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 WRXR20250318003Vane · gougedRH INB FLAP VANE ACCESS PANEL 684ET IS SHOWING SIGNS OF CHAFING. PERFORMED BLENDING ON PANEL 684ET IAW CRJ 900 SRM 51-12-00-001-001-A01. R&R BLENDED RIVETS IAW CRJ 900 SRM 51-42-06-001-001-A01. RESTORED FINISH IAW CRJ 900 SRM 51-21-11-001-001-A01, 51-25-06-00SDR WRXR20250318001Skin Panel · gougedDURING MAINTENANCE, CHAFING DAMAGE WAS FOUND ON LH INBD FLAP PANEL 584ET P/N CC670-14027-3. PERFORMED BLENDING ON PANEL 584ET. PROVIDED 2IN. X 3IN. GRID FOR NDT.SDR SWI2025F00994Beam · gougedLH INBD FLAP INBD VANE ACTUATOR BEAM IS GOUGED. (MARKED) (C-CHECK RO 07/16/2025)REPAIRED LH INBD FLAP VANE ACTUATOR BEAM. PER REO 670-57-52-257 REV -A DATED 2024-08-20. OPS CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.SDR SWI2025F00992Beam · gougedLH INBD FLAP OTBD FLAP VANE ACTUATOR BEAM IS GOUGED. (MARKED) (C-CHECK RO 07/16/2025)COMPLIED WITH REO 670-57-52-257 REV A DATE 2024-08-20 OPS CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKYSDR SWAA2025042406237Flap · delaminatedL/H WING O/B AFT FLAP HAS LARGE AREA OF DELAMINATION ON UPPER SURFACE ON I/B CORNER <[01]. RII: OK TO INSTALL L/H WING OUTBOARD AFT FLAP ASSEMBLY.; [02] INSPECTED THE WORK PERFORMED ON STEP #1; NO DEFECTS NOTED.; [03] REMOVED AND REPLACED LEFT WING OUTBOARD ASDR SWAA2025042406238Flap · delaminatedR/H WING O/B AFT FLAP HAS LARGE AREA OF DELAMINATION ON LOWER SURFACE ON I/B CORNER <[01]. REMOVED AND REPLACED RIGHT WING OUTBOARD AFT FLAP PER. AMM. 27-51-22. OUTBOARD AFT FLAP ADJUSTMENT GOOD IAW AMM 27-51-22; [02] INSPECTED WORK PERFORMED.SDR SWAA2025032107867Flap System · locked<SDR DXTA2025031802728Seal · out of positionWHILE DESCENDING TO IAH ALL THE SUDDEN WE STARTED FEELING VIBRATION AND LOUD HUMMING SOUND WHAT SOUND LIKE A LOOSE LAV CAP. UPON INSPECTION AFTER LANDING, LAV CAP IS INTACT BUT THE RIGHT SIDE FLAP SEAL IS BEING PUSHED DOWN BY RIGHT INBOARD FLAP. CORRECTIVE ACSDR JR2R20250316763Support · chafedLEFT HAND WING, #1 FLAP TRACK SUPPORT, FORWARD INBOARD LUG, HAS 2 CHAFE MARKS.SDR SWAA2025040905686Plate · crackedWIGGLE PLATE ON L/W T/E ORSS 261 IS CRACKED <[01]. REMOVED AND REPLACED WIGGLE PLATE ON L/W T/E AT ORSS 261 IAW SRM 51-40-02-0G-0 PARA. 4.; [02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.SDR UIEA2025031900337Support · corrodedRIGHT WING TRAILING EDGE OUTBOARD FLAP SUPPORT #7, SUPPORT ACTUATOR HOLE WITH CRACK INDICATION AT 6 O´CLOCK APPROX.(<P>RIGHT WING TRAILING EDGE OUTBOARD FLAP SUPPORT #7, SUPPORT ACTUATOR HOLE WAS REPAIRED IAW TRE6757276 ISSUED DATE 21/FEB/25 & CMA-TLS-25-0006SDR UIEA2025031940336Support · corrodedRIGHT WING TRAILING EDGE OUTBOARD FLAP SUPPORT #8, SUPPORT ACTUATOR HOLE WITH CORROSION INDICATION.