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 SWAA2026082446338Skin · delaminatedFOUND LEFT OTBD AFT FLAP DELAMINATED. REMOVED AND REPLACED LT OTBD AFT FLAP IAW AMM 27-51-22-401.SDR SWAA2026082456139Skin · delaminatedFOUND RT OTBD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT OTBD AFT FLAP IAW AMM 27-51-22.SDR FDEA202608111112Rivet · looseRIGHT WING INBD FLAP UPPER SKIN, FOUND SEVERAL RIVETS LOOSE AT XIFH 276.36. RT WING INBOARD FLAP UPPER SKIN LOOSE RIVETS AT XIFH 276.36 CARRIED OUT REPAIR AS PER EA 1-5750-T0308240 B P2. REPAIR CLASSIFIED AS MAJOR, IAW GMM 6-2-100.SDR REXA2026092101861Plate · worn"WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES FLAP FITTING (2EAS) AND PLATE SUPPORT (2EAS) OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01,SRM 51-42-SDR REXA2026092101860Plate · worn"WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES FLAP FITTING (2EAS) AND PLATE SUPPORT (2EAS) OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01,SRM 51-42-SDR REXA2026092101859Fitting · worn"WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES FLAP FITTING (2EAS) AND PLATE SUPPORT (2EAS) OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01,SRM 51-42-SDR REXA2026092101858Fitting · worn"WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES FLAP FITTING (2EAS) AND PLATE SUPPORT (2EAS) OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01,SRM 51-42-SDR SWAA2026082156053Fairing · crackedNR 6 CANOE FAIRING 642BB CRACKED ON THE INSIDE, BELOW LINKAGE NEAR DRAIN HOLE. REPAIRED IAW EA M-21-157-01063, AND RESTORED FINISH IAW AMM 51-21-81.SDR SWAA2026082158844Skin · crackedLEFT WING OTBD AFT FLAP REQUIRES REPLACEMENT DUE TO CRACK AT INBD END RIB. REMOVED AND REPLACED LT OTBD AFT FLAP ON TTG8Q01BR3V8.SDR DALA2026081004615Structure · separatedAFTER LANDING, CREW WAS INFORMED THAT A PIECE OF RT TRAILING EDGE FLAP DEPARTED THE ACFT ON ROTATION, VISUAL INSPECTION AFTER PARKING CONFIRMED PART OF FLAP WAS MISSING. FLAP 25 TAKEOFF. R & R OTBD FLAP ASSY IAW AMM 27-51. (8592099) AIRCRAFT WAS GROUNDED.SDR FDEA202608101102Skin · dentedRIGHT WING OTBD FLAP LWR SURFACE 30 INCHES IB OF NR 7 FLAP SUPPORT FAIRING AND 5 INCHES FROM T/E FOUND DENTED. REPAIRED RHW OB FLAP LWR SURFACE 30 INCHES IB OF #7 FLAP SUPPORT FAIRING AND 5 INCHES FROM T/E DENT AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 ASDR IPXA2026082799311Bracket · crackedLEFT CENTER FLAP, OTBD FACE, AFT BRACKET BROKEN. REMOVED AND REPLACED ONE BRACKET AT LT CENTER FLAP, OTBD FACE IAW SRM 51-40-21-001.SDR SWAA2026082158466Rib · crackedLEFT OTBD AFT FLAP INBD END RIB CRACKED. REPAIRED ON RO TTG8Q01DMPK5.SDR AALA202608288816Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: R/H O/B AFT FLAP HAS LARGE AREA OF DELAMINATION ON THE I/B UPPERSURFACE. REMOVED AND REINSTALLED R/H O/B AFT FLAP IAW B737-NG-AMM 27-51-22 REMOVED DAMAGED SKIN (9.25"X12") ON R/H O/B AFT FLAP IB UPPERSURFACE IAW B737-NG SRM 57-53-SDR UIEA2026081000735Repair · noneEXISTING REPAIR ON RT WING OTBD MID FLAP LOWER SURFACE. PERFORMED PERMANENT REPAIR ON RT WING OTBD MID FLAP LOWER SURFACE, WBL 563 IAW SRM 57-53-01-2R-1 AND SRM 51-70-10-2R-0, REV 107. CONDITION CHECK IS SATISFACTORY. REPAIR PROCESS REFER TO J/C ATTACHING SHSDR FDEA202608081101Skin · damagedEVALUATE EXISTING DOUBLER REPAIR ON RH INBOARD MAIN FLAP LOWER SURFACE, NEAR MF STA 147.00 FOR RSC TRACKING PURPOSE ONLY EXISTING REPAIR ON RH INBOARD MAIN FLAP LOWER SURFACE NEAR MF STA 147.00 WAS EVALUATED UNDER FEDEX EA # F-5750-T0388266 A P1 WITH TITSDR IPXA2026082665162Fairing · damagedDAMAGED RT WING NR 6 AFT FAIRING SURFACE. REMOVED THE DAMAGE MATERIALS AND CLEANED. BONDED THE REPAIR PLIES WITH RESIN CURED AT 200 F FOR 240 MINS WITH MINIMUM VACUUM OF 22 IN/HG. IAW SRM 57-53-70-2R-1, REF SRM 51-70-04-2R-1 AND SRM 51-30-10-0G-0, REV 49.SDR AALA202610059244Wedge · gougedAIRCRAFT IN BASE MAINTENANCE: GOUGE ON UPR SKIN OF LEFT INB AFT FLAP TRAILING EDGE WEDGE, APPROX 4 FEET OUTB FROM FUSELAGE, GOUGE APPROX ONE INCH LONG AND 0,5 INCH WIDE (L=4.35 INCH W=1.51 INCH Y=0.032 INCH). REPAIRED UPPER SKIN INBOARD AFT FLAP TRAILING EDGE SDR IPXA2026091458143Skin · chafedRT WING, INBD FLAP, T/E, INBD SIDE, UPPER SURFACE WITH CHAFING MARK. INSTALLED TAIL END ASSY. AT RT WING, INBD FLAP, T/E, INBD SIDE IAW SRM 51-40-21.SDR IPXA2026090851105Rib · crackedLEFT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 3 EA CRACK INDICATION NOTED AT RIB 26. ACCOMPLISHED PERMANENT REPAIR IAW EO-98405-REQ1 AND EA 300-5750-27-A4600, REV -.SDR IPXA2026090851282Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 EA CRACK INDICATIONS NOTED AT RIB 26. ACCOMPLISHED PERMANENT REPAIR IAW EO-98461-REQ1 AND EA 300-5750-27-A4602, REV -.SDR IPXA2026091051162Rib · crackedMAJOR REPAIR, RT WING, CENTER FLAP, TOP SKIN RIB FLANGE, ONE CRACK INDICATION NOTED AT RIB 25. VERIFIED ACCOMPLISHED PERMANENT REPAIR IAW EO-98461-REQ1 (T3F18E009JLB2) AND EA 300-5750-27-A4602, REV -.SDR IPXA2026091051256Rib · crackedMAJOR REPAIR, RT WING, CENTER FLAP, TOP SKIN RIB FLANGE, TWO CRACK INDICATIONS NOTED AT RIB 27. ACCOMPLISHED PERMANENT REPAIR IAW EO-98461-REQ1 AND EA 300-5750-27-A4602, REV -.SDR IPXA2026091051151Rib · crackedRH WING, CENTER FLAP, TOP SKIN RIB FLANGE, HAD 1 CRACK INDICATION NOTED AT RIB 12. ACCOMPLISHED PERMANENT REPAIR IAW EO-98461-REQ1, AND EA 300-5750-27-A4602, REV -.SDR IPXA2026090851082Rib · crackedMAJOR