JASC 5730
Service difficulty reports · 27,269
Reports filed under 5730 · Wing, Plate/Skin, newest first.
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 = '5730' 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 = '5730' 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 UIEA200900009Skin · delaminatedLT WING UPPER SURFACE FIXED L/E PANEL AT ILES 921.5 AND 25.0 INCHES FROM AFT END OF PANEL HAS AN AREA OF 3.0 INCH DIAMETER OF DELAMINATION. PERMANENT REPAIR ACCOMPLISHED AS PER B747 SRM 51-40-09 FIG 18, SHEETS 3 AND 5, PREPREG 250 DEGREES F CURE PER SRM 51-40SDR A6WA200940026Skin · corroded131226-222, SURFACE CORRODED ON LT WING PLANK FUEL ACCESS HOLES AT PANEL 540AB, 540EB, 550BB, 550DB AND 550FB. REO 601R-57-21-030, REV G. (K)SDR A6WA200940025Skin · corroded131266221, SURFACE CORRODED ON RT WING PLANK FUEL ACCESS HOLE AT PANEL 610AB, 640CB AND 650GB, REO 601R-57-21-030, REV G. (K)SDR UIEA200800354Skin · looseRIGHT WING LEADING EDGE FAIRING AT OUTBOARD OF LANDING LIGHT FOUND LOOSE RIVETS. LEADING EDGE SKIN REPAIRED AS PER SRM 57-41-01-2R-5 REPAIR 5 FIGURE 201.SDR FDEA200901210300Skin · crackedFIVE FASTENER HOLES, FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA XORS=690 AND STA XORS-700.SDR IPXA09M55563Skin · crackedINSPECTION TYPE:3C LT WING FIXED LE THE SKIN SUPPORT ABOVE THE OTBD FUELING MANIFOLD HAS 2 INCH CRACK/VIEW INSIDE FUELING PANEL . REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER, ANGLES, AND FILLER IAW MD-11 SRM 57-10-00 FIG 27SDR IPXA09855337Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 752-W4-07 REPAIR AT RT WING STA 347.750 LOWER L/E HAS A STEEL DOUBLER AND MIN FASTENER SPACING 3&1/2 D AT ONE LOCATION. ALSO CUTOUT IS NOT VISIBLE REF APPENDIX H STEPS 6&7. REMOVED DOUBLER IAW DC8 SRM 51-3-0 AND 51-1-20. FSDR IXXA09SMN005SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT CENTER LEADING EDGE UPPER SKIN CORRODED AT STATION XFS 280.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED SDR IXXA09SMN004SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT CENTER LEADING EDGE UPPER SKIN CORRODED AT STATION XW 253.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NSDR IXXA09SMN006SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XCW 69.500. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION NOTED. FABRICATED NEW SKIN, FILLER PLUG.SDR UPS09M54459Skin · crackedINSPECTION TYPE:3C LT WING L/E TELESCOPIC DUCT CUTOUT I/B AND O/B CORNER CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW MD-11 SRM 57-10-00 FIG 43.SDR IPXA09855222Skin · misrepairedINSPECTION TYPE:SV SS 752-W4-18, RT WING L/E UPPER SURFACE REPAIR AT STA XFS 556 DOUBLER SKIN THICKNESS LESS THAN SRM CALL OUT. REPAIRED PER DC8 SRM 57-02-01-0 FIG 38 SHT 1 REV 78.SDR IPXA09855186Skin · crackedINSPECTION TYPE:SV RT WING L/E SECTION LOWER INTERIOR SKIN CRACKED ON O/B END AFT OF SPAR NEXT TO FWD SCREW ATTACH HOLE XS 526. REPAIRED PER TIMCO REO-G12594 REV A, AND UPS EO DC8-5720-32213A.SDR HNAA2009061700180Panel · unknownALL WING STRESS PANEL NEEDS REWORK. REWORK PANEL IAW RD8-57-1420 AND RD857-1715.SDR IPXA09855259Skin · misrepairedINSPECTION TYPE:SV LT WING L/E UPPER EXT SURFACE AT XFS 195 REPAIR INCORPORATES FASTENERS WITH LESS THAN 4D, SS 572-W3-15. REPAIRED PER TIMCO REO-G12603 REV B, AND UPS EO-5720-32342-A.SDR UIEA200900008Panel · delaminatedRT WING UPPER SURFACE FIXED T/E PANEL AT WBL 445.0 JUST FWD OF INBD AILERON SMALL AREA OF DELAMINATION. AREA IS 3.5 BY 1.250 INCHES. PERMANENT REPAIR ACCOMPLISHED IAW SRM 51-40-09, FIG. 2 SHEET 2 AND 5, PREPREG LAYUP 250 DEGREES F CURE IAW SRM 51-40-12.
