JASC 5753
Service difficulty reports · 31,493
Reports filed under 5753 · Trailing Edge Flaps, 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 = '5753' 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 = '5753' 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 LR7A2026061903837Skin · crackedDURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5712, FOUND RT INBOARD FLAP UPPER CENTER SKIN CRACKED AT CWS121R. REPAIRED IAW SMP583 SRM, FIGURE 51-140-12.SDR LR7A2026061903836Skin · crackedDURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5712, FOUND RT INBOARD FLAP UPPER SKIN TRAILING EDGE CRACKED AT CWS150R. REPAIRED IAW SMP583 SRM, FIGURE 51-140-12.SDR DALA2026061903679Hinge Fitting · corrodedCORROSION LEVEL 2 IN FASTENERS HOLES HOLDING 8 EAS LT WING FLAP INNER HINGE. LT WING FLAP INNER HINGE WAS REPLACED PER SERVICEABLE INNER HINGE IAW AMM 57-55-25. (LP 1654540 - AIRCRAFT WAS GROUNDED).SDR IPXA2026082731916Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. THREE CRACKS NOTED AT RIB 26. MAJOR REPAIRSDR FDEA202606180929Flap · crackedRH WING CENTER FLAP FOUND 1EA CRACK AT RIB26 FIRST FASTENER BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA 6-5750-T0362465 A P2, EA TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP, CRACK IN UPPER FLANGE OF RIB 26 & 27. REMOVED THE EXISTING DOUBLER ON BOTTOM SSDR IPXA2026063033532Skin · corrodedLEFT WING INBD FLAP HAS CORROSION AT T/E OTBD UPPER SURFACE.SDR IPXA2026063024575Tail Cone · debondedNR 7 FLAP TRACK AFT TAIL CONE, LOWER SKIN FOUND TAPE APPLY. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2" AROUND HEATED AREA , IAW NDT MANUAL PART 1 51-01-01 REV:182. NO DEFECT WAS FOUND. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 SDR IPXA2026062923795Seal · brokenBROKEN MOLDING SEAL, LT WING NR 3 V.C FLAP INBD SIDE CORD MOLDING. IAW SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR.SDR IPXA2026062924546Seal · damagedNR 22 V.C FLAP INBOARD MOLDING SEAL DAMAGE. IAW SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR.SDR IPXA2026062924655Seal · brokenBROKEN- MOLDING SEAL, L/H WING NO.1E V.C FLAP INBD SIDE MOLDING. IAW SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIRSDR IPXA2026062924669Seal · brokenBROKEN- MOLDING SEAL, L/H WING NO.9 V.C FLAP INBD SIDE MOLDING. IAW. SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS BELOW. REMOVE THE RAIN EROSION SHIELDS AND CLEAN. APPLY THE SEALANT TO REPAIR AREA CURED AT 70 F FOR 48 HOURSSDR IPXA2026062102849Skin · crackedCRACKED SKIN, LT WING T/E NR 3 FLAP AFT FAIRING INBD. (REPAIR) IAW NDT MANUAL PART 1, 51-01-01 & PART 4, 51-00-03, REV.143 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA WAS HOT PLUS WITHIN 6 INCHES ALL AROUND. RESULT: NO DEFECT FOUND.SDR REXA2026082601722Plate · chafed" WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH/RH WING TRAILING EDGE. FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH/RH WING TRAILING EDGE WERE REPLACED PER CRJ 900 SRM 51-42-21-001-001-ASDR