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 = '5751' 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 = '5751' 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 C8GA20090079Skin · dentedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RT INBD AILERON HAS 2 DENTS ON THE UPPER SURFACE. DAMAGED AREA WAS REMOVED DIM 4.5 INCH CIRCLE. FABRICATED DOUBLER. INSTALLED REPAIR, NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SDR C8GA20090078Skin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RT INBD AILERON TAB WAS DELAMINATED. DAMAGED AREA WAS REMOVED DIM 19.5 INCHES BY 5 INCHES. REMOVED DAMAGED CORE DIM 7.5 INCHES BY 3 INCHES. FABRICATED CORE , FABRICATED FILLER AND DOUBLSDR WRLA2009067Wedge · debondedDURING C3 CHECK IN TPE INSPECTION FOUND EGAT LT OUTBOARD AILERON WEDGE DISBOND AT XOA 842. REMOVE AND CLEANUP AREA. REPAIR THIS WEDGE PER DRAWING SG11570003. CHECK REPAIRED AREA WAS SATISFIED, CALCULATED THE REWORK BALANCE MOMENT IS 66.65 LB-IN PER SRM 57-5SDR IPXA09M55293Spar · damagedINSPECTION TYPE:4C WHILE REMOVING DAMAGE ON LEFT I/B AILERON T/E WEDGE UPPER SURFACE ACCIDENTALLY GROUND THROUGH AFT SPAR CHANNEL VERTICAL FACE APPROX .75 INCH. REPAIRED LEFT I/B AILERON AFT SPAR CHANNEL REF MD11 SRM VOL 1 57-00-01 FIG 11.SDR FDEA200903191551Skin · dentedRT WING AILERON, LOWER SKIN FOUND DAMAGED. LOWER SKIN OF AILERON REPAIRED IN ACCORDANCE WITH SRM 57-61-12 FIG 201.SDR MALA090040Skin · dentedDURING 30K AND 6Y INSPECTIONS, DENT IN AILERON UPPER SKIN LOCATED AT WS 367.4 AND 7 INCH FWD OF TRAILING EDGE. REPAIRED.SDR SWAA091774Aileron · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING AILERON DELAMINATED. REPAIRED AILERON PER SRM.SDR IPXA09M55295Repair · delaminatedINSPECTION TYPE:4C OLD REPAIR DELAMINATING ON LT I/B AILERON UPPER SKIN TRAILING EDGE. REMOVED OLD REPAIR, BONDED NEW REPAIR IAW UPS EO MD11-5750-32969-A.SDR ASAA0944884Aileron · delaminatedLT AILERON LOWER I/B FORWARD CORNER DELAMINATED. REMOVED DAMAGED AREA, REPAIRED PAINTED AND BALANCED IAW B737 400 SRM 57 60 02.SDR ASAA0944840Aileron · delaminatedLT AILERON LOWER I/B FORWARD CORNER DELAMINATED. REMOVED DAMAGED AREA, REPAIRED PAINTED AND BALANCED AILERON IAW B737 400 SRM 57 60 02.SDR USAA2009041490883Skin · delaminatedSAL - C22 - MAJOR REPAIR - DELAMINATION ON RIGHT AILERON TRAILING EDGE UPPER SURFACE BETWEEN WBL 498 TO WBL 522.5. REPLACED RIGHT AILERON IAW US AIRWAYS TASK CARD R3M27015.SDR TAMF20090001SStructure · chafedDURING C3 CHECK, FOUND RT AILERON INBOARD WITH CHAFING IN CORNER RT PART UPPER SIDE. REMOVED INBD AILERON IAW AMM 27-11-01 PAGE 401 TO 408 ACCOMPLISHED EWO 767 57-048 AILERON FITTING THICKNESS FOUND MIN 0.055 INCH IAW 767 NDT MANUAL D634T301 PART 4 SUB 51-00-SDR IPXA09855789Skin · misrepairedINSPECTION TYPE:SV SS 