JASC 5740
Service difficulty reports · 3,003
Reports filed under 5740 · Wing, Attach Fittings, 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 = '5740' 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 = '5740' 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 FDEA202609231416Attach Fitting · crackedLEFT WING- LEADING EDGE COMPARTMENT ATTACH FORMER XOS 939 FOUND CRACK ABOUT 0.6 INCHES. LEFT HAND WING LEADING EDGE COMPARTMENT CRACKED FORMER AT XOS 939 REMOVED IAW SRM 51-33-01-0G AND MD-11 SRM 51-35-01-06. FABRICATED FORMER PER DRAWING ARB 1292 REVISION SDR HYIA20260923002Fitting · corrodedDURING SCHEDULED WING FITTING INSPECTION, A SMALL AREA OF CORROSION WAS VISUALLY IDENTIFIED ON THE LEFT HAND FORWARD UPPER WING ATTACH FITTING. THIS CORROSION MEASURES APPROXIMATELY .500 INCHES LONG, .125 INCHES WIDE, AND .020 INCHES DEEP ON THE TOP FACE OF THSDR IPXA2026092172110Bracket · crackedCRACKED BRACKET, LT WING INBD SLAT TORQUE TUBE SUPPORT AT INBD L/E CAVITY AT ISS 285.233. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO. 114T1240 SH. 6 REV. -.SDR SWAA2026101693391Nut Plate · corrodedCORROSION RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE OFSS 449 LT WING. REPLACED THE RAIL NUT PLATES IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 112A4402, SHEET 40, REV A.SDR SWAA2026090760777Attach Angle · crackedRIGHT WING UPPER SHELF PANEL, ATTACH ANGLE CRACKED INBD AND ABOVE NR 2 AFT BOOST PUMP. REMOVED & REPLACED THE ATTACH ANGLE IAW SRM 51-40-02.SDR DALA2026082604845Bushing · migratedLEFT RIB 6 FITTING FWD LUG ECCENTRIC PIN BUSHING MIGRATED. CORRECTED IAW ERA 635960-14 REV ORIGINAL. (1777705) AIRCRAFT WAS GROUNDED.SDR SWAA2026092313059Nut Plate · crackedCRACKED NUT PLATE, OFSS 604, INTERNAL CAVITY LEADING EDGE, RT WING. REPLACED THE NUT PLATE BTWN OSS 362.51 - 384.24. IAW SRM 51-40-02, & DWG 112A4402, SHEET 14, REV-.SDR SWAA2026092106314Nut Plate · crackedCRACKED NUT PLATE, OFSS 404, INTERNAL CAVITY L/E OF LT WING. REPLACED THE NUT PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 112A4402, SHEET 40, REV A.SDR SWAA2026092127237Nut Plate · crackedCRACKED RAIL NUT PLATE LOC OFSS 570, INTERNAL CAVITY LEADING EDGE OF RT WING. REMOVED THE NUT PLATE IAW SRM 51-40-01 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREAS AND DID NOT FIND OTHER DAMAGE. REPLACED THE NUT PLATE IAW SRM 51-40-01, SRM 51-40-02, SRM SDR SWAA2026092130117Nut Plate · crackedCRACKED RAIL NUT PLATE, OFSS 491 INTERNAL CAVITY LEADING EDGE IN THE RT WING. REPLACED RAIL NUT PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 112A4402, SHEET 40, REV A.SDR SWAA2026092127663Nut Plate · crackedCRACKED RAIL NUT PLATE, OFSS 588 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT PLATE IAW SRM 51-40-02-0G-0, & DWG 112A4402, SHEET 13, REV-.SDR SWAA2026092109501Nut Plate · crackedCRACK RAIL NUT PLATE LOC OFSS 449 