JASC 5753
Service difficulty reports · 31,496
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 DALA2025040802699Vane · dentedDENTS ON AFT MOVABLE VANE (LOWER SURFACE) AT LH WING. SUMMARY OF NRC 00468: AFT MOVABLE VANE (LOWER SURFACE) AT LH WING WAS REPAIRED PER ER/A 624886-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI REV 2. ASSOCIATED ER/A 14-624886 ADDED FOR AC 9547. (LP #08SDR DALA2025040502605Skin · delaminatedAIRFRAFT 3002, R/H WING T/E O/B LOWER FLAP T/E DELAMATED AT O/B ATTACHMENT ARM TAB AREA. MEASURING ABOUT 4.5 INCHES LONG AND 2.24 INCHES WIDE. (915-029). CORRECTIVE ACTION: REMOVED DAMAGED CORE FILLER AND REPAIRED AND RESTORED FINISH PER ER/A 625494-14. (LP 08SDR DALA2025040502604Skin · delaminatedAIRCRAFT 3002, R/H WING T/E O/B LOWER FLAP T/E DELAMATED AT I/B NO 1 ATTACHMENT ARM MEASURING 4 INCH LONG BY 1.2 INCHES WIDE. (915-032). REMOVED DAMAGED CORE FILLER AND REPAIRED AND RESTORED FINISH PER ER/A 625494-14. (LP 0895942)SDR SWIA2025071600403Fastener · looseRIGHT OTBD FLAP PANEL HAS NUMEROUS SMOKING FASTENERS ON UPPER SKIN. INSTALLED 12EA NEW FASTENERS CR3224-5 BLIND RIVETS FROM RT OUTBOARD FLAP, REF SRM 51-42-13-001-001-A01 AND REO 690-57-53-166, REV: -A, COMPLIED WITH SKYWEST ST CARD 51-900-1002-SKY.SDR NACA2025040300004Skin · chafedCHAFING WAS FOUND AT LH WING O/B MID FLAP LOWER SKIN , WBL 272.6 , L:2.1 INCH , W:0.4 INCH. PERFORMED PERMANENT METAL BOND REPAIR WITH 250 F CURE MATERIAL AT LH WING O/B MID FLAP LOWER SKIN, WBL 272.6 IAW B737-300 SRM 57-53-01 REPAIR 6 & SRM 51-70-10 REPAIR 4SDR NACA2025040300003Skin · chafedCHAFING WAS FOUND AT LH WING O/B MID FLAP LOWER SKIN , WBL 258.6 , L:2.1 INCH , W:0.5 INCH. PERFORMED PERMANENT METAL BOND REPAIR WITH 250 F CURE MATERIAL AT LH WING O/B MID FLAP LOWER SKIN, WBL 258.6 IAW B737-300 SRM 57-53-01 REPAIR 6 & SRM 51-70-10 REPAIR 4SDR SWAA2025042955213Fairing · damagedPANEL 642BB; #6 FLAP TRACK FAIRING; HAS SEVERAL ELONGATED HOLES (AFT END).<[01] REMOVED PANEL 642BB FAIRING DRIVE LINKAGE AND INSTALLED ON NEW PANEL 642BB IAW AMM 27-51-18-400-802.<BR>TORQUE WRENCH 2321 S/N 0119121014 DUE: 06/2025;[02] VERIFIED CORRECTIVE ACTISDR SWAA2025042955217Fairing · crackedPANEL 642BB; #6 FLAP TRACK FAIRING; HAS POSSIBLE CRACK 16 INCHES FWD FROM AFT BULKHEAD ASSY BOTTOM OF FAIRING (MARKED).<[01] #6 FLAP TRACK FAIRING 642BB IS BEING REPLACED ON FAULT: TTG8Q00ZN8EZ.;[02] #6 FLAP TRACK FAIRING 642BB IS BEING REPLACED ON FAULT: TTG8SDR SWAA2025042955215Fairing · damagedPANEL 642EB; #6 FLAP TRACK FAIRING TAILCONE; HAS SEVERAL ELONGATED HOLES.