(<P>RIGHT WING TRAILING EDGE OUT BOARD FLAP SUPPORT #8, SUPPORT ACTUATOR HOLE WITH CORROSION LEVEL 2 WAS REPAIRED IAW TRE6757275 ISSUED DATE FEBRUARY 21, 2025. FSDR UIEA2025031900255Skin · dentedLH WING INBOARD TRAILING EDGE FLAP, LOWER AREA UPPER SKIN WITH SEVERAL DENTS.(<P>ONE DENT WAS REPAIRED IAW SRM 57-53-01-2R-1 PAG.1-7 FIG. 201 SHEET 4 AND SRM 51-70-10-2R-4 REPAIR 4</P> / <P>FIG.201 SHEET 1 PAG.1-22 AND THREE FOUND WITHIN LIMITS IAW B767 SRM 57SDR UIEA2025031960223Support · crackedLEFT WING TRAILING EDGE INBOARD FLAP 4 SUPPORT MECHANISM 6-6 OUTER PIN WITH CRACK INDICATION.(<P>THE 6-6 OUTER PIN OF THE LH WING INB FLAP SUPPORT #4 WAS REPLACED IAW AMM 27-51-04-402-135 REV.144 DATE: 22DEC24 TORQUE WERE APPLIED 1000 LB/IN S/N: 0823114442 D/DSDR UIEA2025031500348Flap Track · corrodedRH WING INBOARD FLAP TRACK #6 SUPPORT AFT ATTACHMENT HOLES, BORE WITH CORROSION (4EA).(<P>CORROSION ON RH WING INBOARD FLAP TRACK #6, AFT ATTACHMENT HOLES WAS REPAIRED I.A.W. TRE6757278 R1 ISSUED DATE 05/MAR/25. FAA FORM 8100-9 (2-02) ISSUED DATE 14/MAR/25. NOSDR UIEA2025031500347Flap Track · corrodedLH WING INBOARD FLAP TRACK #3 SUPPORT FWD INBOARD ATTACHMENT HOLE, BORE WITH CORROSION (FLAP STRUCTURE).(<P>LH WING INBOARD FLAP TRACK #3 SUPPORT FWD INBOARD ATTACHMENT HOLES (FLAP STRUCTURE) WERE REPAIRED I.A.W. TRE6757280 ISSUED DATE 04MAR25 AND TRE6757279 RSDR UIEA2025031500346Support · corrodedRH WING INBOARD FLAP TRACK #6 SUPPORT FWD ATTACHMENT HOLES, BORE WITH CORROSION (2EA).(<P>CORROSION ON RH WING INBOA RD FLAP TRACK #6 FWD ATTACHMENT HOLES, WAS REPAIRED I.A.W. TRE5757281 ISSUED DATE 05MAR25 & CMA-TLS-25-0018. FAA FORM 8100-9 (2-02) ISSUED DATESDR FDEA202503150421Skin · damagedRH WING O/B FLAP UPPER SKIN AT T/E RIB14A-15A WORN, AS MARKING. REPAIRED THE RH WING O/B FLAP WORN UPPER SKIN AT T/E RIB14A-15A PER A300-600F SRM51- 75-20 & EA 6-5750-T0382575 P1, EA TITLE: WING - FLIGHT SURFACES - RH OUTER FLAP TRAILING EDGE UPPER SKIN WEASDR SWAA2025042205333Flap · debondedCUSTOMER REQUEST- DEBONDED OB AFT FLAP IB SIDE AT LT WING 2025-202755 <[01]. TOOL USED; CALIPER PN: 500-196-30; SN: A21334230; DUE DATE: 23-MAY-25.; [02] TOOL USED: AUDIBLE BOND TESTER; P/N: S-3; S/N: 064; DUE DATE: 27-AUG-25.; [03] TOOL USED HOT BONDER: P/N: SDR SWI2025F00482Skin · gougedGOUGE FOUND AT RH INBD FLAP (MARKED) MX 29796578 (C-CHECK RO 04/17/2025)COMPLIED WITH REO 601R-57-52-2513 REV -- DATE 2025-03-18 REPAIR TO THE RH INBD FLAP.SDR IPXA2025032041995Skin · damagedBROKEN - PANEL, RIGHT WING INBOARD AFTER FLAP UPPER SURFACE WBL 104. (REPAIR). I.A.W AMM 51-21-10-307-020 REV.144 REPAINT REWORK AREA. ACCOMPLISH THE REPAIR PER SRM (REV. 91) 