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 DALA2026073004398Strut · corrodedCORROSION INTERCONNECTING STRUT IB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED STRUT PER A321 AMM 27-51-44. (1695840) AIRCRAFT WAS GROUNDED.SDR DALA2026072304313Skin · missingLEFT INBD FLAP MISSING LOWER SKIN, JUST OTBD OF INBOARD FLAP FAIRING MEASURING, 31IN BY 13 IN FLAP. R & R T/E WEDGE PANEL (SSE 664006) IAW AMM 27-51. ACFT OK FOR SVC. (8402931) AIRCRAFT WAS GROUNDED.SDR FDEA202607110912Skin · dentedDENT ON LOWER SKIN OF INBOARD AFT FLAP AT 41 IN. INB EDGE AND 2 IN. TRAILING EDGE ON LEFT WING INBOARD AFT FLAP AT 14". INB EDGE AND 2". TRAILING EDGE ON LT WING WAS REPAIRED IAW SRM 57-53-01-2R, FIGURE 201, SHEET 4, AND SRM 51-70-03-0G, PAR. 5.L FIG. 16, SHSDR SWAA2026072402698Skin · delaminatedRIGHT OTBD AFT FLAP WAS DELAMINATED AT INBD END LWR SURFACE. REPLACED THE RT OTBD AFT FLAP WITH NEW.SDR SWIA2026070776753Flap Track · out of limitsLEFT NR 1A FLAP TRACK HAS DEPTH REDUCTION OF .50 MM AT DEEPEST MEASUREMENT. REMOVED AND REPLACED LT, #1A FLAP TRACK IAW AMM 57-54-25 OPS CHECK GOOD IAW AMM 27-50-00.SDR SWIA2026070776752Flap Track · out of limitsRIGHT NR 5 FLAP TRACK HAS DEPTH REDUCTION OF .80 MM AT DEEPEST MEASUREMENT. REMOVED AND REPLACED THE RT NR 5 FLAP TRACK IAW AMM 27-51-08.SDR DALA2026071304087Cover · missingLT WING INBD FLAP PIVOT COVER MISSING. INSTALLED LT WING INBD PIVOT COVER PER A320 AMM 57-54. (LP: 8498046, AIRCRAFT WAS GROUNDED)SDR IPXA2026082786445Skin · crackedRIGHT WING, INBD FLAP, UPPER SKIN, INBD AFT RUB STRIP CRACKED AND DENT ON STRIP & SKIN, RIB 25A. ACCOMPLISHED REPAIR IAW EO-97985-REQ1 & VT-MAE EA 300-5752-27-A4544, REV-.SDR SWIA2026070376977Vane · chafedRT INBD FLAP VANE LE CHAFED/WORN AT RWS 56 (C-CHECK RO 08/29/2026)REMOVED AND REPLACED NEW IB LEADING SKIN FROM R/H IB FLAP WS 56 IAW CRJ200 SRM 51-10-06,51-42-13,51-40-11,57-52-00,51-21-11,51-25-06,51-25-16.SDR SWIA2026070376974Vane · chafedRIGHT INBD FLAP VANE LE CHAFED/WORN AT R/H WS 140 (C-CHECK RO 08/29/2026)REMOVED AND REPLACED LEADING EDGE SKIN FROM R/H IB FLAP VANE AT WS 140 IAW REO: 601R-57-52-004 AND IAW CRJ200 SRM 51-42-13,51-23-00,51-10-06,51-40-11,57-52-00, 51-21-11,51-25-06,51-25-16SDR AALA202607223329Skin · debondedAIRCRAFT IN BASE MAINTENANCE: LEFT WING TRAILING EDGE INBOARD FLAP UPPER SURFACE SKIN PANEL DEBONDED. REPAIRED FLAP PER SRM 57-52-00-300-114.SDR IPXA2026070878270Flap · crackedFOUND RT WING OUTBD AFT FLAP INBD SIDE BOTTOM SURFACE CRACK. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2 INCHES AROUND HEATED AREA ,PER 747 NDT MANUAL PART 1 51-01-01 REV:183 RESULT:NO DEFECT WAS FOUND. IAW AMM 51-24-11-477-083, REV 116, REPAINT PEEL OFF SDR IPXA2026091176154Skin Panel · crackedLEFT WING, INBD FLAP, UPPER SKIN, INBD AFT RUB STRIP AND SKIN UNDER WITH CRACK (RIB 25A). ACCOMPLISH REPAIR IAW EO-97983-REQ1 AND VT-MAE EA 300-5752-27-A4543, REV-.SDR SWAA2026072896745Wedge · debondedDEBONDED WEDGE PANEL ON RT INBD MAIN FLAP AT RT WING. REPAIR ACCOMPLISHED IAW SRM 57-53-01-2R-18, REPAIR 18.SDR SWAA2026072802495Panel · debondedDEBONDED WEDGE PANEL ON LT INBOARD MAIN FLAP AT LT WING. REPLACED WEDGE PANEL ON LT INBOARD MAIN FLAP AT LT WING FOR REMOVAL AND INSTALLATION SEE TTG8Q01D0DSC.SDR SWAA2026072475308Fairing · pulledRIGHT WING, NR 6 FLAP TRACK CANOE FAIRING, AFT TAIL CONE FAIRING HAS NUMEROUS PULLED AND MISSING FASTENERS. REMOVED AND INSTALLED A SERVICEABLE REPLACEMENT NR 6 FLAP SUPPORT FAIRING TAIL CONE IAW AMM 27-51-18.SDR DALA2026071304081Cover · missingLT WING 1 FLAP TRACK MOVEABLE FAIRING PIVOT COVER MISSING. FWD TO CDL 27-00-16. C/W "M" PROCEDURES. PLACARDS INSTALLED, MCC NOTIFIED. ACFT OK FOR SVC. RETAINER ALREADY INSTALLED. R & R FAIRING PIVOT COVER AS PER A319 AMM 57-55. OK TO CLOSE. (LP: 8199436, AIRCSDR IPXA2026070624589Seal · brokenBROKEN MOLDING SEAL, LT WING NR 2 VC FLAP INBD SIDE. REMOVED THE RAIN EROSION SHIELDS AND CLEANED. APPLY THE SEALANT TO REPAIR AREA.SDR AALA202607154559Flap Track · corrodedUPON, REMOVAL, OF RIGHT WING, T/E. INBD AFT FLAP FOUND, INBD.AND OTBD.TRACKS, WITH PITTING CORROSION. MAINTENANCE REPLACED RT WING T/E INBD FLAP TRACKS IAW AMM 27-51-16.SDR IPXA2026070283407Wedge · crackedCRACKED WEDGE, RT WING OUTBD FLAP INBD WEDGE. REMOVE THE CRACK MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. I.A.W UPS SREO-70175-REQ001 REV.1SDR UIEA2026063000562Flap · damagedSUSPECTED HARD LANDING. PERFORMED PHASE 1A INSP PER AMM 05-51-05-222-081. DURING INSP, FOUND LH FLAP DAMAGE AT MIDDLE OF FOREFLAP LEVEL. SUBSEQUENT DAMAGE TO THE MID FLAP TRACK AND FUSELAGE OF LH TRAILING EDGE MIDFLAP.</P>)SDR UIEA2026060900456Skin · tornLHW L/E #7 VC FLAP LSA LAYER FOUND TORN(<P>PERFORMED REPAIR AS PER CMM 57-55-42-81205-601 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026061000457Skin · tornLHW L/E #8 VC FLAP LSA LAYER FOUND TORN(<P>PERFORMED REPAIR AS PER CMM 57-55-42-81205-601 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026061400483Skin · tornLHW L/E #9 VC FLAP LSA LAYER FOUND TORN(<P>PERFORMED REPAIR AS PER CMM 57-55-42-81205-601 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026061400484Skin · tornLEFT WINT L/E NR 6 VC FLAP LSA LAYER FOUND TORN. PERFORMED REPAIR AS PER CMM 57-55-42-81205-601 REPAIR 17-1. NO FURTHER DEFECTS NOTED.SDR UIEA2026061400485Skin · tornRIGHT WING L/E #19 VC FLAP LSA LAYER FOUND TORN. PERFORMED REPAIR AS PER CMM 57-55-42-81205-601 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026061400486Skin · tornRIGHT WING L/E #18 VC FLAP LSA LAYER FOUND TORN. PERFORMED REPAIR IAW CMM 57-55-42-81205-601 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026061800529Fairing · delaminatedRHW T/E FLAP #6 CANOE FAIRING INNER SURFACE FOUND 3EA DELAMINATION. PERFORMED REPAIR AS PER RI-57-50-18310 REV B AND SRM 51-70-04 REPAIR 1. NO FURTHER DEFECTS NOTED.