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 = '5755' 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 = '5755' 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 UIEA2023050900438Seal · unknownLEFT WING O/B FLAP INBOARD EDGE HAS THE UPPER SEAL DAMAGED AT AFT END.(<P>REMOVED DAMAGED SEAL, CLEANED RETAINER LOCATED AND INSTALLED NEW SEAL AT L/H WING O/B FLAP I/B EDGE PER B767-300 AMM 20-10-23-963-001. NO FURTHER DEFECTS NOTED</P>)SDR CALA2023050301347Cover · missingPDA 3 MISSING LH OUTBOARD #4 FLAP TRACK MOVABLE FAIRING PIVOT COVER DURING WALKAROUND. COMPLETED WALKAROUND; NO DAMAGED FOUND.SDR FDEA202304070586Spoiler · delaminatedLH WING #6 SPOILER LOWER SURFACE IS PUNCTURED THROUGH BOTH THE UPPER AND LOWER SURFACES APPROX 12" O/B OF THE I/B EDGE. REPAIRED LH WING #6 SPOILER UPP AND LOWER SKINS IAW B767 SRM 57-70-01-2R FIG 201 SHEET 4 AND 51-70-05. MAJOR REPAIRSDR DALA2023040202507Unknown · unknownAIRCRAFT 3571, LH WING - WING SIDE FITTING INBOARD BUSHING FOUND WITH ABRASION. CORRECTIVE ACTION: DAMAGED BUSH REMOVED AS PER ASR A350-A-51-72-12-00001-660A-A. VISUAL INSPECTION CARRIED OUT ON LUG BORE AND FACES, NIL DEFECT. NEW FABRICATED BUSH INSTALLED AS PSDR DALA2023040202505Unknown · unknownAIRCRAFT 3571, RH WING - WING SIDE FITTING INBOARD BUSHING FOUND WITH ABRASION MARK. LOCATION EBHA - R SPOILER 5 (5CLI). CORRECTIVE ACTION: DAMAGED BUSH REMOVED AS PER A350-A-51-72-12-00001-660A-A. VISUAL INSPECTION CARRIEED OUT ON LUG BORE AND FACES, NIL DEFESDR FDEA202303280781Spoiler · wornLH WING ONE ANCHOR NUT ATTACH SKIN ENLARGED AT O/B WEB AREA OF #2 SPOILER FRONT SPAR CAVITY ACCOMPLISHED THE REINFORCEMENT REPAIR, THIS IS CAT.A REPAIR I.A.W FEDEX EA NO:T6-5750- T0373843 P1, SEQ NO:816, TITLE:WING-FLIGHT SURFACES-LH #2 SPOILER-WEAR DAMAGE SDR DALA2023032302218Unknown · unknownSHIP 1601 FOUND OUT SPOILER NO.6 EXTERNAL LOWER SURFACE CRACKED AT 12 INCHES TO IB EDGE AND 12 INCHES TO AFT EDGE. CORRECTIVE ACTION: CRACK REPAIRED ON SPOILER NO.6 EXTERNAL LOWER SURFACE AS PER B767-300 SRM 57-70-01-2R-1 & SRM 51-70-05.RELEASE:121.00-01/31/ 2SDR FDEA202303200667Skin · delaminated1EA DISBOND AREA WAS FOUND AT RH #5 SPOILER TOP SKIN.