718-W3-07, LT AILERON UPPER SKIN REPAIR AT STA XA 581 DOES NOT CORRELATE TO A CURRENT SRM. REPAIRED PER DC8 SRM 57-2-1 FIG 2-Y.SDR C2XA09SH067Bushing · migratedSHV - DURING C-CHECK LT AILERON TO PCA FITTING HAS MIGRATED I/B & O/B HAT BUSHINGS O/B SIDE. MAINTENANCE REMOVED AND REPLACED LT AILERON PCA FITTING IAW EC5750-01177 REV B. PERFORMED BACKLASHES IAW EMB-145 AMM 27-11-00 AND DEFLECTIONS IAW EMB-145 AMM 27-10-0SDR C2XA09SH064Fitting · wornSHV - DURING C-CHECK LT AILERON TO PCA FITTING HAS MIGRATED I/B & O/B HAT BUSHINGS O/B SIDE. MAINTENANCE REMOVED AND REPLACED LT AILERON PCA FITTING IAW EC5750-01177 AND COMPLETED OPS CHECKS IAW EMB 145 AMM 27-11-00 AND AMM 27-10-00-700-801-A. THE AIRCRAFT WSDR FDEA200902270750Skin · crackedLEFT WING T/E OUTBD AILERON INBD EDGE LOWER SKIN CRACKED AND BENT WBL 492.0. TRIMMED OUT DAMAGE IAW SRM 51-10-1 & 57-50-1 FIG 4. CW HFEC AND NO CRACKS INDICATED, MATERIAL LOSS 0.100 IN LENGTH & FOUND WITHIN LIMITS IAW SRM 57-50-1 FIG 4. TREATED & PRIMED ESDR CA090225013Hinge · cracked(CAN) LT AND RT OTBD AILERON HINGES, ATTACH FLANGES CRACKED IN RADIUS. LT AND RT OTBD AILERON HINGES REPLACED WITH NEW. RIVETING CARRIED OUT IAW AC 43-13-1B, CHAP. 4-57. AILERON REMOVAL AND INSTALLATION CARRIED OUT IAW MM NR D2060-1-13, CHAP. 6-10. DUAL INSDR UPS09554743Skin · delaminatedRIGHT AILERON HAS DELAMINATION. R & R RIGHT AILERON ASSY PER MM 27-11-21-4. CHECKS NORMAL.SDR C2XA09SH050Bracket · wornSHV DURING C-CHECK RT AILERON DAMPNER ATTACHMENT POINT O/B HAT BUSHING ON AILERON SIDE FITTING IS WORN. MX R&R RT AILERON DAMPNER BRACKET IAW EMB 145 SRM 51-40-02. THE ACFT WAS APPROVED TO RETURN TO SERVICE.SDR IPXA09856152Skin · misrepairedINSPECTION TYPE:SV SS 852-W3-30, DOUBLER LT WING O/B AILERON UPPER SURFACE STA XA 633 DOES NOT CORRELATE TO A SRM REPAIR. REPAIRED PER DC8 SRM 57-02-01 FIG 2X SHT 1 REV 78.SDR USAA2009022690449Rib · crackedMCN - C24 - MAJOR REPAIR - CRACK ON LEFT AILERON INBOARD CLOSURE RIB. REPLACED LEFT AILERON INBOARD CLOSURE RIB IAW B737 SRM 51-40-02.SDR USAA2009040390791Structure · deterioratedMCN - C1 - MAJOR REPAIR - DETERIORATED COMPSITE ON AILERON AT WBL 720. REPAIRED DETERIORATED COMPSITE ON AILERON AT WBL 720 IAW B757 SRM 51-70-03.SDR FDEA200902040458Skin · delaminatedRIGHT WING, OUTBOARD AILERON TRAILING EDGE MIDDLE SECTION FOUND DELAMINATION. REPAIRED AS PER DRAWING SG11570003. WEIGHT AND BALANCE CARRIED OUT, ACTUAL = 31.00 IN-LBS, AS PER CMM 57-51-03. REFER TO WORKCARD 27C1306 FOR OPERATIONAL CHECK. REPAIR CLASSIFIEDSDR USAA2009022390408Aileron · delaminatedSAL - C21 - MAJOR REPAIR - RIGHT AILERON DELAMINATED BETWEEN WBL 417.250 TO WBL 521.850. REPLACED RIGHT AILERON IAW US AIRWAYS TASK CARD R3M27015.SDR UPS09M54504Wedge · damagedINSPECTION TYPE:N/A LT WING AILERON I/B TRAILING EDGE WEDGE