51-70-10-2R-0, AND 51-70-10-2R-2. THIS IS A PERMANENT REPAIR.SDR JR2R20250314753Bushing · looseFOUND LOOSE BUSHING ON #1 FLAP TRACK SUPPORT.SDR FDEA202503130389Skin · dentedFOUND RHW T/E I/B AFT FLAP LOWER SURFACE DENT AT THE CROSS ITEF 250 AND T/E 2 INCHES. REPAIRED RHW T/E I/B AFT FLAP LOWER SURFACE DENT AT THE CROSS ITEF 250 AND T/E 2 INCHES AS PER B777 SRM 57-53-01-2R-1. SRM 51-70-04-2R-1 REV 47.5 AND EA:G-5750-T0382576 P1.SDR SWAA2025031704476Bracket · crackedUPPER T/E SHELF PANEL JUST AFT OF #1 PYLON FWD UPPER BRACKET CRACKED. <[01] R&R UPPER T/E SHELF PANEL JUST AFT OF #1 PYLON FWD UPPER BRACKET PER SRM 51-40-02;[02] C/W INSP.R&R UPPER T/E SHELF PANEL JUST AFT OF #1 PYLON FWD UPPER BRACKET PER SRM 51-40-02.SDR SWAA2025031704104Tail Cone · cracked#3 FLAP TRACK FAIRING TAILCONE CRACK <[01]. MATCH DRILLED NEW # 3 FLAP TRACK FAIRING TAILCONE PER SRM 51-40-05;[02] REMOVED AND REPLACED #3 FLAP TACK FAIRING TAIL CONE IAW AMM 51-10-02.SDR DALA2025100807322Skin · corrodedEXFOLIATING CORROSION FOUND ON RIGHT WING REAR SPAR LOWER CAP AT APPROXIMATELY STATION XRS=164. (6925752)SDR SWAA2025041403931Skin · delaminatedL/H MAIN FLAP T/E WEDGE HAS 2 SMALL AREAS OF DELAMINATION<[01] REMOVED DAMAGE TO AREA PER SRM 57-53-01-2R-7.;[02] 02 - INSPECTED PER [SRM 57-53-01-2R-7-B00269 (REPAIR 7 - INBOARD MAIN FLAP TRAILING EDGE WEDGE - PERMANENT)];[03] PART TOOLING UPDATE.;[04] REPAIRSDR SWAA2025041403932Skin · delaminatedR/H MAIN FLAP T/E WEDGE HAS SMALL AREA OF DELAMINATION.<[01] REMOVED DELAMINATIOM DAMAGE PER SRM 57-53-01-2R-7.;[02] VERIFIED REMOVAL OF DAMAGE ONLY;;[03] REPAIRED PER SRM 57-53-01-2R-7.;[04] C/W INSPECTION OF REPAIR AREA NO DEFECTS NOTED.;[05] RESTORED FINISHSDR NACA2025031000004Skin · damagedTHE DAMAGE WAS FOUND AT LH WING O/B AFT FLAP LOWER SKIN , WBL 365.4 , L:1.8 INCH , W:0.7 INCH. PERFORMED CATEGORY A METAL BOND REPAIR AT LH WING I/B AFT FLAP LOWER SKIN. WBL 365.4 REMOVED THE OLD DOUBLER AND USED A LARGE DOUBLER FOR THE OLD DAMAG AND THE NEW DSDR NACA2025031000003Skin · gougedRH WING O/B AFT FLAP SKIN DISBOND BETWEEN WBL 230.68 ~ WBL 233.68. REMOVED THE DISBOND END CAP AT RH WING O/B AFT FLAP BETWEEN WBL 230.68~WBL 233.68. MADE A NEWW PRE-CURED FIBERGLASS END CAP AND INSTALLED WITH SEALANT. I.A.W. BOEING SB 737-57-1219 PG 32, PARA SDR NACA2025031000002Skin · gougedRH WING O/B FORE FLAP UPPER SKIN GOUGE FOUND AT WBL 413.