(1.3"X1.4") ACCOMPLISHED THE COMPOSITE REPAIR, THIS IS CAT.A REPAIR I.A.W A300-600 SRM 57-72-11-201, PARA.12, PAGE.211-217, FIG.207 "MAJOR REPAIR"SDR 9JLA2023032242009Battery · failedTHE FLIGHT CREW REPORTED THAT THE SPOILER FAIL AMBER ANNUNCIATOR ILLUMINATED ON 3 OUT OF 5 LEGS DURING TRIP AFTER ENGINE START ON THE GROUND. EACH TIME RESET PER THE QRH. THE BASE MAINTENANCE TEAM DUPLICATED THE FAULT AND NOTED THE EMERGENCY BATTERY VOLTAGE DRSDR 9JLA2023032244020Position Sensor · failedTHE FLIGHT CREW REPORTED THAT AFTER ENGINE START DURING FLIGHT CONTROL TESTS, A SPEEDBRAKE/ROLL SPOILER POSITION INDICATION AMBER FAULT AT ALL POSITIONS. THE SYSTEM WAS DISABLED AND OPERATIONS WERE CONTINUED PER A 10 DAY MEL 27-60-02. DURNING THE MAINTENANCE ESDR IPXA2023032592242Support · corrodedINSPECTION TYPE:3CR/H #1 SPOILER HAS EXCESSIVE PLAY.REPAIRED CORRODED SUPPORT ON THE R/H #1 SPOILER IAW VTSAA EA 011-5771-01-A9886 I/R AND UPS EO MD11-5740-86337-A DATED 03/24/23 (MINOR)SDR A6WA202302228488Bracket · crackedR/H FLAP STUB FAIRING HAS A BROKEN BRACKET THAT REQUIRES REPLACEMENT. ****AIRCRAFT REMOVED FROM SERVICE********** INSTALLED NEW R/H FLAP STUB FAIRING BRACKET AND RESTORED SURFACE FINISH IAW MHIRJ CRJ200 SRM 51-42-06-00 AND 51-21-16-00SDR SWAA2023021302210Spoiler · leakingLOSS OF HYDRAULIC B ON FINAL; EMERGENCY DECLARED.<[01] REMOVED AND REPLACED #5 FLIGHT SPOILER DUE TO LEAKING IAW AMM 27-61-51; ALSO R&R #2 ENGINE HYDRAULIC PUMP; B ELECTRIC HYDRAULIC PUMP; AND HYDRAULIC FILTERS CHANGED PRECAUTIONARY IAW AMM 29-11-21;AMM 29-11-SDR SWAA2023021301527Spoiler · missingLEFT WING #1 GROUND SPOILER UPPER SURFACE PREVIOUS REPAIR DOUBLER MISSING.<[01] R&R LEFT WING #1 GROUND SPOILER REF AMM 27-62-91.SDR AALA202301255534Spoiler · crackedAIRCRAFT WAS GROUNDED: RIGHT WING #5 SPOILER UPPER SURFACE OUTBOARD AFT CORNER CRACKED AND DELAMINATED. MAINTENANCE REPLACED SPOILER PER TASK CARD 26L00027024.SDR SWAA2023012383869Web · crackedLEFT WING JUST O/B OF I/B GROUND SPOILER FIXED TRAILING EDGE PANEL FWD WEB CRACKED O/B SIDE. REMOVED DAMAGED WEB. INSTALLED WEB WITH FASTENERS PER SRM 51-40-02.SDR SWIA2023011367103Nut · corrodedHARDWARE FOR RT FLIGHT SPOILER HINGE FITTINGS APPEARS TO BE CORRODED. INSTALLED SERVICEABLE NUTS AND WASHERS ONLY ON THE RT OTBD FLIGHT SPOILER CENTER HINGE FITTINGS IAW AMM 27-64-01-400-801, STEP 2B,(3D-3G), 2B, (4D, 4F-4H) AND 2C(3).SDR DALA2022111007264Skin · damaged(LOG 2485614) DURING INSPECTION FOUND NICKS LOWER SURFACE SPOILER NBR 6 LH WING. SPOILER NBR 6 LH WING WAS REPAIRED PER B737-900ER S.R.M. 51-70-10-2R PROCEDURE 4 REPAIR 4 IN REFERENCE TO B737-900ER S.R.M. 57-70-01-2R PROCEDURE 1 REPAIR 1.SDR DALA2022110407147None · noneSHIP 5638 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 603236-14AD. CORRECTIVE ACTION: REF ERA 603236-14AD.SDR SWAA2022111765411Support · crackedLH