REPAIR, LT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 EA CRACK INDICATION NOTED AT RIB 27. ACCOMPLISHED PERMANENT REPAIR IAW EO-98405-REQ1 AND VT-MAE EA 300-5750-27-A4600, REV -.SDR IPXA2026090758082Bracket · brokenRIGHT CENTER FLAP, OTBD FACE, AFT BRACKET BROKEN. REMOVED AND REPLACED ONE BRACKET AT RT CENTER FLAP, OTBD FACE IAW SRM 51-40-21-001.SDR IPXA2026090758776Bracket · damagedRIGHT WING OTBD FLAP INBD EDGE AFT ANGLE HAS ELONGATED HOLES. REMOVED AND REPLACE NEW ANGLE IAW SRM 51-40-21-001.SDR HNAA2026090100851Support · corrodedRIGHT INBD FLAP, OTBD FLAP SHROUD SUPPORT, PITTED ON MATING SURFACE. REMOVED THE CORROSION ON RT INBD FLAP, OTBD FLAP SHROUD SUPPORT BY BLENDING. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 51-10-05-PR, STEP 3. REPLACED THE SHROUD SUPPORT WITH NEW.SDR AALA202608113432Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: CUST REQ: RIGHT WING OUTBD AFT FLAP HAS DELAM , INBD UPPER SIDE. MAINTENANCE REPLACED RIGHT WING OUTBD AFT FLAP.SDR SWIA2026080577248Vane · chafedRIGHT INBD FLAP VANE, OTBD LEADING EDGE CAP REQUIRES REPLACEMENT DUE TO CHAFE DAMAGE OUT OF LIMITS. REPLACED RT INBD FLAP VANE- LEADING EDGE OTBD CAP IAW SRM 51-42-13, AND DWG 601R14302, REV E. COMPLIED WITH SKYCARD 51-900-1003-SKY. MAJOR REPAIR.SDR SWIA2026080577233Vane · chafedRIGHT IBD FLAP VANE, INBD LEADING EDGE CAP REQUIRES REPLACEMENT DUE TO CHAFE DAMAGE OUT OF LIMITS. REPLACED THE DAMAGED FLAP VANE NEW IAW SRM 51-42-13, & DWG 601R14302, REV E. COMPLIED WITH SKYCARD 51-900-1003-SKY. MAJOR REPAIR.SDR SWAA2026081022001Fairing · pulledNUMBER 3 FLAP CANOE FAIRING TAILCONE, AFT TOPSIDE 2 SCREWS PULLED 1/2 & LOOSE, LEFT WING. OK TO CONTINUE IAW CDL 57-10-4. INSTALLED NEW NR 3 FLAP CANOE FAIRING TAILCONE IAW AMM 27-51-18. REF TTG8Q01E3EE0 FOR INITIAL FAULT.SDR IPXA2026080703836Wedge · damagedRIGHT OUTBOARD FLAP, INBOARD T/E WEDGE UPPER AND LOWER SKIN DAMAGE. (REPAIR). I.A.W UPS SREO-70175-REQ001 REV. 1 PERFORM REPAIR AS BELOW. REMOVED THE CRACK MATERIALS AND CLEANED. MEASURE THE DAMAGE AREA ( L : 0.8", W : 0.05", 6" FROM AFT EDGE , AT INBD EDGESDR IPXA2026080789540Skin · debondedDISBOND - SKIN , LT WING T/E OUTBD FLAP INBD LWR. (REPAIR). IAW SRM 57-53-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV.55. PERFORM REPAIR AS BELOW STEP:1.1 REMOVED THE DISBOND MATERIALS AND CLEANED. MEASURE THE DAMAGE SIZE AND LOCATION (L:4.5", W:2", 1.3" FROM AFSDR SWAA2026081724331Skin · delaminatedLEFT AFT FLAP HAD A DELAMINATED AREA ON INBD AFT SIDE, 3 INCH IN DIA. R & R LT OTBD AFT FLAP IAW AMM 27-51-22. R & R LT OTBD AFT FLAP IAW AMM 27-51-22.SDR IPXA2026092347719Flap Track · debondedDISBOND-SKIN,LOWER FACE OF LT WING NR 4 FLAP TRACK AFT FAIRING. IAW SRM 57-53-70-2R-1 REFER TO SRM 