<[01] REMOVED AND REPLACED PANEL 642EB; #6 FLAP TRACK FAIRING TAILCONE; P/N 113A9352-1 LOT 1601033-1<BR>RECEIVED NEW TAIL CONE WITH FULL SIZE HOLES; COUNTERSANK HOLES IAW SRM 51-40-08 & ISDR SWI2025F00718Fitting · gougedLH WING OB FLAP, CENTER HINGE BOX FITTING HAS A GOUGE, AFT FITTING (C-CHECK RO 06/07/2025)PERFORMED REPAIR ON LH WING OB FLAP, CENTER HINGE BOX FITTING, AFT FITTING IAW CRJ700 51-12-00, MHIRJ REO 670-57-21-1053, REV: --, DATE: 2025-05-02.NDT PERFORMED BY BAROSDR SWI2025F00717Fitting · gougedLW WING, IB FLAP, OB HINGE BOX FITTING HAS A GOUGE AFT FITTING (C-CHECK RO 06/07/2025)REPAIRED DAMAGE TO HINGE BOX FITTING ON LH WING, INBD FLAP, OTBD AFT FITTING IAW REO 670-57-21-1053 REV-- DATE 2025-05-02 AND CRJ700 SRM 51-10-06, 51-12-00. NDT PERFORMED BYSDR SWI2025F00715Fitting · gougedLH WING OB FLAP, OB HINGE BOX AFT FITTING HAS A GOUGE (C-CHECK RO 06/07/2025)PERFORMED BLEND OUT DAMAGE ON LH WING OB FLAP, OB HINGE BOX IAW MHI RJ REO 670-57-21-1053 REV: --, DATE: 2025-05-02 AND CRJ 700 SRM 51-12-00.NDT PERFORMED INSPECTION BY BARON NDT, LSDR SWIA2025060900402Fitting · gougedLH WING OB FLAP, IB HINGE BOX FITTING HAS A GOUGE, AFT FITTING (C-CHECK RO 06/07/2025)PERFORMED BLEND OUT ON LH WING OB FLAP, IB HINGE BOX FITTING FOUND TO BE LIMITS IAW REO 670-57-21-1053 REV-- DATE:2025-05-02 AND CRJ700 SRM 51-12-00 SRM 51-11-00PERFORMED NDSDR SWIA2025070100401Fitting · wornRH OUTBOARD FLAP PANEL CAM ROLLER FITTING FLS179.96 WORN FROM BUTE DOOR ROLLER (C-CHECK RO 06/29/2025)RH OUTBOARD FLAP PANEL CAM ROLLER FITTING FLS179.96 REPAIRED PER REO 670-57-53-008 REV -C DATED 2017-12-19. WITHIN LIMITS. BUTE DOOR ROLLER REPLACED WITH NEWSDR NACA2025040100003Skin · bulgedBULGE WAS FOUND AT LH WING I/B AFT FLAP NOSE LOWER SKIN , BETWEEN WBL 149 AND WBL 151. SHIM REPLACED, REMOVED AND INSTALLED LEADING EDGE SKIN AT LH WING I/B AFT FLAP, BETWEEN WBL 149 AND WBL 151. PER AIR ASIA W.P.S. CODE LM 65-46434-506, SRM 51-40-02 PARA 4 PSDR VNAA20250525016Skin · wornWEAR ON LWR SKIN OF LH OUTBD FLAP BTW FL168.63 TO WS 262. REPAIRED PER REO 670-57-53-409 REV--.SDR VNAA20250525015Skin · dentedDENT ON LOWER SKIN OF LH INBOARD FLAP BTW FLS92.80 TO FLS101.40. DENT ON LOWER SKIN OF LH INBOARD FLAP BTW FLS92.80 TO FLS101.40 WAS REPAIRED PER REO 670-57-52- 605. REV. - -.SDR DALA2025040402555Strut · corrodedSHIP 3118 DISC: CORROSION INTERCONNECTING STRUT OB FLAP TARGET ON RH WING. C/A: REMOVED THE INTERCONNECTING STRUT R/H P/N D5757032201100 S/N 03985 UNSERVICEABLE CONDITION AS PER A320 FAM AMM 27-51-44-000- 001-A. EXCEPT STEP 3.D(2) JOB IN PROGRESS. PERFORMED THSDR DALA2025040402556Strut · faultedSHIP 3118 DISC: CORROSION OB FLAP TARGET OF INTERCONNECTING STRUT ON LH WING. C/A: REMOVED THE INTERCONNECTING STRUT L/H P/N D5757032201100 S/N 01841 UNSERVICEABLE CONDITION AS PER A320 FAM AMM 27-51-44-000- 001-A. EXCEPT STEP 3.D(2) JOB IN PROGRESS. REPLACED SDR SWAA2025042419377Tail Cone · elongated#6 FLAP TRACK FAIRING TAIL CONE UPPER CENTER MOUNT HOLE ELONGATED. <[01] REPAIRED