WING ACCESS PANEL FWD O/B SUPPORT CRACKED; UNDER SPOILER NO. 2 / [01] REMOVED AND REPLACED LEFT WING ACCESS PANEL FWD O/B SUPPORT UNDER SPOILER #2 IRW SRM 51-40-02.;[02] VERIFIED STEP 1;COMPLETESDR UIEA2022102201170None · noneCORROSION DAMAGE ON RIGHT INBOARD TE FLAP TORQUE TUBE(<P>RIGHT INBOARD TE FLAP TORQUE TUBE WAS REPLACED IAW SB 767-57A0066</P>)SDR DALA2022102406867None · noneSHIP 3115 - CORROSION BUSHING CENTER HINGE FITTING SPOILER 4 AT REAR SPAR ON RH WING. CORRECTIVE ACTION: REPLACED BUSHINGS PLAIN (3EA) ON CENTER HINGE FITTING OF SPOILER #4 RH WING AT REAR SPAR AS PER A319 SRM 51-72-12.(2465096)SDR DALA2022102406871None · noneSHIP 3115 - CORROSION BUSHING CENTER HINGE FITTING SPOILER 5 AT REAR SPAR ON RH WING. CORRECTIVE ACTION: REPLACED BUSHINGS PLAIN (3 EA) ON CENTER HINGE FITTING OF SPOILER #5 RH WING AT REAR SPAR AS PER A319 SRM 51-72-12.(2463956)SDR DALA2022102406870None · noneSHIP 3115 - CORROSION BUSHING CENTER HINGE FITTING SPOILER 3 AT REAR SPAR ON RH WING. CORRECTIVE ACTION: REPLACED BUSHINGS PLAIN (2 EA) ON CENTER HINGE FITTING OF SPOILER #3 RH WING AT REAR SPAR AS PER A319 SRM51-72-12.(2463933)SDR FDEA202210012429Hinge Arm · delaminatedRH WING - #5 SPOILER CENTER O/B HINGE ARM LOWER SURFACE FOUND DELAMINATION (AREA: 22MM*35MM,DEPTH:2.0MM) AND CENTER I/B HINGE ARM LOWER SURFACE FOUND DELAMINATION (AREA: 11MM*15MM,DEPTH: 2.3MM). COMPLIED WITH EA:6-5750-T0370909 P1. TITLE:WING - FLIGHT SURFSDR FDEA202210012427Hinge Arm · delaminatedLH WING - #5 SPOILER CENTER O/B HINGE ARM LOWER SURFACE FOUND DELAMINATION. (AREA: 30MM*45MM,DEPTH:2.59MM) COMPLIED WITH EA:6-5750-T0370908 P1. THIS IS CAT A REPAIR. MINOR REPAIR IAW FEDEX GMM 6 6082 RO3 CONFIGURATION, SO THE DAMAGE IS WITHIN THE ALLOWABLSDR SWAA2022100349480None · cracked-RIGHT WING UPPER T\E SHELF PNL O\B OF #7 SPOILER VERTICAL WEB CRACKED WHERE IT CONNECTS TO DEFLECTOR RIB. / [01] R&R RIGHT WING UPPER T\E SHELF PN VERTICAL WEB O\B OF #7 SPOILER REF SRM 51-40-02 AND SRM 51-10-02.SDR FDEA202209212710Spar · damagedLH WING #2 SPOILER FRONT SPAR O/B FACE GOT ABRASION. ACCOMPLISHED THE REPAIR WITH DOUBLER , FILLER AND SHIM. THIS IS CAT.A REPAIR I.A.W EA NO:6-5750-T0370876P1 , SEQ NO:000654 , TITLE:WING-FLIGHT SURFACES-LH #2 SPOILER OUTBOARD FACE OF THE FRONT SPAR AT RISDR FDEA202209212352Skin · delaminatedNO.8 SPOILER LWR SURFACE OB AFT CORNER FOUND DELAMINATION. NO.8 SPOILER LWR SURFACE OB AFT CORNER REPAIRED AS PER B777 SRM 57-70-01-2R REPAIR 1 AND SRM 51-70-04-2R REPAIR 1 REV 41.0.THE B777 