(DAMAGE :L:0.2" ,W:0.3",D:0.030") PERFORMED CATEGORY A METAL BOND REPAIR AT RH WING O/B FORE FLAP UPPER SKIN WBL 413 I.A.W. B737-300 SRM 57-53-02 REPAIR 2 AND SRM 51-70-10 REPAIR 2 (REV135)SDR SWAA2025033114799Skin · delaminatedL/H O/B AFT FLAP IS DELAMINATING ON I/B SIDE LOWER CORNER<[01] REMOVED L/H O/B AFT FLAP. REF AMM 27-51-22;[02] RII. VERIFIED. REMOVED L/H O/B AFT FLAP. REF AMM 27-51-22;[03] RII. OK TO INSTALL L/H O/B AFT FLAP. REF AMM 27-51-22;[04] INSTALLED L/H OB AFT FLAP. SDR AALA202503285532Flap Track · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT WING FLAP TRACK FAIRING NUMBER 6 HAS EXCESSIVE PLAY. REMOVED AND REPLACED RIGHT WING FLAP TRACK AFT FAIRING NUMBER 6 (AALA202503285532), PER B737-NG AMM 27-51-18. REMOVED AND REPLACED AFT FAIRING NUMBER 6 ATTACH BEAM ASSEMBLSDR AALA202503287788Fairing · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT WING FLAP TRACK FAIRING NUMBER 6 HAS EXCESSIVE PLAY. REMOVED AND REPLACED RIGHT WING FLAP TRACK AFT FAIRING NUMBER 6 (AALA202503285532), PER B737-NG AMM 27-51-18. REMOVED AND REPLACED AFT FAIRING NUMBER 6 ATTACH BEAM ASSEMBLSDR SWAA2025032404018Skin · delaminatedL/H O/B AFT FLAP IS DELAMINATING ON I/B SIDE LOWER CORNER<[01] REMOVED L/H O/B AFT FLAP. REF AMM 27-51-22;[02] RII. VERIFIED. REMOVED L/H O/B AFT FLAP. REF AMM 27-51-22;[03] RII. OK TO INSTALL L/H O/B AFT FLAP. REF AMM 27-51-22;[04] INSTALLED L/H OB AFT FLAP. SDR UIEA2025030600212Flap · damagedTRANSFER FROM ADD PAGE 2 OF 11, MDDR 224933 - RH WING VARIABLE CAMBER FLAP PERM REPAIR DUE WITHIN 25FC IAW EA-1957A200.(<P>RH WING VAIABLE CAMBER FLAP PERM REPAIRED AS PER B747-400F SRM 51-70-17 PARA 5B REV.103 & EA 1957A200 PART 3. DMI 224933 CLOSED.</P> / <!SDR SWAA2025031203790Fairing · pulled#3 FLAP FAIRING RUB STRIP RIVETS PULLED THROUGH <[01]. REPAIRED #3 FLAP FAIRING REF SRM 57-53-70-2R-2 ALTERNATIVE 1 REPAIR 2. REPAIR INSPECTION DUE 500 FC. HOLE DIAMETER DIMENSIONS: 0.255; 0.302; 0.303; 0.287; 0.245.; [02] ADDED TOOLING; [03] CW; [04] AFTERSDR DALA2025031101893Hinge Fitting · corrodedRIGHT WING INBOARD FLAP HINGE FITTING LOWER OUTBOARD STUD ON AFT SPAR HAS HEAVY RUST/PITTING. SUMMARY SEE NRC 004-0001:5720-01103-01B/006 00006: CORROSION LEVEL 2. REPLACED 4 EA MOUNTING STUDS PER B717 AMM 57-55-25-300-801. (LP #0849083)SDR SWAA2025033103168Skin · debondedRIGHT O/B T/E AFT FLAP I/B CORNER LOWER SKIN AND UPPER SKIN HAVE DISBONDS. (MARKED)<[01] REMOVED AND REPLACED RIGHT O/B T/E AFT FLAP PER AMM 27-51-22-401;[02] COMPLETED ALL STEPSSDR SWAA2025033103167Skin · debondedLEFT I/B MAIN FLAP T/E LOWER SKIN IS DISBONDED. (MARKED)<[01] REMOVED AND REPLACED LEFT I/B MAIN FLAP T/E LOWER SKIN PER AMM 20-50-11-910-801 AND SRM 51-40-050G-0 AND BOEING DWG 113A2100 REV.: A.;[02] VERIFIED CORRECTIVE ACTION 1;[03] VERIFIED CARD COMPLETESDR FDEA202503080494Rib · damagedLH WING I/B FLAP INTERNAL STRUCTURE WAS FOUND 1EA FASTENER HOLE ENLARGED AT RIB25A RS PLUS 5" FABRICATED WEB AND INSTALLED WITH FASTENERS AT LH I/B FLAP RIB25A RS PLUS 5" I.A.W AIRBUS