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED THE NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG:112A4402, SHEET 40, REV A.SDR SWAA2026081997521Attach Bracket · crackedRIGHT WING INBD FIXED T/E PANEL SUPPORT BEAM, FWD ATTACH BRACKET CRACKED. REMOVED AND REPLACED RT WING INBD FIXED T/E PANEL SUPPORT BEAM FWD ATTACH BRACKET IAW SRM 51-40-02.SDR HYIA20260731001Fitting · crackedDURING SCHEDULED WING FITTING INSPECTION 2 CRACKS WERE VISUALLY IDENTIFIED IN THE LOWER RADIUS OF THE RIGHT SIDE LOWER AFT WING ATTACH FITTING (OEM: 0822550-44). THE INBOARD CRACK MEASURES APPROXIMATELY 2.750 INCHES LONG AND THE OUTBOARD CRACK MEASURES APPROXISDR SWAA2026080334290Attach Angle · crackedLEFT WING TRAILING EDGE OTBD ATTACH ANGLE AT TRANSVERSE WEB ABOVE NR 1 AFT PYLON TIP CRACKED. REMOVED AND REPLACED LEFT WING TRAILING EDGE OTBD ATTACH ANGLE AT TRANSVERSE WEB ABOVE NR 1 AFT PYLON TIP IAW SRM 51-40-02 AND AIPC 57-42-51-03.SDR CALA2026071317731Bracket · crackedRIGHT WING ABOVE 651GB,FIXTURE PANEL HAS BRACKET CRACKED THAT ATTACHES TO FLAP DEFLECTION FITTING. REMOVED AND REPLACED RH WING,FIXTURE PANEL BRACKET IAW B737 SRM 51-40-02 AND BAC DWG# 115A6200 REV:B DOT REMOVED.SDR HNAA2026082400747Attach Fitting · chafedF138484 LT WING NR 1 LEADING EDGE INTERNAL INBD ATTACHMENT FLANGE IS CHAFED. REMOVED DAMAGE FROM LT WING NR 1 LEADING EDGE INTERNAL INBD ATTACHMENT FLANGE (LOWER SURFACE) IAW SRM 51-10-03. FOUND TO BE WITHIN ALLOWABLE LIMITS IAW ETD 2026-145-013669 REV: A, ASDR IPXA2026081116351Bracket · crackedLEFT WING, BRACKET WITH CRACK AT FIXED LEADING EDGE (INTERNAL STRUCTURE) INSIDE THE FLAP KRUEGER COMPARTMENT. INSTALLED NEW ANGLE ON WING INBOARD SECTION, LOWER SURFACES IAW SRM 51-40-21.SDR SWAA2026072764870Attach Angle · crackedLEFT WING TRAILING EDGE TRANSVERSE WEB ABOVE #1 PYLON AFT TIP O/B ATTACH ANGLE CRACKED. REMOVED AND REPLACED LEFT WING TRAILING EDGE TRANSVERSE WEB ABOVE #1 PYLON AFT TIP O/B ATTACH ANGLE IAW SRM 51-40-02. VERIFIED CORRECTIVE ACTIONSDR FXTA20260628001Bolt · looseFLAP ACTUATOR ATTACHMENT HARDWARE FOUND LOOSESDR ECPR202606004Bracket · corrodedTHE RIGHT WING CENTER FLAP HINGE BRACKET WAS FOUND WITH CORROSION PITTING THAT WAS BEYOND REWORK LIMITS NECESSITATING THE REPLACEMENT OF THE BRACKET. THE ORIGIN OF THE CORROSION WAS THE BONDING WIRE ATTACHMENT POINT.SDR AALA202608075316Attach Fitting · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD FLAP NTERCONNECTING STRUT ATTACH FITTING WORN - REPLACED ATTACH FITTING PER SRM 51-42-11.SDR ECPR20260624001Bracket · corrodedTHE LEFT WING CENTER FLAP HINGE BRACKET WAS FOUND WITH CORROSION PITTINING THAT WAS BEYOND REWORK LIMITS NECESSITATINING THE REPLACEMENT OF THE BRACKET. THE ORIGIN OF THE CORROSION WAS THE BONDING WIRE ATTACHMENT POINT.SDR SWAA2026072471735Nut Plate · corrodedCORRODED RAIL NUT PLATE, OFSS 449 RT WING LE. REPLACED RAIL NUT PLATE AND FASTENERS IAW SRM 51-40-02-0G, AND DWG 112A4402, SHEET 40, REV A. CORROSION WAS NOT FOUND ALLOWABLE, DAMAGE IAW SRM.SDR IPXA2026061904932Bracket · crackedCRACKED BRACKET, LT WING L/E INBD PANEL 511KB TORQUE TUBE SUPPORT LES 281. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 114T1240 SH 4 REV: D.SDR 2026F00127Nut Plate · corrodedLEFT MLG WHEEL WELL HAS 6 NUTPLATES WITH EVIDENCE OF CORROSION LOCATED AROUND 6 NUTPLATES WHERE ACCESS PANEL 512DB ATTACHES. REPAIRED CORRODED PANEL LAND COMMON TO PANEL 512DB PER AQRD RFTS-117476 REV.0 TITLE "N576QS (560-5708) PANEL 512DB NUTPLATE CORROSION";SDR FDEA202606160765Not Reported · not reportedWRI 57-40-5108 FACTED IN ERROR. EA: F-5740-T0387288 P1. CREATED WRI 5740-5115 FOR SDR OF WRI 5740-5108 BEING FACTED IN ERROR. REF MAJOR REPAIR E.A. F-5740-T0387288 P1.SDR IPXA2026061548249Bracket · crackedCRACKED BRACKET, RT WING INBD SLAT TORQUE TUBE SUPPORT AT INBD L/E CAVITY, ISS 285.233. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV. 95 AND DWG NO. 114T1240 SH. 6 REV. -.SDR ABXR2026060400010Angle · crackedRIGHT WING L/E #9 SLAT AREA INTERNAL ANGLE CRACKED AT LOWER FWD WEB LOWER ANGLE. LES668. FABRICATED NEW ANGLE IAW B767 SRM 57-41-13 REPAIR 1SDR IPXA2026061694292Angle · crackedLEFT WING, FIXED L/E, INBD SIDE, INTERNAL STRUCTURE, JUST NEXT TO KRUEGER FLAP COMPARMENT, ANGLE WITH A CRACK 1/2 LONG. REMOVED ANGLE WITH CRACK IAW SRM 51-40-21. INSTALLED ANGLE IN LT WING, FIXED L/E, INBD SIDE, INTERNAL STRUCTURE IAW SRM 51-40-21.SDR KCSA202606021044Attach Fitting · corrodedLEFT INBD FOREFLAP INBD CARRIAGE ATTACHMENT FITTING HAS CORROSION.SDR AALA202605286613Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT STA 663.5 AND LBL 9. REPAIRED ANGLE PER SRM 57-10-10-2R-5.SDR IPXA2026053056047Attach Bracket · crackedCRACK - BRACKET, L/H WING INBOARD L/E COMPARTMENT. (REPLACE) INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 114T1240 SH. 6 REV. -.SDR IPXA2026053056997Attach Bracket · crackedRIGHT WING INBOARD L/E CAVITY, PANEL RIB ATTACH BRACKET CRACK, ISS 285. (REPLACE) INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 114T1240 SH. 6 REV. -.SDR SWAA2026062206215Fitting · crackedCRACKED LOWER SURFACE AROUND FASTENER ON LEFT WING ACTUATOR FITTING SLAT 4. PERFORMED A PERMANENT REPAIR ON THE NOSE SKIN SLAT 4, LT WING IAW SRM 57-42-01-2R-8, REPAIR 8, & SRM 51-40-02.SDR AALA202605222750Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPA VAPOR BARRIER ATTACH ANGLE AT BS 663.5 AND RBL 2. REPLACED ANGLE PER SRM 57-10-10-R2-5.SDR IPXA2026051880648Bracket · crackedCRACKED BRACKET, RT WING INBD L/E CAVITY TORQUE TUBE SUPPORT BRACKET. REMOVED DAMAGED BRACKET IAW SRM 51-40-02-0G, REV.95. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND DWG 114T1240, SH 6, REV-.SDR SWAA2026060103789Fitting · crackedREMOVE AND REPLACE SLAT NR 8 DUE TO CRACKED ACTUATOR FITTING. REPLACED LEADING EDGE SLAT 8 AT RT WING IAW AMM 27-81-21-401. TESTED OK.SDR CALA2026051116126Bracket · corrodedLEFT T/H WHEEL WELL PTU BRACKET HAS EXFOLIATION. REMOVED AND REPLACED BRACKET AT LH WHEEL WELL PTU IAW SRM 51-10-02 AND 51-40-02.SDR SWAA2026060195830Fitting · crackedCRACK LOWER SURFACE OF LEADING EDGE SLAT 8 NOSE SKIN AT ACTUATOR LOC. AROUND FASTENER AT RT WING. SLAT 8 HAS BEEN REPLACED BECAUSE THE ACTUATOR FITTING WAS FOUND TO BE CRACKED IN TWO HOLES DURING THE ROTO TEST INSPECTION FOR SLAT REPLACEMENT.SDR SWAA2026051192311Attach Angle · crackedRIGHT WING TRAILING EDGE PANEL 651FB FWD ATTACH 'L' ANGLE CRACKED.<[01] REMOVED AND REPLACED RIGHT WING T/E PANEL 651FB FWD ATTACH 'L' ANGLE PER SRM 51-40-02; AND IPC 57-50-00-38.;[02] VERIFIEDSDR 2026F00081Nut Plate · corrodedFOUND 6 AREAS OF CORROSION AROUND NUT PLATES FOR PANEL 652DB, MECHANICALLY REMOVED 6 AREAS OF CORROSION WHERE 6 NUTPLATES LOCATED INSIDE RH WING ACCESS BAY 652DB WERE REMOVED IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNA 68SDR 2026FA0000286Attach Plate · misaligned8 EACH HOLES THROUGH THE YAW PLATE/WING ATTACH FITTING WERE NOT DRILLED PERPENDICULAR TO THE CONTOUR OF THE STRUCTURE CREATING A NONSHEAR CONDITION FOR THE FASTENER INSTALLATION. THESE HOLES WERE REQUIRED TO BE OVERSIZED BEYOND SRM LIMITATIONS TO CREATE A SHEASDR IPXA2026042563692Hinge · wornFOUND NR 8 TAI DOOR AFT HINGE WORN OUT. IAW AMM 57-41-58-434-044, ADJUSTED AND PERFORMED A BONDING TEST OF NR 8 TAI DOOR AFTER HINGE,RESULT WAS SATISFACTORY.SDR SWIA2026040976354Fitting · gougedLEFT WING REAR SPAR AT WS162.49 HAS A FITTING GOUGED & DAMAGED. REMOVED, REPLACED, AND INSTALLED FITTING ON LT WING REAR SPAR AT WS 162.49 IAW SRM 57-51-14,51-40-11,51-21-11,51-25-06,51-25-16,51-42-06, & 51-42-20,51-23-00.SDR SWAA2026050587998Attach Angle · crackedLEFT WING TRAILING EDGE ATTACH ANGLE FOR OTBD END OF TRANSVERSE WEB CRACKED. REMOVED AND REPLACED LEFT WING TRAILING EDGE ATTACH ANGLE FOR OTBD END OF TRANSVERSE WEB IAW SRM 51-40-02-0G-0.SDR HNAA2026042100321Attach Fitting · gougedF111356 LH AILERON DAMPER ATTACHMENT FITTING IS GOUGED 2 EACH. RAR LH AILERON DAMPER ATTACHMENT FITTING IAW EMB 145 SRM 51-40-02SDR IPXA2026041094730Bracket · crackedCRACKED TORQUE TUBE SUPPORT BRACKET, RT WING L/E COMPARTMENT ACCESS PANEL 611LB. INSTALL A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, & DWG 114T1240, SHT 6, REV -.SDR SWAA2026051187258Attach Angle · crackedHFEC VERIFIED BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED APPROX. RBL 9. REMOVED ALL FASTENERS ON R/H VERTICAL FLANGE IN REPAIR AREA STA 663 RBL 5 TO RBL 16 IAW SRM 57-10-10-2R-5. CUT AND REMOVED DAMAGED SECTION OF RH VAPOR BARRIER ATTACH ANGLE FROM RBL 5 TOSDR CALA2026041415343Bracket · crackedRIGHT WING LOWER ATTACH BRACKET HOLE NO.6 AS MARKED ON AIRCRAFT IS CRACKED REMOVED AND REPLACED BRACKET PER APB DWG 757-340 REV B AND B757-200 SRM 51-40-02
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