REXA2026082601721Fitting · chafed" WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH/RH WING TRAILING EDGE. FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH/RH WING TRAILING EDGE WERE REPLACED PER CRJ 900 SRM 51-42-21-001-001-ASDR REXA2026082601720Fitting · chafed" WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH/RH WING TRAILING EDGE. FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH/RH WING TRAILING EDGE WERE REPLACED PER CRJ 900 SRM 51-42-21-001-001-ASDR SWAA2026071637897Angle · crackedCRACKED ANGLE TRAILING EDGE LOCATED IRSS 140 UPPER POSITION AT RT WING. REPLACED ANGLE TRAILING EDGE LOCATED IRSS 140 UPPER POSITION AT RT WING IAW SRM 51-40-02-0G-0 & DWG:115A2000; SHEET 22, REV A. MEASUREMENT OF CRACK IS: 1.495 IN.SDR SWAA2026062312885Skin · delaminatedDELAMINATION ON INBOARD CORNER ON AFT FLAP OUTBOARD LT WING. EVALUATED DAMAGE ON INBOARD CORNER OF OUTBOARD AFT FLAP AT LT WING IAW SRM 57-53-01-2R-16. FOR REMOVE AND INSTALL AFT FLAP OUTBOARD LT WING PROCEDURE SEE TTG8Q01CRW1PSDR LR7A2026061603827Skin · crackedDURING SCHEDULED B-2 CHECK WHILE PERFORMING SP-157, FOUND LT OUTER WING FLAP BAFFLE UPPER FORWARD SKIN CRACKED AT OWFS0L. REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR 1001386070.SDR LR7A2026061603826Fitting · crackedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HB2703, FOUND RT OUTER WING TRAILING EDGE FLAP TRACK FITTING CRACKED AT OWFS241.6R. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR 1001385898.SDR IPXA2026061860062Flap Track · crackedCRACK - SKIN, R/H WING NO.6 FLAP TRACK MID FAIRING INBD SIDE T/E SKIN. (REPAIR) I.A.W. B767 NDT MANUAL PART 1, 51-01-01 AND PART 4, 51-00-03, REV.143 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA WAS HOT PLUS WITHIN 6" ALL AROUND. NO DEFECT FOSDR SWAA2026071783960Flap · crackedCRACK INDICATION ON RT OTBD AFT FLAP INBD CARTRIDGE RADIUS ZONE. EVALUATED OTBD AFT FLAP INBD CARTRIDGE AND DID NOT FIND ALLOWABLE DAMAGE IAW SRM 57-53-02-1A-4 AND REPLACED OTBD AFT FLAP AT RT WING IAW AMM 27-51-26/401. INSTALLATION IS DOCUMENTED ON TTG8Q01SDR SWAA2026071607247Rib · crackedCRACK INDICATION ON LT OTBD AFT FLAP INBD CARTRIDGE RADIUS ZONE.CRACK LENGHT 0.250 IN APPROX. LEFT WING. REPLACED OTBD AFT FLAP INBD CLOSURE RIB LT WING IAW SRM 51-10-02, ITEM 9; FOR CARTRIDGE ASSEMBLY INSTALLATION SEE TTG8Q01BR3XMSDR SWAA2026071600476Rib · crackedCRACK INDICATION ON RT OTBD AFT FLAP INBOARD CLOSURE RIB RADIUS ZONE.CRACK LENGHT 0.250 IN APPROX. RIGHT WING. EVALUATED OTBD AFT FLAP INBD CLOSURE RIB (CARTRIDGE) RT WING AND NOT FOUND ALLOWABLE DAMAGE IAW SRM 57-53-02-1A-4 AND REPLACED OTBD AFT FLAP AT RT WISDR JGVR20260612201Flap Track · wornFOUND WEAR AND GOUGES ON LH AND RH WING FLAP INBOARD AND OUTBOARD TRACKS, REMOVED FASTENERS AS REQUIRED, BLENDED AREAS SMOOTH, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED AND TREATED AREAS AND REINSTALLED FASTENERS PER NETJETS REQUEST FOR TECHNISDR VNAA202607280001Skin · nickedSEVERAL NICKS ON LOWER SKIN OF RT - LT