DRAWING NO:A57960114 REV E SHEET 1 & A300-600 SRM 51-40-21-001, PARA7 PSDR SWIA202509020006Vane · chafedRIGHT INBOARD FLAP VANE IS CHAFED, 67" FROM THE INBOARD END OF THE FLAP. REPLACED VANE CAP RUB STRIP REF CRJ-700 SRM 51-42-13-001-001-A01, DWG: CC670-14010 REV F. COMPLIED WITH TASK CARD 51-900-1002-SKYSDR DALA2025030701777Skin · delaminatedLHW I/B FLAP, AFT FLAP UPPER SURFACE DELAMINATION AT FROM I/B EDGE 63 INCH AND AFT EDGE 2 INCH. LHW I/B FLAP AFT FLAP UPPER SURFACE REPAIRED AT FROM I/B EDGE 63 INCH AND AFT EDGE 2 INCH PER B767-300 SRM 57-53-01-2R-1 AND 51-70-10-2R-4, REV 126.00. AUG-22-2024.SDR SWAA2025041402048Skin · delaminatedRIGHT WING O/B AFT FLAP UPPER SURFACE ON THE I/B END IS DELAMINATED<[01] RIGHT WING O/B AFT FLAP UPPER SURFACE ON THE I/B END IS DELAMINATED; WAS REPAIRED IAW SRM 57-53-01-2R-4 AND SRM 51-70-10-2R-0.;[02] COMPLETESDR IPXA2025032645221Skin · damagedFAULT - SINK - SCREWS, L/H WING OUTBOARD AFT FLAP INBOARD SIDE EDGE (AGING A/C INSPECTION) (REPLACE). REPAIR GOUGE DAMAGE ON INBD EDGE OF L/H OUTBD AFT FLAP UPPER PANEL NEAR WBL 515 I.A.W. EGAT EI NO. F2025A57M-532 REV.1 AND UPS EO-93259-REQ1 REV.1 REVIEW COSDR DALA2025030501711Hinge Fitting · damagedAN ELONGATED HOLE WAS FOUND AT THE RH WING FLAP HINGE FITTING #3 PIVOT POINT. SUMMARY OF NRC 00535: RH WING FLAP HINGE FITTING #3 WAS REPAIR PER PRI 624272-14 REV 1 AND ER/A 624272-14 REV ORIGINAL. ASSOCIATED ER/A 14-624272 ADDED FOR AC 9514. (LP #0840814)SDR DALA2025030501710Hinge Fitting · corrodedAN ELONGATED HOLE INBD ON INBD FACE ON HINGE FLAP #3 AT LH WING, ALONG WITH CORROSION ON BOTH HOLES INBD/OUTBD HINGE. SUMMARY OF NRC 00543: HINGE FLAP #3 AT LH WING WAS REPAIRED PER PRI 624271-14 REV 1 AND ER/A 624271-14 REV ORIGINAL. ASSOCIATED ER/A 14-624271SDR SWIA20250430003Hinge Arm · gougedRH IB FLAP HIMGE ARM GOUGED EVAL (WS 128.00) (C-CHECK RO 04/30/2025)PERFORMED REPAIR ON RH IB FLAP HINGE WS128.00 LUG FOUND TO BE STRUCTURRALLY ACCEPTABLE IAW REO 670-57-52-604 REV -- DATE 2025-04-03, CRJ 700 SRM 57-52-27, 51-12-00, NDT PERFORMED BY BARON DNTSDR SWIA20250418303Hinge Arm · gougedRIGHT OUTBOARD FLAP HINGE ARM AT WS220.00 GOUGED NEAR LOWER ATTACH FITTING AS MARKED (C-CHECK RO 04/17/2025) BLENDED GOUGE AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ REO 601R-57-54-374 REV -- DATE 2025-03-17. SEE CONTINUATION CARD FOR DETAILS.SDR IPXA2025032329386Skin · dentedDENT - SKIN, R/H WING INBOARD AFT FLAP LOWER SKIN, 2 PLACE, (AGING A/C INSPECTION) (REPAIR). REPAIR DENTS WITH AN ESISTING REPAIR ON THE LOWER SURFACE OF THE RH WING INBD FLAP I.A.W. UPS EO-93256-REQ1 REV.1 AND EGAT EI NO. F2025A57M-505 REV.1. CONDITION CHE
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