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 IXXA07SMN128SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION, FOUND RT WING OUTBOARD SECTION LEADING EDGE HAS A NONE STANDARD REPAIR DOUBLER AT STATION XFS 710. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND AFTER NDT SDR IXXA07SMN127SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND NUMBER 1 STUB WING SKIN LOWER PART HAS A NON STANDARD REPAIR AT STATION XFS 562.5. REMOVED EXISTING NON STANDARD REPAIR. PERFORMED STOP HOLE ON CRACK END. FABRICATED EXTERNAL DOUBLER AND INTERNAL DOUBLER. PERFORMESDR IXXA07SMN123SSkin · crackedDURING ROUTINE C CHECK INSPECTION, RT WING OTBD L/E OUTER SECTION SHOWS 1" CRACKED AT STA XFS 885.000 (NEAR EXISTING REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 07110 DATE 03/14/07, SEMAN DRAWING NR ED-4463. DATE 02-15-07 AND EO SEMAN NR 2007221 DSDR IXXA070010SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING-EXTERNAL UPPER SKIN CRACKED AT STATION XRS74.000 STRINGER 14. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVESDR IXXA070009SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING-EXTERNAL UPPER SKIN CRACKED AT STATION XRS74.000 STRINGER 12. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVESDR EIA2007047Skin · corrodedRIGHT WING LOWER SKIN CORRODED ON UPPER SURFACE AT FSSO 1290 AT OUTBOARD JACKPAD. REMOVED CORROSION, NDT AREA, FABBED AND INSTALLED REPAIR PER ECRA 477-57-114-2SDR EIA2007046Skin · corrodedRIGHT WING FSSO 1528-1530 HAS AREA OF PREVIOUS CORROSION REMOVAL WHICH WAS OUT OF LIMITS AT UPPER SURFACE OF LOWER SKIN, FORWARD OF FRONT SPAR LOWER CHORD. REMOVED CORROSION, FABBED AND INSTALLED REPAIR PER ECRA 477-57-116-2.SDR EIA2007044Skin · corrodedRIGHT WING LEADING EDGE LOWER SKIN UPPER SURFACE CORRODED AT OLES/FSSO 1476-1490. REMOVED CORROSION, NDT'D AREA, FABBED AN INSTALLED REPAIR PER ECRA 477-57-117-2.SDR UIEA200700083Skin · corrodedRIGHT WING UPPER SURFACE WS 697, STR28R AT FRONT SPAR FOUND CORROSION. CORROSION REMOVED AND PROTECTED AS PER SRM 51-10-01 AND 51-10-02.SDR UIEA200700084Skin · corrodedLEFT WING UPPER WING SKIN AT WS320, STR 14L-14L FOUND CORROSION. CORROSION REMOVED AND PROTECTED AS PER SRM 51-10-01 AND 51-10-02.SDR UIEA200700081Skin · corrodedFOUND RIGHT WING UPPER SURFACE RWS642 AT MID SPAR FOUND CORROSION. CORROSION REMOVED AND PROTECTED AS PER SRM51-10-01 AND 51-10-02.SDR UIEA200700080Skin · corrodedFOUND LEFT WING UPPER WING SKIN AT WS 1280 FOUND CORROSION. CORROSION REMOVED AND PROTECTED AS PER SRM 51-10-01 AND 51-10-02.SDR 07FDEA00539Skin · crackedDURING HFEC OPEN, HOLE INSPECTION, QTY: 03 FASTENER HOLES REVEALED CRACK INDICATION FACING FORWARD OF RIGHT WING LOWER SKIN AT ACCESS DOOR AREA (APPROX XORS 696). CARRIED OUT REPAIR AS PER FEDEX E.A. 