INBD FLAP FLS 15.5 TO FLS 75.5. LOWER SKIN OF RT - LT INBD FLAP FLS 15.5 TO FLS 75.5 WERE REPAIRED IAW SRM 57-52-01-201-005-A01.SDR SWAA2026072093453Wedge · debondedLEFT INBD MID FLAP OTBD T/E WEDGE TRAILING EDGE, DISBONDED. REMOVED AND REPLACED LEFT, INBD MID FLAP OTBD T/E EDGE WEDGE IAW SRM 51-40-02-0G-0, CMM 20-50-11-910-801, SRM 51-40-05-0G-0, AND DWG 113A2100, REV C, AND AMM 51-31-00.SDR CALA2026061217056Skin · dentedLEFT WING, INBD MAIN FLAP, UPPER SURFACE BY MFS 105 HAS A DENT. REPAIRED DAMAGED AREA IAW SRM 51-70-10-2R-2.SDR IPXA2026061612251Skin · dentedDENTED SKIN, LOWER FACE OF LT WING T/E OUTBD FLAP T/E LOWER SKIN, WBL 373. IAW AMM 51-21-10-307-020 REV.148, REPAINT REWORK AREA.. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR FDEA202606110724Skin · puncturedSECONDARY FINDING, PUNCTURE ON HONEYCOMB OF THE RIGHT OUTBOARD FLAP AT UPPER PANEL, OTEF 89.25 AND 9" FROM LEADING EDGE HONEYCOMB OF THE RIGHT OUTBOSRD FLAP AT UPPER PANEL, OTEF 89.25 AND 9" FROM LEADING EDGE WAS REPAIRED IAW B767 SRM 57-53-01-1A AND SRM 5SDR FDEA202606110711Skin · delaminatedDELAMINATION ON L. EDGE SKIN AT 20" FROM OUTB EDGE. RH INB MAIN FLAP L. EDGE SKIN AT 20" FROM OUTB EDGE RH INB MAIN FLAP WAS REPAIRED IAW B767 SRM 57-53-01- 2R FIG 201 REP 1 SHEET 5 AND 51-70-17-0G REV 94 DEC 15/2025SDR FDEA202606110710Skin · delaminatedDELAMINATION ON L. EDGE SKIN AT 32" FROM OUTB EDGE. RT INBD MAIN FLAP L. EDGE SKIN AT 32" FROM OUTB EDGE RH INBD MAIN FLAP WAS REPAIRED IAW SRM 57-53-01-2R AND 51-70-17-0G, REV 94. DEC 15/2025SDR FDEA202606110701Skin · delaminatedLHW OB FLAP LWR SURFACE 265IN FROM IB EDGE, 10IN FROM LWR EDGE FOUND DELAMINATION. REPAIRED LHW OB FLAP LWR SURFACE DELAMINATION AT OTEF STA 281 AS PER B777 SRM 57-53- 01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4 FIGURE 210 REV 53.0 AND EA: G-5750- TSDR AALA202607226500Skin · debondedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD TRAILING EDGE FLAP LOWER SKIN PANEL IS DEBONDED AT THE TRAILING EDGE OF THE FLAP 45 INCHES FROM THE FUSELAGE BETWEEN FLAP RIBS 4 AND 5. REPAIRED FLAP PER EA 360105D AND SRM 57-52-00-300-093,SDR SWAA2026063010342Skin · delaminatedRIGHT OTBD AFT FLAP LOWER INBD END DELAMINATED. RECEIVED A NEW RT OTBD AFT FLAP, INSTALLATION WILL BE ACCOMPLISHED ON CC TTG8Q01CM9EG.SDR SWAA2026063010344Wedge · delaminatedLEFT INBD MID FLAP OTBD T/E EDGE WEDGE DELAMINATED AT TRAILING EDGE. REMOVED AND REPLACED LEFT INBD MID FLAP OTBD T/E EDGE WEDGE IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, 51-40-02-0G-0, DWG 113A2100 REV. C, & AMM 51-31-00.SDR IPXA2026062381318Web · crackedINTERCOSTAL LOCATED ON RT WING TRAILING EDGE ABOVE #2 OUTBD FLAP CARRIAGE FWD LOWER CORNER IS CRACKED. AA010. REMOVED WEB AND BRACKET ON RH WING TRAILING EDGE ABOVE #2 OUTBD FLAP IAW A300 SRM 51-40-21. INSTALLED NEW WEB IN RH WING TRAILING EDGE ABOVE #2 OUTBD SDR IPXA2026062388115Carriage · crackedINTERCOSTAL LOCATED ON LEFT WING TRAILING EDGE ABOVE THE NR 2 OTBD FLAP CARRIAGE IS CRACKED AT THE LOWER