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.

SDR SWI2025F00577Beam · gougedS/N 0594RH INBD FLAP MOVEABLE VANE ACTUATOR BEAM #2 IS GOUGED AND PITTED. FLAGGED (C-CHECK RO 04/26/2025)REPAIRED RH I/B FLAP MOVEABLE VANE ACTUATOR BEAM #2 REF REO-670-57-52-257 REV. A, DATE 2024-08-20. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY OPS CHFeb 14, 2025 · N817SK · Cndair CL6002D24SDR SWI2025F00582Beam · gougedS/N 0589LH INBD FLAP MOVEABLE VANE ACTUATOR BEAM #1 IS GOUGED AND PITTED. FLAGGED (C-CHECK RO 04/26/2025)REPAIRED GOUGES AND PITTING ON LH I/B FLAP VANE ACTUATOR BEAM #1 IAW REO 670-57-52-257 REV -A DATED: 2024-08-20. OPS CHECK GOOD. COMPLIED WITH SKYWEST TASFeb 14, 2025 · N817SK · Cndair CL6002D24SDR SWAA2025032496261Wedge · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP TRAILING EDGE WEDGE PANEL AT LT WING 2025-139096<[01] TOOL USED CALIPER PN: 500-464; SN: B17030933; DUE DATE: 21/DEC/25.;[02] TOOL USED ON STEP 3: BONDTESTING UNIT; P/N: BONDMASTER 600M; S/N:220052310; CAL DUE DATE: 04-Feb 14, 2025 · N8613K · Boeing 7378H4SDR SWI2025F00761Lug · gougedLH O/B FLAP HINGE BOX(WS178.00) FWD MOUNT LUG GOUGED. CAMP # 29632585. (C-CHECK RO 06/23/2025)REMOVED GOUGE ON LH O/B FLAP HINGE BOX(WS178.00) FWD MOUNT LUG PER REF.CRJ/200 SRM.51-12-00-00 AND COMPLIED WITH ALL THE STEPS OF THE REO 601R-57-21-3903 REV -- DATEFeb 13, 2025 · N919EV · Cndair CL6002B19SDR SWAA2025032495999Fairing · damagedELONGATED HOLE ACCESS PANEL 544CL FLAP SUPPORT FAIRING 1 AT LT WING 2025-136774<[01] REPLACED ACCESS PANEL 544CL FLAP SUPPORT FAIRING 1 AT LT WING I.A.W. B737-800 AMM 27-51-28-400-802 STEP 5.H. (4). THE INSTALLATION IS DOCUMENTED ON TTG8Q00Y0Q6F;[02] CERTIFIEDFeb 13, 2025 · N217JC · Boeing 7377H4SDR AALA202502172619Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT WING OUTBOARD FLAP UPPER SURFACE DELAMINATED AT OUTBOARD TRAILING EDGE FLAP (OTEF) STA 258.06. REPAIRED PER SRM 51-70-04-2R REPAIR 2.Feb 13, 2025 · N788AN · Boeing 777223SDR AALA202504147779Tab · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD TRAILING EDGE FLAP TAB LOWER SURFACE DELAMINATED. REPAIRED FLAP TAB PER EA 362852Feb 12, 2025 · N171US · Airbus A321211SDR DALA2025021101078Skin · wornSHIP 1821 FOUND RH WING I/B FLAP AFT FLAP UPPER SURFACE WORN AT I/B EDGE AREA. CORRECTIVE ACTION: REPAIRED RH WING I/B FLAP AFT FLAP UPPER SURFACE WORN AT I/B EDGE AREA AS PER B767-400 SRM 51-70-10-2R-2 AND SRM 57-53-01. (0804433)Feb 10, 2025 · N845MH · Boeing 767432ERSDR JR2R20250210268Nut Plate · damagedRIGHT HAND OUTBAD FLAP LOWER SIDEHAS A DAMAGED NUTPLATE WITH