1-5710-107789, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-10SDR UHLA2007022100001Skin · damagedDEFORMATION OF STRUCTURE - LT WING LEADING EDGE SKIN DENTED AND TORN BEHIND BEHIND SLAT NR 1 AT I/B ATTACH POINT. UNSUPPORTED EDGES OF CUTOUT WERE BENT FORWARD. AN 8.25 INCH TEAR IN UPPERMOST EDGE OF CUTOUT WHERE IT WAS BENT UNTIL METAL RUPTURED, OUT OF LIMISDR UIEA200700074Skin · corrodedLEFT WING LEADING EDGE BULLNOSE FOUND CORROSION OUTBOARD OF LANDING LIGHT. PERMANENT REPAIRED ACCOMPLISHED AS PER BOEING MESSAGE 1-286780848-2 DATED 13 FEB,2007 AND EO NR 4757A281.SDR 07FDEA00509Skin · crackedFOUND CORROSION ON BOTTOM SKIN, MLG REINFORCING PLATE RT WING. NDT DETECTED A CRACK IN HOLE NR 552. REPAIR WAS PERFORMED IAW RAS/BAE/1003853/2006 ISS.: A AND EA 6-5720-103395.SDR ABXA070059Skin Panel · crackedCRACK ON RIGHT LOWER WING SKIN PANEL JUST FORWARD OF BUTE DOOR 1601. REMOVED AND REPLACED SKIN PANEL IAW DC9 SRM.SDR ABXA070060Skin Panel · crackedCRACK ON LEFT LOWER WING SKIN PANEL JUST FORWARD OF BUTE DOOR 1501. REMOVED AND REPLACED SKIN FORWARD OF BUTE DOOR IAW DC9 SRM 51-30-1, 51-30-2 AND 51-30-5.SDR UPS07M49200Paint · missingINSPECTION TYPE:N/A LEFT WING UPPER TRAILING EDGE SKIN HAS SEVERAL AREAS OF PAINT MISSING JUST INBD OF WINGLET. LEFT WING INBD SIDE OF WINGLET SKIN HAS SEVERAL AREAS OF PAINT MISSING COMPOSITE PANELS & T/E IS DELAMINATED. ITEM DEFERRED D344293. *S/D* REMOVSDR 07FDEA00497Skin · crackedLEFT WING ANTI-ICING TELESCOPING DUCT DOOR CUTOUT FOUND CRACKED. LT WING ANTI-ICING TELESCOPIC DUCT CUTOUT CRACK REPAIRED AS PER SRM 57-10-00 FIG. 42 VOL.I. (TR) REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.SDR 07FDEA00485Skin · misrepairedFOUND OLD CORROSION REPAIR ON UPPER WING SKIN LT, CLOSED TO RIB 5. REPAIR WAS VERIEFIED IAW RAS/BAE/0937/2004 ISSUE B AND CAL EO AB6-57-00-0057R1. THE REPAIR DIDN'T CORRESPOND WITH THE DOCUMENTS. THE REPAIR WAS ACCOMPLISHED IN THE FOLLOW DR 456.SDR WRNA200700034Rib · crackedDURING C-CHECK, THE LOWER RIB CORD OF NR 4 FUEL TANK ACCESS PANEL 652AB, WS 972 WAS FOUND CRACKED FROM RADIUS BLOCK TO RADIUS BLOCK. REMOVED LOWER RIB CORD IAW SRM 51-30-00, FABRICATED NEW RIB CORD IAW DRAWING 65B01073 AND INSTALLED RIB CORD IAW SRM 51-30-02SDR UPS07849367Skin · corrodedINSPECTION TYPE:C3 LEFT WING UPPER SKIN AT XW 408 TP CANT 508 BETWEEN STR 6 AND REAR SPAR REQUIRES REPAIR. REPAIR WING UPPER SKIN IAW SAA EA 008-5730-01-A0660 AND UPS EO DC8-5 730-26300-A.SDR UPS07849366Skin · corrodedINSPECTION TYPE:C3 LEFT WING UPPER SKIN AT XRS650 TO XRS659 OVER STR 7 REQUIRES REPAIR. REPAIR WING UPPER SKIN IAW SAA EA3 008-5730-01-A0655 AND UPS EO DC8-57 30-26300-A.SDR UPS07849365Skin · corrodedINSPECTION TYPE:C3 LEFT WING UPPER SKIN AT CANT 495 TO XW408 OVER CENTER SPAR REQUIRES