FWD AND AFT CORNERS. REMOVED INTERCOSTAL AND BRACKET AT ZONE 500 LT WING TRAILING EDGE ABOVE THE NR 2 OTBD FLAP CARRIAGE IAW SRM 51-40-21. INSTALLED INTERSDR IPXA2026061535378Skin · debondedFAULT - DISBOND - SKIN , INBD EDGE OF L/H WING T/E OUTBD FLAP T/E UPPER SKIN , WBL 355. I.A.W CMM 57-53-51 REV 39 REMOVE THE RETAINER AND SEAL. REMOVE THE DISBOND MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUSDR IPXA2026061235691Skin · debondedFAULT - DEBONDED SKIN , LOWER FACE OF LT WING T/E OTBD FLAP WEDGE LOWER SKIN , WS 663. IAW SRM 57-53-01-2R-1 REFER TO SRM 51-70-06-0G-0 REV. 55 PERFORM REPAIR AS BELOW STEP : 1.REMOVE THE DISBOND MATERIALS AND CLEAN. MEASURE THE DAMAGE SIZE AND LOCATION ( DISDR IPXA2026061235713Skin · debondedDEBONDED SKIN , FORWARD FACE OF LT WING T/E OUTBD FLAP L/E SKIN , WBL 420. REMOVE THE DISBOND MATERIALS AND CLEAN. MEASURE THE DAMAGE SIZE AND LOCATION ( DIA : 1", 5.4" FROM LOWER EDGE, 67" FROM INBD EDGE ). BONDED THE REPAIR PLIES WITH RESIN CURED AT 150°F FSDR DALA2026061103542Vane · dentedDENTS ON UPPER SURFACE OF AFT MOVABLE VANE AT RH WING. UPPER SURFACE OF AFT MOVABLE VANE AT RH WING WERE REPAIRED PER B717-200 SRM 51-70-02-0G PROCEDURE GENERAL, B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 AND ADJUSTMENT UNDER AMDS 2750-4008. (LP 1632855 -SDR SWAA2026060809642Cartridge · crackedLEFT WING OTBD AFT FLAP INBD PROGRAM ROLLER CARTRIDGE ASSY; HAS A HFEC CRACK INDICATION ON THE LOWER AFT SURFACE. R & R LT WING OTBD FLAP IAW AMM 27-51-21, INSPECTED IAW AMM 27-51-22-601-NG.SDR SWAA2026070609326Fairing · damagedELONGATED HOLES ON ON FLAP TRACK FAIRING 544BB UPPER SURFACE AT LT WING. REPAIRED FLAP TRACK FAIRING 544BB UPPER SURFACE AT LT WING IAW SRM 51-70-04-2R-9, REPAIR 9.SDR IPXA2026060408199Flap · damagedACCOMPLISHED REPAIR ON FAULT #T3F18E008THNS, LT OUTBD AFT FLAP DAMAGE.SDR IPXA2026060408251Flap · damagedACCOMPLISHED REPAIR ON FAULT #T3F18E008THPU, LT OUTBD AFT FLAP UPPER SURFACE DAMAGE.SDR SWAA2026060808772Skin · debondedLEFT WING OTBD TE FLAP HAS DISBONDED SKIN ON THE INBD UPPER SURFACE. REMOVED LT OTBD AFT FLAP IAW AMM 27-51-22. REMOVED AND REPLACED IAW AMM 27-51-22-401.SDR KCSA202606031076Rib · damagedINNERMOST RIB IS DAMAGED WHERE LOWER SPRING TUBE OF ACCORDIAN SEAL COMES THROUGH ON THE RT INBD FOREFLAPSDR UIEA2026060300447Skin · damagedCRACK AND BROKEN DAMAGE ON SKIN PANEL ASSY OF LT WING NR 9 V.C FLAP. REPAIRED CRACK AND BROKEN DAMAGE ON SKIN PANEL ASSY OF LT WING NR 9 V.C FLAP IAW EGAT EI T2026A57M-1011 REV 1. 2. CONDITION CHECK IS SATISFACTORY.SDR SWAA2026061708717Skin · delaminatedRIGHT OTBD AFT FLAP IS DELAMINATED AT I/B AREA. RECIEVED NEW RT WING OTBD AFT FLAP. REMOVAL AND INSTALLATION TO BE ACCOMPLISHED ON FAULT TTG8Q01BR0WX.SDR VNAA202607120005Fairing · dented3801.90FH PERM REPAIR - LH FLAP STUB FAIRING (171DL) WITHIN 3801.90 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. LH FLAP STUB FAIRING (171DL) WAS REPAIRED PER EA NO: 53
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