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 06FDEA1020Skin · crackedLEFT WING UPPER SURFACE T/E FOUND 1EA CRACK ON HONEYCOMB PANEL AT XORS 299. REPAIRED PANEL IAW SRM 57-00-01 FIG 1 SHT 1 VOL 1 AND SRM 51-70-00 PARA 16 VOL 2, FABRICATED PART IAW DETAIL PART TRAVELER F163459/N00459 AND IAW SRM 57-00-01 AND 51-70-00 VOL 1-2.SDR 06FDEA1006Skin · crackedRIGHT WING FIXED L/E TELESCOPE DUCT CUTOUT FOUND CRACKED. RIGHT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT CRACKED AREA REPAIR CARRIED OUT AS PER FEDEX EA #1-5740-94613, TITLE: WINGS. LEADING EDGE AND LEADING EDGE DEVICES, RIGHT FIX LEADING EDGE SKIN RSDR 06FDEA1005Doubler · crackedRIGHT HAND WING FIXED L/E BEADED DOUBLER FOUND CRACKED AT XORS 542. REPAIR CARRIED OUT AS PER FEDEX EA 1-5730-95786.SDR 06FDEA1007Doubler · crackedRIGHT HAND WING FIXED L/E BEADED DOUBLER FOUND CRACKED AT XORS 522. REPAIR CARRIED OUT AS PER FEDEX EA 1-5730-95786 PT1. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 06FDEA1002Skin Panel · corrodedUPPER CARGO BAY, UNDER FLOOR AREA, CENTER WING TANK TOP SURFACE FOUND WITH CORROSION BS 1204 RBL 107. SURFACE CORROSION ON UPPER CARGO BAY UNDER FLOOR AREA, CENTER WING TANK TOP SURFACE AT BS 1204 RBL 107 REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHSDR 06FDEA1001Skin · corrodedUPPER CARGO BAY UNDER FLOOR AREA, CENTER WING TANK TOP SURFACE FOUND WITH CORROSION FS STA 1239 LBL 02. SURFACE CORROSION ON UPPER CARGO BAY UNDER FLOOR AREA, CENTER WING TANK TOP SURFACE AT STATION 1239 LBL 02 REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUNDSDR 06FDEA1000Skin Panel · corrodedUPPER CARGO COMPARTMENT UNDER FLOOR AREA, CENTER WING TANK TOP SURFACE FOUND WITH CORROSION FS STA 1219 LBL 95. REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER FEDEX E.A 1-5710-95783. MATERIAL ORIGINAL THICKNESS=0.173", MATERIAL RESDR 06FDEA01000Skin Panel · corrodedUPPER CARGO COMPARTMENT UNDER FLOOR AREA, CENTER WING TANK TOP SURFACE FOUND WITH CORROSION FS STA 1219 LBL 95.SDR IXXA06SMN099SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, RIGHT WING OUTBOARD INNER LEADING EDGE EXTERNAL UPPER SKIN HAS NON STANDARD REPAIR AT STATION XFS 572.500. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 38 TR # 57-85 DATE 11-27-2000. REMOVED EXISTING REPAIR DOUBLER IAW DC8SDR IXXA06SMN088SSkin · dentedDURING ROUTINE C CHECK, RT WING L/E DENTED (STA XFS 888.000 920.000). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-3-3 FIG 8. REMOVED DAMAGED PLATING IAW DC8 SRM 57-1-0, DC8 SRM 51-1-21. FABRICATED NEW PLATING (AL 7075 T6 0.050) IAW DC8 SRM 57-3-3 FIG 8 ITEM A, DC-SDR IXXA06SMN075SPanel · crackedDURING ROUTINE C-CHECK INSPECTION, NR 1 PYLON LT UPPER PART PANEL CRACKED 2 INCHES, YN 321.000. PERFORMED MAJOR REPAIR IAW DC8-70 SB 54-93 CONDITION V. REMOVED FASTENERS IAW SB 54-93 PAGE 11 FIG 2 DC8 SRM 51-3-0, DC8 SRM 51-1-21. PERFORMED VISUAL INSPECTIONSDR IXXA06SMN076SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, LT WING NR 1 STUB WING CRACKED 2.5 INCH, XILD 42 LWR SKIN. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1A FIG 1. REMOVED EXISTING DOUBLERS IAW DC8 SRM 51-1-20D, DC-8 SRM 51-1-21. PERFORMED STOP HOLE ON CRACK END. FABRICATED ESDR QXEA200600783Access Panel · corrodedPDX C4, LEFT HAND WING FUEL TANK ACCESS PANEL 524AT MATTING SURFACE HAS FRETTING CORROSION ON BOTH INBOARD AND OUTBOARD ENDS. REPAIRED IAW RD 8-57-320.SDR QXEA200600782Access Panel · corrodedPDX C4, LEFT HAND WING FUEL TANK ACCESS PANEL 524BT MATTING SURFACE HAS FRETTING CORROSION ON BOTH INBOARD AND OUTBOARD ENDS. REPAIRED IAW RD 8-57-320.SDR QXEA200600781Access Panel · corrodedPDX C4, LEFT HAND WING FUEL PANEL 524CT INBOARD END MATTING SURFACE HAS FRETTING (ENTIRE END). FUEL TANK ACCCESS PANEL FRETTING CORROSION ON ENTIRE INBOARD END. REPAIRED IAW RD 8-57-320.SDR QXEA200600780Skin · corrodedPDX C4, LEFT HAND WING FUEL TANK OPENING MATTING SURFACE FOR FUEL PANEL 524AT HAS A AREA OF FRETTING CORROSION AT OUTBOARD END. REPAIRED IAW RD 8-57-611, PAGE 11-3, STEPS 1-4.SDR QXEA200600758Panel · damagedYYC C4 LEFT HAND WING UPPER INBOARD REBATE FOR PANEL AT YW57 HAS THREE LOOSE RIVETS, FORWARD SPAR. REPLACED IAW DHC-8-200 SRM 51-40-11, PAGES 1-4.SDR USAA060445Skin · delaminatedSTA WBL 170-160 AND 181 UPPER FIXED WING T/E DELAMINATED. REMOVED DAMAGE AND APPLIED A COMPOSITE REPAIR IAW EA 78270, DEFECT SIZE: 3 INCHES.SDR QXEA200600755Skin · gougedYYC C4, RIGHT HAND OUTBOARD FLAP, GOUGE IN END LEADING EDGE. REPAIRED IAW RD 8-57-3320, PAGE 3 AND DHC-8-200 SRM 51-30-26.SDR QXEA200600720Fastener · looseYYC - C4 LEFT HAND WING BOTTOM TRAILING EDGE SKIN HAS LOOSE FASTENERS AT STATION YW 315. REPLACED IAW DHC-8-200 SRM 51-40-11, PAGES 1-4.SDR 06FDEA0987Skin · crackedRIGHT HAND WING NR 3 SLAT TELESCOPIC ANTI-ICE LEADING EDGE SPRING CUTOUT AREA UPPER CORNER CRACKED. CURRENT SRM REPAIR IS ONLY APPLICABLE FOR LOWER SURFACE AREA OF THE WING FIXED LEADING EDGE CUTOUT AREAS. COMPLIED WITH FEDEX EA 1-5740-94606.SDR QXEA200600722Skin · gougedYYC - C4 LEFT HAND WING UPPER SKIN HAS TWO GOUGES AT STATION YW 240. REPAIRED IAW DHC-8-200 SRM 51-20-11, PAGE 3, PARAGRAPH 2, 51-20-16, 51-20-36, 51-20-51 AND RD 8-57-3308, ISSUE 1. HORIZON AIR EA 2-57-351,SDR QXEA200600753Panel · corrodedYYC C4 , LEFT HAND UPPER WING PANEL 521AT HAS FRETTING CORROSION IN COUNTER SINK HOLES. REPAIRED IAW RD 8-57-1420, ISSUE 3.SDR AWXA200600574Skin · crackedMCN - DURING C16 CHECK DISCOVERED 2 EACH CRACKS, 0.375 INCHES, ON BOTTOM NR 1 SLAT SKIN BELOW INBD AUX TRACK AT WS 318.0L. MAINTENANCE CUTOUT DAMAGE AND FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. THEN INSTALLED FILLER ANDSDR QXEA200600682Panel · corrodedYYC C4, RIGHT HAND WING PANELS 622AT AND 623AT HAVE FRETTING