REPAIR. REPAIRED WING UPPER SKIN IAW SAA EA 008-5730-01-A0659 AND UPS EO DC8-5730-26300-A.SDR UPS07849364Skin · corrodedINSPECTION TYPE:C3 LEFT UPPER WING SKIN AT CANT 495 TO XRS 554 BETWEEN STR 5 AND 8 REQUIRES REPAIR. REPAIRED UPPER WING SKIN IAW SAA EA 008-5730-01-A0658 AND UPS EO DC8-5730-26300-A.SDR UPS07849363Skin · corrodedINSPECTION TYPE:C3 LEFT UPPER WING SKIN AT XRS 589 BETWEEN STR 1 TO REAR SPAR REQUIRES REPAIR. REPAIRED WING UPPER SKIN IAW SAA EA 008-5730-01-A0656 AND UPS EO DC8-5730-26300-A.SDR UPS07449350Skin · crackedINSPECTION TYPE:C LEFT WING UPPER SURFACE I/B LEADING EDGE SKIN FOUND CRACKED AT WS 450 AFT NR 12 K/FLAP. LEFT WING UPPER SURFACE LEADING EDGE SKIN REPAIRED AS PER SRM 57-30-04 FIG 2.SDR 213200744ASSkin · damagedPULLED FASTENERS AND CRACK IN LT WING LOWER SKIN.SDR CA070222002Skin · dented(CAN) CREW REPORTED BIRDSTRIKE ON APPROACH, MAINTENANCE INSPECTION FOUND DENT IN LT WING LEADING EDGE APPROX 6 FT OB FROM FUSELAGE. DENT ALLOWABLE IAW SRM LIMITS. (TC NR 20070222002)SDR UPS07849344Skin · crackedINSPECTION TYPE:C3 LEFT WING UPPER SKIN 1 INCH CRACK AT XRS 107.000 UPPER FRONT SPAR SKIN. REPAIRED UPPER WING SKIN AT XRS 107.000 FRONT SPAR IAW SAA EA 008-5710-01-A0685 AND UPS RAA DC8-57-20211.SDR NWAA070729984Panel · crackedDURING "L" CHECK, FOUND CRACK IN LT WING LEADING EDGE PANEL NR 1590 APPROXIMATELY 4 INCHES AFT OF NR 3 FLAP HINGE. REPAIRED PER EA 99-208468.SDR C4S2007F00000Skin · corrodedDURING A WING INSPECTION ACCOMPLISHED APRIL 9, 2006, CORROSION WAS NOTED IN THE UPPER RT WING PLANK AT FS 452 AND BL33. THE CORROSION DID NOT REQUIRE REPLACEMENT OF THE PART AND DID NOT REQUIRE BLENDING THAT EXCEEDED THE MFG ALLOWANCES. MFG ENGINEERING ALLOWSDR UPS07449485Panel · delaminatedINSPECTION TYPE:C LEFT WING I/B MID FLAP UPPER PANEL 577LT INTERNAL FOUND DELAMINATION. LEFT WING I/B MID FLAP UPPER PANEL 577LT REPAIRED AS PER RS R57-55-35711 AND US EO B747-5730-15355.SDR DHL2007802536Access Door · delaminatedRT WING T/E UPPER ACCESS DOOR NR 510 DELAMINATED (XA 475.000 - 507.000). REMOVED AND REPLACED DELAMINATED ACCESS DOOR NR 510 RT WING T/E IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).SDR TRAX200700208Skin · crackedRIGHT WING PLANK CRACKED ON WS 148 COMMON TO AFT SPAR FLANGE. PERFORMED REPAIR ON R/H LOWER WING PLANK AFT AT WS 148.019, IAW REO 601R-57-21-130. (EMP 752 - INSP RA333) ALL WORK DONE IAW ASA EO 600-57-13402. (EMP 818 - INSP RA189) FUEL LEAK CHECK REQUIRED. LESDR 07FDEA00426Skin · corrodedL/T WING BOTTOM SKIN UPPER SURFACE CORROSION ADJACENT TO HYD PRESSURE LINE THROUGH HOLE. AREA WHERE HYD LINE AT WING T/E PASS THROUGH TO NR 1 PYLON. AFTER CORROSION REMOVAL, HYDRAULIC LINE PASS, THROUGH HOLES WERE FOUND TO BE ELONGATED. HYDRAULIC BULKHEAD FSDR G60A200800011Skin · corrodedFOUND