UP TO PARAGRAPH 4 K PER SRM 51-70-04-2R-9; [02] VERIFIED REPAIRED UP TO PARAGRAPH 4 K PER SRM 51-70-04-2R-9. PART REQUIREMENTS.; [03] FINISHED REPAIR PER SRM 51-70-04-2R-9; [04] SDR DALA2025033002338Flap Track · corrodedSHIP 3141 DISC: *DTE* DURING M2 AND WHILE ACCOMPLISHING JIC 2750-1020-LT CORROSION WAS FOUND IN TRACK #3, RIB #5 INB'D AND OUTB'D FACES OF RIB 5 BORE. DTE REQUIRED PER SECITON DTE OF 624541-14, THE REPAIR OF SECTION I IS LIMITED TO 97,976 FC FROM SECTION I. ASDR IPXA2025042288075Skin · debondedRIGHT WING OUTBOARD FLAP, TOP PANEL 666KT SKIN DISBOND, 22 INCH TO INBOARD EDGE AREA (REPAIR). CLEAN, SEAL AND FINFISH AT REPAIR AREA I.A.W. 767-300F SRM 51-70-10-2R-0 PARAGRAPH 22 REV.91. I.A.W SRM 51-41-02 REV 91 INSTALL PANEL NO 666KT AT RIGHT WING OUTBOSDR IPXA2025033188075Skin · debondedRIGHT WING OUTBOARD FLAP, TOP PANEL 666KT SKIN DISBOND, 22 INCH TO INBOARD EDGE AREA (REPAIR) CLEAN, SEAL AND FINFISH AT REPAIR AREA I.A.W. 767-300F SRM 51-70-10-2R-0 PARAGRAPH 22 REV.91. OPENSDR SWAA2025050509864Skin · debondedCUSTOMER REQUEST - DEBONDED OB AFT FLAP ON IB SIDE AT LT WING 2025-224275<[01] TOOL USED CALIPER PN: 8647A42; SN: A22356048; DUE DATE: 25/JUL/25.;[02] TOOL USED: AUDIBLE BOND TESTER; P/N S-3; S/N: 064; CAL DUE DATE: 27-AUG-25;[03] TOOL USED ON STEP 18 ULTRASONSDR SWAA2025043054344Skin · debondedCUSTOMER REQUEST - DEBONDED OB AFT FLAP ON IB SIDE AT LT WING 2025-224275<[01] TOOL USED CALIPER PN: 8647A42; SN: A22356048; DUE DATE: 25/JUL/25.;[02] TOOL USED: AUDIBLE BOND TESTER; P/N S-3; S/N: 064; CAL DUE DATE: 27-AUG-25;[03] TOOL USED ON STEP 18 ULTRASONSDR WRXR20250326001Vane · dented2 GOUGES ON LEFT HAND INBOARD FLAP VANE AT WS80 AND WS90. BLENDED GOUGES, GRIDDED, AND REQUESTED NDT FOR REMAINING THICKNESS MEASUREMENTS IAW CRJ 900 SRM 57-52-01-101-001-A01. COMPLIED WITH REO 690-57-52-513 REV--.SDR IPXA2025040836232Skin · debonded**SUPPLEMENTAL SDR**FAULT - DISBOND - SKIN , LOWER FACE OF L/H WING T/E OUTBD FLAP LOWER SKIN , WBL 682. I.A.W SRM 51-40-02 REV.91 REMOVED THE PANEL NO.566LT.G.V.I & CHECK CONDITION CHECK NORMAL.REMOVED DAMAGED ALUMINUM HONEYCOMB CORE AND MADE ALL THE CORNERS SDR SWAA2025033108852Fairing · cracked#6 AFT FAIRING TAIL CONE IS CRACKED AND DELAMED<[01] REMOVED AND REPLACED TAIL CONE ON #6 AFT FAIRING REF AMM 27-51-18.SDR DALA2025032702272Plate · damagedSHIP 3141 DURING M2 AND WHILE ACCOMPLISHING JIC 2750-1020-RT CORROSION FOUND IN OB ALUMINUM PLATE (FACE AND BORE) AT TRACK #3 IN OUTER RIB 5 ECCENTRIC BEARING AREA ON RH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 624731-14. (0875905)SDR IPXA2025032636232Skin · debondedDISBOND - SKIN , LOWER FACE OF L/H WING T/E OUTBD FLAP LOWER SKIN , WBL 682. (REPAIR) REQUEST UPS ENGINEERING DETERMINE MAJOR OR MINOR REPAIR. OPENSDR