ALSO,SDR UALA2009011900214Skin Panel · damagedDEICER STRUCK LT OUTBOARD WING TIP DAMAGING T/E. AFT WING TIP PANEL REMOVED AND ROUTED TO SHOP 273 FOR PERMANENT REPAIR. PANEL REINSTALLED, LIGHT AND STATIC DISCHARGERS CHECKED BY SFOOV AMT. WORK ACCOMPLISHED ON WU U5098J.SDR UPS09854403Skin · damagedINSPECTION TYPE:P T/E SKIN DAMAGED AFT EDGE STATION XRS 337, 14.4 INCHES INBOARD / OUTBOARD AND 1.8 INCH FORE / AFT. REPAIR PER EO DC8-5730-31951A.SDR IPXA09855488Doubler · gougedINSPECTION TYPE:SV SS 814-W3-15, LT INBOARD LEADING EDGE UPPER SKIN REPAIR DOUBLER GOUGED, XSF 9.5. REPLACED PER DC8 SRM 57-2-1 FIG 37 REV 78.SDR IPXA09855419Doubler · gougedINSPECTION TYPE:SV SEQ 814-W3-15 LEFT I/B LEADING EDGE UPPER SKIN REPAIR DOUBLER GOUGED XFS 1 TO XFS 9.5. FABRICATED REPAIR DOUBLER IAW DC8 SRM 57-2-1 PG 135-136 FIG 37. INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-1 FIG 37 PG 135-136.SDR UALA2009011600182Fairing · damagedRIGHT WING MOST O/B CANOE FAIRING IS DAMAGED. PER SHOP EST WILL REQUIRE 10HR FOR REPAIR. REPAIRED BY SHOP 273. REPAIRED PER GNMM 1-0-1-24 FROM 1-14-09 2300 TO 1-15-09 0600.SDR SWAA090349Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND LT UPPER WING SKIN CRACKED AT BS WBL 173. REPAIRED SKIN PER SWA EA.SDR UPS09M54643Skin Panel · gougedINSPECTION TYPE:1C RT WING PNL 617CT GOUGES AS MARKED (OFF A/C PART). REMOVED SKIN, FABRICATED, AND BONDED REPAIR DOUBLER IAW MD-11 SRM 51-71-00 PARA 16(B).SDR DLM88090391Access Panel · corrodedTANK ACCESS PLATE CORRODED AT FASTENER HOLE.SDR IPXA09855511Skin · misrepairedINSPECTION TYPE:SV SS 814-W4-30, RT WING CTR L/E STA XFS 422.750 REPAIR DOUBLER FASTENER EDGE DISTANCE LESS THAN 1.5D. ACCOMPLISHED REPAIR PER TIMCO REO-G12606 REV B, AND UPS EO DC8-5720-3 2403B.SDR IPXA09855490Skin · misrepairedINSPECTION TYPE:SV SS 814-W3-2, DOUBLER DOES NOT CONTAIN REPAIR FASTENERS, LT WING AT XFS 67.5. REPLACED PER TIMCO REO-G12617 REV A, AND PER UPS EO DC8-5720-32400A.SDR UPS09554336Skin · delaminatedINSP TYPE: C2 RESTORE FIBERGLASS OUTER PLY FINISH ON RW INBD FLAP LOWER SURFACE 85 INCHES FROM INBD END. REMOVED DAMAGE FROM AREA AND REPAIRED IAW SRM 57-53-01-2R-2.SDR COEA2009011204913Skin Panel · dentedFOUND IN COE MAJOR REPAIR. DENTS AND GOUGES ON RT WING LWR SKIN IN AREA OF SINGLE POINT FUELING DOOR. BLEND OUT OF CORROSION BEYOND SRM (STRUCTURAL REPAIR MANUAL) ALLOWABLE LIMIT. MULTIPLE DENTS BETWEEN RIBS 19 - 21 STRINGERS 2 - 5 FROM FUEL CAP. SRAS DO/TSDR ABXA200901090002Panel · missingPANEL MISSING ON RT WING. REPLACED RT WING ANTI-ICING DUCT DOOR IAW 767 MM 57-41-58.SDR UALA2009031000084Panel · crackedFOUND 6 INCH CRACK IN UPPER WING INBD L/E PANEL 4FT INBD OF NR 3 ENG. REPAIRED REF SRM 57-41-01 REPAIR 2.SDR FDEA200901080100Skin · crackedRIGHT WING OUTBD FLAP; INBD SECTION; UPPER SKIN IS GOUGED. REMOVED DAMAGED SKIN. FABRICATED & INSTALLED NEW SKIN IAW EA 6-5750-123685 & SRM 51-40-21 PG 13. ALODINED PRIMED & PAINTED IAW SRM 57-21-10; PARA 2-B & 51-10-13. PART MARKED SKIN IAW GMM 7-0-1001.SDR UALA2009010800084Panel · crackedFOUND 6 INCH CRACK IN UPPER WING INBD LEADING EDGE PANEL 4FT INBD OF NR 3 ENGINE. REPAIRED REF SRM 57-41-01 REPAIR 2.SDR SWAA090120Skin · crackedDURING SCHEDULED 24Y CHECK, FOUND RT WING INBD L/E SKIN CRACKED. REPAIRED SKIN PER SRM.SDR FDEA200901070077Skin · chafedRIGHT WING DROOP LEADING EDGE INBOARD EDGE SKIN WITH CHAFE MARK. REPAIRED AS PER E.A. 1-5750-127877. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR UIEA200900005Panel · delaminatedLT WING, UPPER SURFACE FIXED L/E PANEL AT OLES 1210.5 AND 5.0 INCHES FROM FORWARD EDGE OF PANEL, SKIN HAS AN AREA OF 2.0 BY 3.0 INCHES OF DELAMINATION. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18, SHEETS 4 AND 5, PREPREG 250 DEGREES F CUSDR AALA200810555Skin · wornLEFT WING LOWER SKIN WORN BEYOND LIMITS AT OUTBOARD SIDE OF STRUCT FAIRING FORWARD AND AFT OF TANK PLATE CUT OUT. DAMAGE BLENDED TREATED, PRIMED AND REPAIRED PER ESO 61000 DATED 1/2/09.SDR MASA2009010600012Winglet · damagedPERMANENT REPAIR TO RT WINGLET TIP FAIRING DUE TO LIGHTNING STRIKE DAMAGE.SDR MASA2009010500007Skin · crackedRT LWR WING PLANK CRACKED AT WS 148.019, PERMANENT REPAIR.SDR AALA200810550Skin · wornRT WING INBD FLAP OTBD TRACK FWD FAIRING LOWER WING SKIN WORN INBD SIDE IN EXCESS OF 0.030 INCH FROM CONTACT WITH SEAL. REPAIRED IAW ESO 61000, DATED 1-02-09.SDR AALA200810549Skin · wornRT WING LWR SKIN PANEL WORN IN EXCESS OF 0.030 IN OTBD SIDE FROM RT AFT STRUT FAIRING, AFT SIDE OF TANK PLATE.SDR FDEA200901050039Skin · gougedLT WING LWR SKIN LOWER SURFACE IS GOUGED AT THE FWD SPAR ATTACHMENT BETWEEN THE PRESSURE FUELING CAPS.SDR UPS09554369Skin · damagedINSPECTION TYPE:C1 AOG RESPONSIBILITY, WHILE DRILLING OFF FASTENER HEAD ON CNTR TANK ACCESS PANEL 134AZ CAME OFF FASTENER AND CAUSED DAMAGE TO FUEL CELL CUT OUT EDGE. REPAIRED PER ATS ENGINEERING REPAIR 09-1026.SDR UPS09M54384Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQ 289-W4-03 SOME HI-LOKS NOT FLUSHED AND SOME FASTENERS OUT OF EDGE DISTANCE ON RT WING L/E STA XOS 708-729. REMOVED EXISTING REPAIR ON RT WING L/E STA XOS 708 TO 729 REF REPAIR SURVEY SEQ 289-W4-03 AND REPAIRED L/E SKIN REFSDR MASA2008122900761Winglet · damagedPERMANENT REPAIR TO LT WINGLET TIP FAIRING DUE TO LIGHTNING STRIKE DAMAGE.SDR MASA2008122900760Winglet · damagedPERMANENT REPAIR ON LT WINGLET DUE TO LIGHTNING STRIKE DAMAGE.SDR I5HA0858015Skin · damagedDURING CLIMB OUT, EN-ROUTE, THE CREW FELT A "THUMP" POSSIBLY FROM THE LT WING. THE CREW COULD NOT SEE ANY DAMAGE AND DID NOT EXPERIENCE ANY CONTROL PROBLEMS. THE CREW CONTINUED THEIR FLIGHT AND LANDED UNEVENTFULLY. EXAMINATION BY THE CREW OF THE LT WING REVSDR ASAA0944223Skin · damagedLT WING FIXED LE HAS FIBER DAMAGE AT NR 1 SLAT IB AUX TRACK CUTOUT. REPAIRED LT WING FIXED LEADING FIBER DAMAGE AT NR 1 SLAT IB AUX TRACK CUTOUT.SDR ASAA0844098Skin · damagedLT WING FIXED LE HAS FIBER DAMAGE AT NR 1 SLAT I/B AUX TRACK CUTOUT.SDR FDEA200812225259Skin · crackedRIGHT WING FIXED LEADING EDGE ACCESS PANEL NR 619CB CUTOUT FOUND CRACKED. RIGHT WING FIXED LEADING EDGE ACCESS PANEL 619CB CUTOUT CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR FDEA200812225258Skin · crackedRIGHT WING FIXED LEADING EDGE SLAT TRACK 12 SKIN FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
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