DAMAGED AT O/B SECTION. REPAIRED AILERON AS PER EO MD11-2710-32103-B.SDR QXEA2009020200060Skin · chafedPDX - C2 - LT AILERON FWD UPPER SKIN PANEL AT LEADING EDGE IS CHAFING. BLENDED CHAFING SMOOTH IAW CRJ 700 SRM TASK 57-61-01-101-001-A01 PG 102 TABLE 1. HFEC AND FPI INSPECTED BLENDED AREAS FOR CRACKS IAW CRJ 700 NDTM 51-20-006 AND 51-20-008, NO CRACKS NOTED.SDR IPXA09855501Skin · misrepairedINSPECTION TYPE:SV SS 814-W4-4, RT WING, AILERON LOWER SKIN EXT DOUBLER STA 552 DOES NOT CORRELATE TO A SRM. STA XA552. ACCOMPLISHED REPAIR PER TIMCO REO-G12611 REV D, AND UPS EO DC8-5720-3 3066A.SDR UPS09554511Skin · damagedINSPECTION TYPE:C2 RT AILERON HAS LIGHTNING STRIKE DAMAGE ON UPPER T/E SURFACE 8 INCHES I/B OF THE O/B END. REMOVED AND REPLACED CONDUCTIVE FRAME PER SRM 51-40-02-0G, AMM51-21-10-7 SRM 51-60-01-0G.SDR C2XA09SH022Bushing · migratedDURING C-CHECK, RT GROUND SPOILER ATTACHMENT BRACKET HAS MIG HAT BUSHING. R&R RT GROUND SPOILER ATTACHMENT BRACKET IAW EMB 145 AMM 57-51-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH021Bushing · migratedDURING C-CHECK, LT AILERON BRACKET HAS MIGRATED HAT BUSHINGS. R&R AILERON BRACKET IAW EC5750-01177. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR 2009FA0000084Rod End · lack of lubeINSTRUCTOR NOTED ON A PREFLIGHT THAT THE LT AILERON WAS EMITTING A SQUEAKING SOUND . FOUND THAT IT WAS DUE TO A LACK OF LUBRICATION OF THE AILERON ROD END BEARING . NOTING THIS, DUE TO A EARLIER INSTANCE OF ANOTHER SN SAME TYPE ACFT THAT A STIFF AILERON CONTROSDR IPXA09855535Skin · gougedINSPECTION TYPE:SV SS 814-W4-21, RT WING INBOARD AILERON UPPER SURFACE FWD END AT STA 508.07 78, REPAIR DOUBLER GOUGED. ACCOMPLISHED REPAIR PER TIMCO REO-G12646 REV B, AND UPS EO DC8-5720-32 972A.SDR IPXA09855498Skin · misrepairedINSPECTION TYPE:SV SS 814-W4-05, RT AILERON, LOWER SKIN, INBOARD EDGE STA XA621, REPAIR DOUBLER FASTENER EDGE DISTANCE LESS THAN 1.5D AT ONE OR MORE FASTENERS. ACCOMPLISHED REPAIR PER TIMCO REO-G12607 REV C, AND UPS EO DC8-5720-32 842A.SDR C2XA09SH008Bracket · out of limitsSHV DURING C-CHECK RT AILERON DAMPER BRACKET O/B FITTING OUT OF LIMITS IAW EC5740-01152B. MX R&R RT AILERON BRACKET O/B FITTING IAW EMB-145 SRM 51-40-02 AND EMB-145 CPM 51-21-07. THE ACFT WAS APPROVED TO RETURN TO SERVICE.SDR DL76S090128Structure · damagedRIGHT INBOARD AILERON HOLE REPAIRED IAW SRM 51-70-17 WITH REF SRM 57-60-01. C/W SRM 51-70-17.SDR C2XA08SH162Shroud · corrodedSHV DURING C-CHECK LT AILERON LOWER SHROUD HAD CORRODED BONDING PLATE. MX REPAIRED LT LOWER AILERON SHROUD IAW EC 5750-01315 (E). THE ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA08SH160Shroud · corrodedSHV DURING C-CHECK RT AILERON LOWER SHROUD HAD CORRODED BONDING PLATE. MX REPAIRED RT AILERON LWR SHROUD IAW EC 5750-01315 (E). THE ACFT