JR2R20250325777Hinge Fitting · damagedRH MAIN FLAP HAS ELONGATED HOLW WHERE AFT PYLON FAIRING ROD CONNECTSSDR DALA2025032702273Support · corrodedSHIP 3141 DURING M2 AND WHILE INSPECTING PER JIC 2750-1020-LT CORROSION FOUND IN PENDULUM SUPPORT, INB'D AND OUTB'D LUG BORES OUTER FACE OF OUTB'D LUG AT FLAP TRACK #4 OF OUTB'D FLAP ON LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 31-624475. (0875434)SDR UIEA2025030800226Skin · corrodedRH WING INBOARD TE FLAP, CORROSION ON LOWER SKIN.(<P>RH WING INBOARD TE FLAP, LOWER SKIN WAS REPAIRED IAW TRE 6757282 RI ISSUED 13MAR25, AND FAA FORM 8100-9 (2-02) DATE 21MAR25. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032100366Skin · dentedRH WING, INBOARD TRAILING EDGE FLAP, LOWER SECTION, OUTER SKIN WITH DENTS.(<P>RH WING, AFT FLAP - INBOARD TRAILING EDGE FLAP, LOWER SECTION, OUTER SKIN WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG.201 SHEET 4 PAG.2,5 AND SRM 51-70-10- 2R-4 FIG.201 SHEET 1 PAG.1,3,7 SDR UIEA2025032100367Skin · dentedRIGHT WING INBD FLAP UPPER AND LOWER SKIN WITH SEVERAL DENTS.(<P>RH WING, AFT FLAP - INBOARD TRAILING EDGE FLAP, LOWER SECTION, OUTER SKIN WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG.201 SHEET 4 PAG.2,5 AND SRM 51-70-10- 2R-4 FIG.201 SHEET 1 PAG.1,3,7 REV.127 15 DESDR UIEA2025032100368Skin · delaminatedRH WING, OUTBOARD FLAP, LOWER SURFACE, 9" TO 24" FROM INBOARD EDGE AND 23.5" TO 34" FROM LEADING EDGE, DELAMINATION.(<P>RH WING, OUTBOARD FLAP, LOWER SURFACE WAS REPAIRED I.A.W B767 SRM 57-53-01-2R-1 AND SRM 51-70-10-2R-4 PAG 1,4 FIG 201 SHEET 3 REV 127 15-DECSDR UIEA2025032200376Skin · corrodedRH WING INBOARD TE FLAP, CORROSION LOWER SKIN.(<P>RH WING INBOARD TE FLAP, LOWER SKIN WAS REPAIRED IAW TRE 6757282 R1 ISSUED 13MAR25, AND FAA FORM 8100-9 (2-02) DATE 21MAR25. NO FURTHER DEFECTS NOTED</P>)SDR FDEA202503230483Skin · crackedLEFT WING OUTBD TE FLAP LEADING EDGE WITH CRACK AT WS 746.2. LEFT WING OUTBOARD T/E FLAP L/E SKIN AT WS 746.2 WAS REPAIRED I.A.W. B767 SRM 57-53-01-2R FIG. 201 SHEET 5 TABLE I AND SRM 51-70-03-0G PARAG 5.B. FIG. 15. REV 90 AUG15,2024SDR DALA2025032402191Skin · dentedDENT ON UPPER MID AREA NEAR L/E AT LH WING FWD MOVABLE VANE. SUMMARY OF NRC 00554: AREA DAMAGE WAS REPAIRED ON UPPER MID AREA NEAR L/E AT LH WING FWD MOVABLE VANE PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 PAR 4. (LP #0873498)SDR FDEA202503220471Skin · dentedRH WING, INBOARD FLAP, AFT FLAP, LOWER SURFACE WITH DENT RH WING, INBOARD FLAP, AFT FLAP, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-53-01-2R REPAIR 1 FIG 201 (SHEET 4), SRM 51-70-10-2R REPAIR 2 FIG 202 (SHEET 1) AND SRM 51-70-03-0G PAR 5.A REV 90 AUG 15,SDR SWAA2025042854207Skin · debondedDEBONDED OB AFT FLAP INBOARD SIDE AT RT WING. PERFORMED INTERIM REPAIR AT