SRM 57-70-01-2R REPAIR 1 AND SRM 51-70-04- 2R REPAIR 1 REV 41.0 COSDR AALA202209159407Bolt · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING #4 SPOILER HINGE BOLT HAS WORN THREADS. REPLACED HINGE BOLT PER AMM 27-64-44.SDR FDEA202208312119Skin · delaminatedRH WING #5 SPOILER CENTER I/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: 30MM*10MM, DEPTH: 1.5MM COMPLIED WITH EA: 6-5750-T0370081 P1. TITLE: WING - FLIGHT SURFACES - RH 5# SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE RH WINGSDR FDEA202208312118Skin · delaminatedLH WING #4 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: 35MM*40MM, DEPTH: 1.7MM COMPLIED WITH EA: 6-5750-T0370080 P1. TITLE: WING - FLIGHT SURFACES - LH 4# SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE LH WINGSDR FDEA202208312117Hinge · delaminatedLH WING #3 SPOILER CENTER I/B & O/B HINGE ARM LWR SURFACE AND CENTER I/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: (1) 65MM*28MM, DEPTH: 2.36MM (2) 35MM*15MM, DEPTH: 2.05MM (3) 40MM*35MM, DEPTH: 1.5MM COMPLIED WITH EA: 6-5750-T0370SDR FDEA202208202008Skin · delaminatedRH WING #5 SPOILER TOP SKIN FOUND DELAMINATION(AREA:35MM*32MM,DEPTH:1.8MM) AND CENTER O/B HINGE ARM O/B SIDE FOUND DELAMINATION(AREA:25MM*40MM,DEPTH:0.85MM) PERFORMED THE REPAIR ON RH WING #5 SPOILER AS PER A300-600F SRM57-72-11-201 PARA12 AND FEDEX EA 6-5SDR FDEA202208192003Skin · delaminatedLH WING #5 SPOILER CENTER O/B HINGE ARM LOWER SURFACE FOUND DELAMINATION (AREA: 15MM*25MM, DEPTH: 2.05MM) AND CENTER I/B HINGE ARM O/B SIDE FOUND DELAMINATION (AREA: 30MM*10MM, DEPTH: 1.12MM) AND UPPER SURFACE FOUND DELAMINATION (AREA1: 30MM*12MM, DEPTH:SDR FDEA202208192001Skin · delaminatedLH WING #4 SPOILER CENTER I/B HINGE ARM LOWER SURFACE FOUND DELAMINATION (AREA: 32MM*30MM, DEPTH: 2.25MM) AND CENTER I/B HINGE ARM O/B SIDE FOUND DELAMINATION (AREA: 20MM*20MM, DEPTH: 0.73MM) AND UPPER SURFACE FOUND DELAMINATION (AREA1: 40MM*15MM, DEPTH:SDR FDEA202208031855Skin · puncturedRIGHT WING SPOILER NO 7 LOWER SURFACE WITH PUNCTURE. RIGHT WING SPOILER NO 7 LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-70-01 REP. 1, FIG. 201 SHEET 1, 2, 4, PAGE 1-4 AND SRM 51-70-17-0G PARA. 4.C. PAGE 1, 25, 26, 36, 49; FIG. 11 REV.82 DEC15/2021SDR FDEA202208031854Skin · puncturedRIGHT WING SPOILER NO. 8 LOWER SURFACE WITH PUNCTURE R.H. WING SPOILER NO. 8 LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-70-01 REP. 1, FIG 201 SHEET 1, 2, 4, PAGE 1-4 AND SRM 51-70-17-0G PARA. 4.C. PAGE 1, 25, 26, 36, 