51-70-05-2R-1 REV.49 PERFORM REPAIR AS BELOW STEP:1.1 REMOVE THE DISBOND MATERIALS AND CLEAN.1.2 MEASURE THE DAMAGE AREA (DIA:1", 21.5" FROM UPPER EDGE, 47" FRSDR IPXA2026080747679Seal · brokenBROKEN MOLDING SEAL , LT WING NR 4 V.C FLAP OUTBD SIDE MOLDING SEAL IAW SRM 57-43-02-2R-4, REV 49, REFER TO SOPM 20-50-12 REV 160. PERFORM REPAIR AS BELOW STEP :1. REMOVE THE RAIN EROSION SHIELDS AND CLEAN. APPLY THE SEALANT TO REPAIR AREA CURED AT 70 F FORSDR FDEA202607311073Skin · dentedTHREE DENTS ON LOWER SURFACE OF OUTBOARD FLAP RH ON AREA BTW 6'' TO 11'' FROM INBOARD FAIRING AND BTW 22'' TO 30'' FROM AFT EDGE. DENTS ON LOWER SURFACE OF OUTBOARD FLAP ON AREA BTW 6'' TO 11'' FROM INBOARD FAIRING AND BTW 22'' TO 30'' FROM AFT EDGE, WAS ESDR FDEA202607311072Skin · delaminatedL/H WING INB MAIN FLAP UPPER SURFACE OUTB SECTION PREVIOUS REPAIR IS DISBONDED APPLIED PERMANENT REPAIR AT LH WING I/B MAIN FLAP UPPER SURFACE IAW B757 SRM 57-53-01- 2R, REP 1, DETAIL I, FIG 201, SHEET 2, SRM 51-70-10--2R REP 4 AND COMPLIED WITH F EA # F-5750SDR FDEA202607311071Skin · delaminatedRH WING I/B FLAP UPPER SURFACE WITH PREVIOUS REPAIR DISBONDED APPLIED PERMANENT REPAIR AT RH WING I/B FLAP UPPER SURFACE IAW B757 SRM 57-53-01-2R REP 1 DETAIL I, FIG 201, SHEET 2, SRM 51-70-10-2R, REP 4, FIG 201, SHEET 1 AND COMPLIED WITH FEDEX EA # F-5750SDR CALA2026080218178Flap · crackedFLAP DAMAGED, OUT-OF-LIMITS.SDR VNAA202610060003Flap · nickedSEVERAL NICKS BTW FLS=15.00 TO FLS=40.00 INBOARD FLAP AT RH WING. SEVERAL NICKS BTW FLS=15.00 TO FLS=40.00 ON INBOARD FLAP AT RH WING WAS REPAIRED PER CRJ-900 SRM 57-52-01-201-005-A01SDR SWAA2026080308795Cartridge · crackedLEFT WING OUTBOARD AFT FLAP INBOARD CLOSURE RIB CARTRIDGE ASSEMBLY IS CRACKED ON AFT LOWER SURFACE. REMOVED AND REPLACED LT OTBD AFT FLAP IAW AMM 27-51-22. VERIFIED ADJUSTMENT ADJUSTMENT GOOD. OP CHECKED GOOD. VERIFIED WORK ACCOMPLISHED IAW AMM 27-51-22.SDR UIEA2026072000615Skin · debondedRHW I/B AFT FLAP UPPER O/B PANEL PREVIOUS REPAIR DOUBLER FOUND DISBOND(<P>PERFORMED METAL HOT BOND REPAIR AT DISBOND AREA AS PER HX RI-57-53-18374 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000619Fairing · delaminatedLHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000620Fairing · delaminatedLHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000621Fairing · delaminatedLHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000622Fairing · delaminatedLHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000623Fairing · delaminatedLHW I/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000624Skin · delaminatedLHW O/B FORE FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)
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