CORROSION LEFT WING DROOP LEADING EDGE INBD UPPER SKIN.SDR AALA20070648Skin · wornAFW - LEFT WING LOWER SKIN SURFACE AT APPROXIMATELY WING STATION 602 AND JUST AFT OF STRINGER 66 UNDER FAIRING FOR OUTBOARD FLAP HAS TWO WORN AREAS. AREA OF DISCREPANCY IS 0.7 INCHES BY 1.0 INCHES AND 7 INCH DIAMETER WITH .005 DEPTH. BLENDED AREA UNTIL SMOOTSDR IXXA07SMN103SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD LEADING EDGE OUTER SECTION HAS A NON STANDARD REPAIR, BETWEEN STATION XFS 710.000 AND XFS 716.250. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK SDR IXXA07SMN096SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE SLOT VANE UPPER SKIN HAD NON STANDARD REPAIR AT STATION XS 520.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. SDR EIA2007050Skin · corrodedRIGHT WING LEADING EDGE SKIN CORRODED ON UPPER SURFACE AT FFSO 1405. REMOVED CORROSION, NDT'D AREA, FABBED AND INSTALLED REPAIR PER B747 57-30-03 PAGE 9-13.SDR 07FDEA00377Skin · damagedON LT WING LOWER SKIN PANEL AFT FROM PYLON NR 1 ARE ELONGATED HOLES ON HYDRAULIC FITTINGS. REPAIR WAS PERFORMED IAW RAS/BAE/1003815/2006 ISSUE: A, APPROVED BY EA 6-5720-103392.SDR A6WA200740056Skin · corrodedRT WING LOWER PLANK FUEL ACCESS PANEL 640AB HOLE NR 4 AT WS 54.681 HAS MINOR CORROSION ON AFT FLANGE APPROX .003 INCH DEEP AND 3 INCHES LONG IN CRITICAL AREA. MAINTENANCE REPAIRED FUEL WING PLANK CUTOUT HOLE NR 4 (640AB) IAW REO 601R-57-21-030 REV (F).SDR DHL2007802530Panel · delaminatedLT WING T/E LWR PANEL DELAMINATED (STA XW 97.000 - XRS 162.000). REMOVED AND REPLACED LT WING T/E LWR PANEL IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).SDR 07FDEA00347Panel · gougedRT WING INBD TE LWR SURFACE PANEL JUST OB OF MLG FWD TRUNNION, DELAMINATED ON UPPER SURFACE FWD EDGE. OIL SOAKED REMOVED DAMAGED PANEL ASSY. TRIED TO REMOVE DAMAGE REF SRM 51-40-9 PG 4 AND DAMAGE WAS MORE THEN 25% OF PANEL, BEYOND REPAIRABLE LIMITS REF SRM SDR UIEA20070067Skin · corrodedRIGHT WING LOWER SKIN FOUND WITH CORROSION JUST INBOARD OF OUTBOARD MIDSPAR FUSE PIN FITTING OF NR 4 PYLON. CORROSION ON SAID WING LOWER SKIN REMOVED PER SRM 51-10-00. HFEC ACCOMPLISHED, NO DEFECTS. SKIN SHOT PEENED AND REPROTECTED.SDR GLBA20060890Skin · damagedRT WING SKIN TRAILING EDGE RIVETS LOOSE AND RIVET HOLES ELONGATED AT TRAILING EDGE BETWEEN WS 124.6 TO WS 136.6.SDR 07FDEA00328Skin · corrodedOLD REPAIR ON LT/RT OUTBOARD WING TIP UNDERNEATH STATIC DISCHARGER. REPAIR WAS PERFORMED IAW RAS/FOK/247/2000 ISSUE B.SDR 07FDEA00261Skin · corrodedOLD CORROSION REPAIR ON LT OUTER WING, BOTTOM SKIN, NEAR RIB 21 REPAIR WAS PERFORMED BY BLEND OUT THE CORROSION WITH CAL EO AB 6-57-00-0023 AND APPROVED BY RAS/BAE/0701/2003 ISS.A AND EA 6-5720-106353.
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