WAS APPROVED TO RETURN TO SERVICE.SDR ASAA0844081Fitting · gougedRT AILERON O/B CORNER FWD EDGE FITTING IS GOUGED. REMOVED GOUGED FITTING INSTALLED REPLACEMENT FITTING IAW B737 SRM 51 40 02.SDR UIEA200800345Skin · delaminatedLT WING OUTBOARD AILERON UPPER SURFACE HAS 3 AREAS WITH PREVIOUS REPAIRS DELAMINATING. DELAMINATION AT WBL 883.0 AREA IS 3.5 BY 2.0 INCHES, LOCATED 9.5 INCHES FROM T/E, WBL 991.0 AREA IS 4.0 BY 2.0 INCHES, LOCATED 8.5 INCHES FROM T/E AND AT WBL 1033 AREA IS 7SDR KCSA081607Skin · gougedLT INBOARD AILERON LOWER L/E IS GOUGED.SDR KCSA081606Rib · crackedLT INBOARD AILERON INBOARD RIB CRACKED.SDR CA081208009Bracket · cracked(CAN) DURING MAINTENANCE INSPECTION BOTH THE LT AND RT AILERON QUADRANT SUPPORT BRACKETS WERE FOUND CRACKED. PART NUMBERS INCLUDED, LT END PIECE P/N 85711570-101, RT END PIECE P/N 85711570-102, LT BOTTOM PLATE P/N 85711572-101, RT BOTTOM PLATE 85711572-102, OSDR HALA2008112300872Structure · damagedFOUND DAMAGE TO LT WING OTBD AILERON OTBD STATIC WICK. OK TO CONTINUE.SDR CA081124007Support Bracket · cracked(CAN) DURING HEAVY CHECK INSPECTION FOR ACFT (316), BOTH THE LT AND RT AILERON INPUT QUADRANT SUPPORT BRACKET ASSEMBLIES, ON BOTH THE INBD AND OTBD SIDES, WERE FOUND TO HAVE SIGNIFICANT CRACKING. FLEET CAMPAIGN HAS BEEN INITIATED TO INSPECT THE AFOREMENTIONESDR CA081121004Seal · split(CAN) THE AILERONS WERE REMOVED AT THE ANNUAL INSP FOR BEARING REPLACEMENT. A SMALL RIP WAS FOUND IN THE INNER SEAL OF THE LT AILERON WHICH ATTACHES BETWEEN THE WING AND THE AILERON BALANCE WEIGHT ATTACHMENT. WHEN THE MS35207-XXX SCREWS WERE REMOVED THE WERE FSDR CA081110004Control Cable · dislodged(CAN) RT WING FWD AILERON CONTROL CABLE FOUND SITTING BEHIND THE AILERON INPUT ROD QUADRANT GUARD. CABLE MOVED OUT OF ITS LOCATION WITH SLIGHT FINGER ACTION. CABLE HAS LIGHT RUBBING MARK BUT ALUMINUM QUADRANT GUARD FOUND BADLY GROOVED. WINGS CONTROL CABLE TSDR QXEA2008112001175Structure · chafedPDX - C3 - LT AILERON TOP LEADING EDGE IS CHAFED IN SEVERAL PLACES. BLENDED CHAFE IAW SRM 57-61-01-001-A01. UT THICKNESS CHECKED BLENDED AREAS IAW NDTM 51-20-04 FOUND TO BE OUT OF LIMITS. REMOVED LT AILERON TOP LEADING EDGE IAW SRM 51-42-06 PG 8 STEP 11 ANDSDR UPS08854030Skin · misrepairedINSPECTION TYPE:SV LT WING OUTBOARD AILERON UPPER SURFACE AT STA XA685 HAS EXTERNAL DOUBLER SURVEY DOES NOT MEET SRM REQUIREMENTS. REPAIRED AS PER UPS EO DC8 5720 31284 A.SDR C2XA08SH135Bushing · migratedSHV - DURING C-CHECK RT AILERON CENTER O/B BRACKET HAS MIGRATING HAT BUSHING. MX REMOVED AND REPLACED RT AILERON CENTER O/B BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR UPS08854013Doubler · damagedINSPECTION TYPE:SV LT AILERON STA 454 HAS A REPAIR DOUBLER WITH EDGE DAMAGE. REPAIRED AS PER UPS EO DC8 5710-31295A.
Back to JASC 5751