</P>)SDR IPXA2026063066815Strut · wornFOUND RH WING OUTBD FLAP SUPPORT STRUT LOWER INSERT, COVE ATTACH WORN OUT, WBL 695. REVIEWED PER GMM-MTX 09.05.01.09. IAW CMM 57-52-55 601, REPAIR PARAGRAPH 1.F.(4), REV 212. REFER TO SRM 57-53-01-2R-1 AND SRM 51-70-07-0G-0 REV. 107 PERFORMED REPAIR.SDR AALA202607155904Flap Track · corrodedAIRCRAFT IN BASE MAINTENANCE: UPON, REMOVAL OF LEFT WING T/E .I/B. AFT. FLAP FOUND TRACKS WITH PITTING CORROSION. MAINTENANCE REPLACED L/H WING T/E I/B AFT FLAP TRACKS IAW B737NG AMM 27-51-16.SDR SWIA2026062577242Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE RA111654-REO 601R-57-53-1337 REV-, PERMANENT REPAIR ON RA ID 111654. PERFORMED PERMANENT REPAIR OF DENT TO LT, OTBD FLAP VANE LEADING EDGE SKIN IAW SRM 51-42-10, DWG 601R14502, REV D, & COMPLIED WITH TASK CARD 51-900-100SDR U2RA2026070800032Skin · dentedDURING AIRCRAFT C-CHECK IN ICN (INCHEON, SOUTH KOREA) SHARP TECHNICS K MAINTENANCE DISCOVERED CHAFE DAMAGE ON THE UPPER SURFACE OF THE INBOARD TRAILING EDGE AFT FLAP OUTER SKIN PANEL P/N 65B02077-508. PERFORMED PERMANENT REPAIR IAW FLIGHT VEHICLES CONSULTING, SDR SWAA2026062915694Bracket · crackedLT WING UPPER TRAILING EDGE DEFLECTION RIB TO WING BRACKET IS CRACKED. C/W SRM 57-51-02-2R-3 UP TO 4.M. DRILLED HORIZONTAL FLANGE OF ONE FITTING TO THE DEFLECTION CONTROL RIB. INSPECTED IAW SRM 57-51-02-2R-3-B00043, REPAIR 3. C/W SRM 57-51-02-2R-3 FROM SSDR FDEA202606250801Skin · dentedRIGHT WING INB MAIN FLAP TRAILING EDGE OTBD SECTION, UPPER AND LOWER SURFACE SHOWS MULTIPLE DENTS APPLIED PERMANENT REPAIR AT UPPER AND LOWER SURFACE ON RH WING INBD MAIN FLAP TRAILING EDGE IAW SRM 57-53-01-2R REP 1, DETAIL I, FIG 201, SHEET 2 AND SRM 51-SDR SWAA2026072104757Fairing · crackedNR 6 CANOE IS CRACKED ON INSIDE LOWER SKIN. REPAIRED PER E/A M-21-157-01063 AND RESTORED FINISH IAW AMM 51-21-81.SDR SWAA2026062915293Angle · crackedAFT FIXED T/E L ANGLE THAT ATTACHES TO THE FLAP PROGRAMING BEAM IS CRACKED. REMOVED AND REPLACED 1 EACH AFT FIXED T/E L ANGLE THAT ATTACHES TO THE FLAP PROGRAMMING BEAM PER SRM 51-40-02.SDR SWAA2026062915291Fitting · crackedAFT UPPER FIXED T/E SEAL RETAINER IS CRACKED JUST INBD OF FLAP PROGRAMING BEAM. REMOVED AND REPLACED SEAL RETAINER FITTING IAW SRM 51-40-02.;[02] C/W INSPECTIONSDR SWAA2026062915391Rib · crackedPOSSIBLE CRACK INDICATION ON LT OTBD AFT FLAP INBOARD CLOSURE RIB UPPER HOLE AT 7 O'CLOCK POSITION. R & R T/E AFT FLAP LT OTBD IAW AMM 27-51-22, NO DEFECTS NOTED.SDR DALA2026062503773Support · corrodedLH WING, OTBD FLAP, SUPPORT AT TRACK 3, RIB 5 AND TRACK 4, BETWEEN INNER RIB 14 AND OUTER RIB 14, WITH CORROSION INTERNAL STRUCTURE. FOR REMOVAL OF THE LH WING OUTBOARD FLAP S/N: D01703, SEE DELTA WORK CARD 2750-6020-LT. (LP: 1664687, AIRCRAFT WAS GROUNDED)SDR AALA202606293250Trunnion · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION AND GOUGE ON THE RIGHT WING INBOARD TRAILING EDGE FLAP TRUNNION FACE. REPLACED TRUNNION PER CMM 57-52-23.SDR SWIA2026062277020Hinge Arm · out of limitsLH OB FLAP HINGE ARM WS178.00 INBD LEADING EDGE-SIDED BUSHING REQUIRES FABRICATION (C-CHECK RO 08/28/2026)PERFORMED A MAJOR REPAIR BY FABRICATING FREEZE PLUG AND DRILLING TO SIZE, AND INSTALLING SERVICEABLE BUSHING INTO HINGE ARM WITH BOMBARDIER REO 601R-57-5SDR HNAA2026072400627Rib · damaged00361 LH INBD FLAP HAS AN ELONGATED SCREW HOLE AS MARKED. COMPLIED WITH PERMANENT REPAIR OF THE L/H IB FLAP FAIRING ATTACH RIB PER EMB 145 ETD2026-145-010947 REV.: A, AND PIEDMONT EO1-57-26-0313SDR SWAA2026062314142Rib · crackedRIGHT OTBD AFT FLAP INBOARD CLOSURE RIB HAS AN INDICATED HFEC SURFACE CRACK ON THE LOWER SURFACE OF THE CARTRIDGE ASSEMBLY. REMOVED AND REPLACED IAW AMM 27-51-22-401-NG. OPS AND RIG CHKD GOOD.SDR SWAA2026072890712Support Bracket · corrodedRIGHT WING TRAILING EDGE LOWER PANEL SUPPORT BRACKET CORRODED AT FASTENER LOCATIONS. (LOCATED BETWEEN FLAP TRACKS 6 AND 7). REMOVED AND REPLACED SOPPORT BRACKET AT R/W T/EDGE LOWER PNL IAW SRM 51-40-05 AND 51-40-02 REF AIPC 57-50-00-20.SDR LR7A2026061903880Skin · crackedDURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5711, FOUND LT OTBD FLAP UPPER CENTER SKIN CRACKED UNDER BUMPER PAD AT OWFS207L. REPAIRED IAW SRM 51-14-12.SDR LR7A2026061903879Skin · crackedDURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5711, FOUND LT OTBD FLAP UPPER CENTER SKIN CRACKED UNDER CHAFE PAD AT OWFS0L. REPAIRED IAW LOCKHEED SRM 51-140-12.SDR LR7A2026061903861Spar Cap · corrodedDURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5511, FOUND HORIZONTAL STAB FRONT SPAR UPPER CAP CORRODED AT FS 1041, HSS 62-64R, WL 283. REPAIRED IAW MEA 382-55-25-064.SDR LR7A2026061903858Skin · chafedDURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5712, FOUND LT INBOARD FLAP LEADING EDGE SKIN CHAFED AT CWS82R. REPAIRED IAW LOCKHEED SRM 51-140-12.SDR LR7A2026061903857Skin · chafedDURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5711, FOUND LT INBD FLAP LEADING EDGE SKIN CHAFED AT CWS82L. REPAIRED IAW LOCKHEED SRM 51-140-12.SDR LR7A2026061903854Rib · crackedDURING SCHEDULED C-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT OUTBOARD FLAP RIB CRACKED AT OWFS336L. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
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