OB AFT FLAP INBOARD SIDE AT RT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. AND THE REPAIR REQUIRED TAP TEST INSPECTION EVERY 6;875 CYCLES OR 30 MONTHS WHICHEVER COMES FIRST.SDR 2025F00072Lug · corrodedREMOVED RH MIDDLE FLAP ASSEMBLY TO WORK CORROSION ON FWD, OUTBD LUG. MECHANICALLY REMOVED RH MIDDLE FLAP ROLLER, OUTBD LUG CORROSION, INBD SURFACE IAW C680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND C680 SRM 51-70-02 LIMITATIONS EXCEEDING .002" OF MATERISDR SWAA2025042407808Web · crackedR/H UPPER FIXED TRAILING EDGE PANEL ATTACH WEB INBOARD OF DEFLECTION RIB IS CRACKED. <[01] REMOVED DAMAGED WEB PER SRM 51-40-02.; [02] REMOVED AND REPLACED RT WING UPPER FIXED TRAILING EDGE ATTACH WEB PER SRM 51-40-02.; [03] REMOVED AND REPLACED RT WING UPPER SDR FDEA202503200466Skin · dentedLEFT WING OUTBD TE FLAP LOWER SURFACE WITH DENT AT WS 746.2 AND AT 6'' FROM TE. LEFT WING OUTBD TE FLAP LOWER SURFACE AT WS 746.2 AND AT 6'' FROM TE WAS REPAIRED I.A.W B767 SRM 57-53-01-2R FIG 201 SHEET 6 TABLE 2 AND SRM 51-70-17-0G PAR 4-A FIG 10 REV 90 ASDR SWAA2025042423564Doubler · looseRT WING UPPER T/E PANEL LOOSE AT DEFLECTION ARM ATTACH POINT. <[01] REMOVED DAMAGE ON DEFLECTION CONTROL RIB UPPER TAB PER SRM 57-51-02-2R-4 AND REMOVED DAMAGE ON SUPPORT BEAM PER SRM 57-51-02-2R-1.; [02] C/W INSPECTION OF REPAIR AREA. ACCOMPLISHED HFEC HOLE PSDR VNAA20250320057Skin · dentedHN00204234 SN: 00651 DISCREPANCY: FOUND MULTIPLE DENTS ON L/H INBOARD FLAP INNER SKIN INBOARD SIDE. CORRECTIVE ACTION: PREFORMED A MAJOR REPAIRED TO THE L/H INBOARD FLAP IAW CRJ 700 SRM 57-52-01-201-A01SDR VNAA20250320015Actuator · corrodedHN00205126 SN: 00703 DISCREPANCY: LH IB FLAP VANE ACTUATOR AT FLS65.50 UPPER TRUNNION HAS CORROSION CORRECTIVE ACTION: LOCATED AND MACHINED 3EA HOLES IN LH IB FLAP VANE ACTUATOR ROD AT FLS 65.50 IAW CRJ 700 SRM 51-40-11-001-001-A01 REFERENCING DWG CC670-14303 SDR YENA2025032000289Skin · abnormalDURING HEAVY MAINTENANCE: DENT OB FLAP EXISTING REPAIR LOWER SURFACE ON RH WING; REF AEROMAN N/R 2025-125365, PERFORMED VISUAL AND TAP TEST INSPECTION ON EXISTING REPAIR ON O/B FLAP LOWER SURFACE ON RH WING AS PER A320 NTM 51-10-03 AND A320 NTM 51-90-00. REPAISDR LR7A2025031903752Skin · crackedDURING SCHEDULED A-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH OUTBOARD FLAP LOWER CENTER SKIN CRACKED AT OWFS249R. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 0035. (SRM REPAIRS)SDR SWIA202503260018Rivet · looseMULTIPLE SMOKEING RIVETS FOUND ON LH OUTBOARD FLAP UPPER SURFACE BETWEEN WS 162.49 - WS 178.00 AND BETWEEN WS 213.08 - WS 242.00. (C-CHECK RO 03/25/2024)REMOVED AND REPLACED MULTIPLE SMOKING RIVETS FOUND ON LH OUTBOARD FLAP UPPER SURFACE BETWEEN WS 162.49 - WS
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