANEL REF AMM 57-50-01.;[02] REMOVED INSPECTION REQUIREMENTS. ADJUSTED PANEL REF AMM 57-50-01.SDR SWAA2023090582809Panel · crackedCRACK ACCESS PANEL 642BB AT RT WING 2023-469765<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: B20189527; DUE DATE: 26-DEC-23.;[02] TOOL USED: HOTBONDER P/N: HCS9200B-AV S/N: 18196021 DUE DATE: 24-JAN-24;[03] TOOL USED: SCALE P/N: CR5200; S/N: 8343110809; DUE D
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