49; FIG. 11 REV. 82 DEC15/2021SDR UIEA2022072600774Skin · debondedDISBOND - RH WING #11 SPOILER UPPER SURFACE T/E DISBOND(<P>1) PERFORM PERMANENT REPAIR AT RH WING #11 SPOILER UPPER SURFACE, REFER TO J/C ATTACHING SHEET 0307861 FOR DETAIL PROCESS, & SRM 57-70-02-2R-1 REV 95, SRM 51-70-10-2R-4 REV 95, & SRM 51-70-10-2R-0 REV SDR UIEA2022072600775Skin · debondedDISBOND - LH INBD #5 SPOILER UPPER SURFACE DISBOND(1) PERFORM PERMANENT REPAIR AT LH WING #5 SPOILER UPPER SURFACE. REFER TO J/C ATTACHING SHEET 0307862 FOR DETAIL PROCESS, & SRM 57-70-02-2R-1 REV 95, SRM 51-70-10-2R-4 REV 95, & SRM 51-70-10-2R-O REV 95. 2) COSDR FDEA202207201786Skin · gougedLEFT WING #5 SPOILER LOWER SKIN GOUGED REPAIRED LEFT WING #5 SPOILER LOWER SKIN IAW FEDEX EA # H-5730-T0369501 AND B767-300F SRM 57- 70-01-2R AND 51-70-04-0G.SDR 2022F00277None · dirtyWE HAD TO ABORT THE TAKEOFF FORM KPWA AT APPROXIMATELY 1630 LOCAL, DUE TO A RED SPILERS EXT CAS AND AURAL WARNING OCCURRING BETWEEN 90-100 KIAS ON THE TAKEOFF ROLL. THE CAS MESSAGE CLE3ARED ON ITS OWN AND AFTER RUNNING THE QRH AND WAITING 15 MIN, THE SECOND TSDR UIEA2022062400651Spoiler · delaminatedLHW #6 SPOILER LWR SURFACE I/B UPR CORNER DELAMINATED(PERFORMED METAL HOTBOND REPAIR AS PER SRM 51-70-10 REPAIR4 /FIG202)SDR 2022FA0000317Spoiler · corrodedSPOILER ASSY FOUND TO BE DELAMAINATED ON UPPER SKIN. LOWER SKIN IS MISSING / CORRODED CORESDR 2022FA0000305Spoiler · delaminatedSPOILER ASSY ARRIVED MISSING LOWER SKIN AND UPPER SKIN & DELAMINATED.SDR SWAA2022070620020Spoiler · delaminatedR/H WING #12 SPOILER UPPER SURFACE HAS A DENT WITH DELAMINATION MEASURING 3'L X 2.7'W X .070' DEEP WITH A W/Y RATIO OF 38 R/H WING #12 SPOILER UPPER SURFACE HAS A DENT WITH DELAMINATION MEASURING 3"L X 2.7"W X .070" DEEP WITH A W/Y RATIO OF 38 / [0SDR SROM06142201Hinge · corrodedRH INBD SPOILER, INBD HINGE, CHAFING WEAR ON BOTH AIRCRAFT FITTING AND SPOILER FITTING. DAMAGE MAX DEPTH IS 0.018", MAX WIDTH IS 0.600" AND DAMAGE LENGTH IS 1.700".SDR VNAA202206099910Rib · crackedR/H OUTBD GROUND SPOILER CENTER HINGE UPPER SURFACE LEADING EDGE CRACKED.SDR UIEA2022052500543Spoiler · dentedRHW #12 SPOILER FOUND 1EA DENT MARK AS MARKED. PERFORMED METAL HOTBOND REPAIR AS PER SRM 51-70-10 REPAIR 2 AND FIGURE - 203 REV 94 ,FEB 20/2022</P>)SDR UIEA2022052500544Spoiler · dentedLHW #4 SPOILER FOUND 1EA DENT MARK AS MARKED. PERFORMED METAL HOTBOND REPAIR AS PER SRM 51-70-10 REPAIR 4 AND FIGURE - 201 REV94 ,FEB20/2022
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