CORROSION IN COUNTER SINKS. REPAIRED IAW DHC8 RD 8-57-1420, ISS 3 AND RD 8-57-1715, ISSUE 3.SDR 06FDEA0896Skin · wornLT 1R REF FOUND LE FWD WEAR ON SKIN. PERFORMED REPAIR DOUBLER IAW SRM 57-00-01 FIG 4 SHT 2 VOL 1 FABRICATED PART IAW SRM 57-00-01 FIG 4 AND DETAIL PART TRAVELER F166343/N00343.SDR QXEA200600754Skin · damagedYYC C4, RIGHT HAND WING BOTTOM SKIN, TRAILING EDGE AS WING STATION YW315.0 HAS NINE LOOSE RIVETS. REPAIRED IAW DHC-8-200 SRM 51-40-11, PAGES 1-4.SDR QXEA200600752Panel · corrodedYYC C4, LEFT HAND WING UPPER WING PANEL 522AT HAS FRETTING CORROSION IN COUNTER SINKS. REPAIRED IAW RD 8-57-1715, ISSUE 3.SDR QXEA200600756Skin · gougedYYC C4 - RIGHT HAND WING, TOP SURFACE, GOUGE AT WING STATION 765.00 JUST AFT OF NACELLE PANEL 623AT. REPAIRED IAW DHC-8-200 SRM 51-20-91, 51-20-16, 51-20-36, 51-20-51, PAGE 1-7 AND RD 8-57-8996, ISSUE 1.SDR QXEA200600698Access Panel · corrodedYYC C4 - RIGHT HAND WING FUEL BAY PANEL 624CT HAS AREA OF CORROSION INNER INBOARD END. REPAIRED IAW DHC8 RD 8-57-321, ISSUE 2 AND DHC8/200 SRM 51-20-16.SDR QXEA200600681Panel · corrodedYYC C4, RIGHT HAND WING TANK LID 624BT, FRETTING CORROSION ON INBOARD END OF LID AT INBOARD END OF TANK REBATE. REPAIRED IAW DHC8 RD 8-57-633, PAGE 2 AND 3.SDR QXEA200600751Panel · corrodedYYC C4, LEFT HAND WING UPPER WING PANEL 523ET HAS FRETTING CORROSION IN COUNTER SINKS. REPAIRED IAW RD 8-57-1420, ISSUE 3 AND DHC-8-200 SRM 51-20-16.SDR ASAA0610211Skin · chafedFOUND LT WING UPPER SKIN AT WBL 76.75 FM AFT EDGE OF SKIN FWD FOR 9.5" SKIN CHAFED. REPAIRED PER ERO 5279 AND EA 5720 01297.SDR ASAA0610214Skin · chafedFOUND LT WING UPPER SKIN CHAFED. REPAIRED PER ERO 5279 AND EA 5720 01297.SDR 06FDEA0836Skin · crackedLT WING T/E FOUND 1EA CRACK 0.25 INCH LONG ON SKIN OF ISLAND LOWER SKIN AT STA XORS 486. TRIMMED OUT DAMAGED AREA AND REPAIRED SKIN IAW SRM 57-00-01 FIG 4 SHT 2 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F176333-3 FILLER AND F176333-5 REPAIR DOUBLER ISDR 06FDEA0821Doubler · crackedLT WING L/E 2EA CRACK 1 INCH LONG INTERNAL DOUBLER AT STA XOS 589. PERFORMED REPAIR IAW SRM 57-10-00 FIG 71 VOL 1, FABRICATED PART IAW DETAIL PART TRAVELER NR N00374 AND IAW SRM 57-10-00 FIG 71 VOL 1.SDR 06FDEA0811Skin · crackedHFEC OPEN HOLE INSPECTION CARRIED OUT ON RT LOWER SKINS PANEL/ACCESS DOOR CUT-OUT BETWEEN STA XORS = 683.4 AND XORS = 713.6 - FASTENER HOLES FOUND CRACK INDICATIONS ON QTY: 02 EA. HOLES. REPAIR CARRIED OUT AS PER FEDEX E.A 1-5710-90773.SDR QXEA200600634Access Panel · chafedPDX- C4 CHECK, ROOT FAIRING ACCESS PANEL 262LT CHAFED RIGHT AFT CORNER. REPAIRED IAW RD 8-53-3366.SDR PIDA06023Fairing · crackedFAIRING ON TOP OF LEFT WING AT NR 3 FLAP TRACK HAS A CRACK AT THE FORWARD EDGE. REPLACED FAIRING PER SRM 51-00-05 AND 51-40-02.SDR CA060224001Skin · departedDURING TAKEOFF THE AIRCRAFT LOST THE RT INBOARD LEADING ASSY 611AR UPON ROTATION. THE LEADING EDGE SECTION REPORTEDLY BLEW OFF, AND OVER THE TOP OF THE WING AND CAME DOWN WITHIN THE AIRPORT BOUNDARY AREA TOWARDS THE END OF THE RUNWAY. THE AIRCRAFT WAS ABLE TSDR 06FDEA0675Skin · crackedRIGHT HAND WING FIXED LEADING EDGE TELESCOPING DUCT CUTOUT FOUND CRACKED. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE TELESCOPING DUCT CUTOUT CRACKED AREA AS PER FEDEX EA 1-5730-90745, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR DHL2006804541Skin · crackedRT WING LWR SKIN EXTERNAL FASTENER HOLE CRACKED 0.250 INCHES S-64 STA XRS 445.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SB 57-100 FIG. 5 SHEET 2. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SB 57-100 FIG. 5 SHEET 2. FABRICATED REPAIR DSDR QXEA200600525Skin · chafedYYC C3 LEFT HAND WING, WS 168 LOWER WING SKIN, TOP SIDE AT TRAILING EDGE IS CHAFED FROM OUTBOARD FLAP INBOARD ROLLER FITTINGS. REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01, SRM 51-25-16-001-001-A01, REO 57-51-089 AND HORIZON AIR EA R-57-140.SDR 06FDEA0598Skin · corrodedFOUND CENTER WING TANK LOWER SKIN PANEL HAS INTERGRANULAR CORROSION IN THE LEFT UPPER A/C PLENUM BETWEEN STA BS 795 AND 810 BETWEEN LBL 25 AND LBL 35. REMOVED ALL THE CORROSION,FABRICATED AND INSTALLED EXTERNA L REPAIR DOUBLER,2 EA INTERNAL REPAIR DOUBLESDR P5CA0601438Skin · corrodedWING CENTER SECTION UPPER SKIN CORROSION AT BS 1241 BETWEEN BBL 0 AND RBL 11.33. REPAIRED PER BOEING 8100-9 DATED 23JAN2006, PER EO-4757A238.SDR 06FDEA0541Skin · crackedFOUND LT WING L/E XOS 613 FOUND CRACK 1" LONG ON THE REFUEL DOOR VANE EXTERNAL SKIN. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 68 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163380/N00380.SDR 06FDEA0540Skin · crackedRT WING L/E FOUND CRACK 2" LONG ON EXT SKIN AT STA XORS 480. REPAIRED CRACK IAW SRM 57-10-00 FIG 68 SHT 2-3 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163612/N00612 AND IAW SRM 57-10-00 FIG 68 SHT 2 VOL 1.SDR EIA2006022Skin · corrodedDURING "B" CHECK, FOUND CORROSION ON THE RT WING LWR SKIN PNL AT WS 1371. REMOVED CORROSION TO RT LWR WING SKIN. THIS REPAIR IS LIMITED TO 135000 HOURS OR 38788 CYCLES WHICHEVER COMES FIRST. WAITING FOR FINAL REPAIR INFORMATIONSDR UPS06446381Skin · corrodedINSPECTION TYPE:C RT WING T/E CAVITY REAR SPAR LOWER SKIN FOUND CORRODED BETWEEN WS 510 & WS 515 (ACCESS FROM T/E PNL 671AB). CORROSION BLEND OUT 0.074 X 2 X 5 INCH EXCEED SRM LIMIT. RT WING T/E CAVITY REAR SPAR LOWER SKIN UPPER SURFACE AT WS 516.5 REPAIRED SDR EIA2006019Skin · corrodedCORROSION FOUND ON THE LT WING BETWEEN WS 1044 (LES 1054). INSTRUCTS TO REMOVE CORROSION, ACCOMPLISH NDI INSPECTION, CUT OUT THE DAMAGED WING SKIN MATERIAL AND FABRICATE REPAIR. THIS REPAIR IS LIMITED TO 135000 HOURS OR 38788 CYCLES WHICHEVER COMES FIRST.
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