NO ACCESS TO CHANGE IT. INSTALLE RIVNUT IAW ENGINEERING DATA.Feb 10, 2025 · N89304 · Emb ERJ170200LRSDR IXXA2025020702Skin · dentedLT I/B MAIN FLAP HAS A LARGE DENT ON THE LEADING EDGE THAT IS DELAMEDFeb 7, 2025 · N239AZ · Boeing 767323SDR IXX2025F00002Skin · dentedLT I/B MAIN FLAP HAS A LARGE DENT ON THE LEADING EDGE THAT IS DELAMEDFeb 7, 2025 · N239AZ · Boeing 767323SDR SWAA2025031493986Flap · debondedCUSTOMER REQUEST - DEBONDED OB AFT FLAP ON IB SIDE AT LT WING 2025-112824 <[01]. TOOL USED ON STEP 4: BONDTESTING UNIT; P/N: BONDMASTER 600M; S/N:220052310; CAL DUE DATE: 04-DEC-25; [02] TOOL USED HOT BONDER PN: HCS9200B; SN: 18185847; DUE DATE: 01/OCT/25.; [Feb 6, 2025 · N216WR · Boeing 7377H4SDR DALA2025100807321Hinge Fitting · corrodedIN REFERENCE TO NRC 00309: AFTER REMOVAL SEALANT WAS FOUND CORROSION ON CENTER FLAP HINGE AT LH WING. CENTER WING FLAP HINGE FITTING WAS REMOVED PER B717 AMM 57-55-25-000-802 AND CENTER WING FLAP HINGE (0797513)Feb 5, 2025 · N979AT · Boeing 717200SDR SWIA20250428205Access Panel · damagedRH IB FLAP AT APPROX. FLS24.00 HAS ELONGATED FASTENER HOLE, FOUND UPON REMOVAL OF ACCESS PANEL (C-CHECK RO 04/26/2025)REPAIRED ELONGATED HOLE AT RH IB FLAP AT APPROX. FLS24.00 REF. REO 690-57-52-510 REV -- DATE 2025-03-05 STEPS 1-13. SEE CONTINUATION CARD FORFeb 5, 2025 · N817SK · Cndair CL6002D24SDR SWI2025F00764Hinge Box · damagedFOUND (NICK(S)/GOUGE) DAMAGE AT FWD INBD SIDE OF L/H FLAP HINGE BOX AT WS 220.00 (MARKED) (C-CHECK RO 06/23/2025)REMOVED AND REPLACED THE L/H FWD INBD BUSHING ON THE L/H OUTBD FLAP HINGE BOX WS220.00 PER REO 601R-57-21-3901 REV -- DATE 2025-02-18 STEP 1. & CRFeb 4, 2025 · N919EV · Cndair CL6002B19SDR IPXA2025030765715Hinge · corrodedSTR-UPON REMOVAL OF HINGE 7 L/H O/B FLAP O/B AFT HINGE FOUND CORROSION ON MOUNTING HOLES. ACCOMPLISHED REPAIR PER EO-92991-REQ1 AND VT-SAA EA 011-5757-01-B0386 I/R. REVIEWEDFeb 4, 2025 · N255UP · Doug MD11FSDR SWAA2025020492572Tail Cone · pulledRT WING #6 FLAP CANOE FAIRING TAIL CONE HAS PULLED FASTENER ON O/B SIDE. <[01] REMOVED AND REPLACED PULLED FASTENER ON RT WING #6 FLAP CANOE FAIRING TAIL CONE ON O/B SIDE. REF SRM 51-40-02.Feb 4, 2025 · N8327A · Boeing 7378H4SDR SWIA202503060203Hinge Arm · gougedLH OTBD FLAP HINGE ARM AT WS220.00, FWD OTBD HINGE LUG ON FLAP SIDE GOUGED (C-CHECK RO 3/5/2025) REPAIRED LH OTBD FLAP HINGE ARM AT WS220.00, FWD OTBD HINGE LUG REF MHIRJ REO 670-57-53-398 REV - - DATED 2025-02-08, COMPLIED WITH 51-900-1002-SKY, FOR COMFeb 3, 2025 · N764SK · Cndair CL6002C10SDR DALA2025020400847Flap Track · out of adjustSHIP 3327 - ATB - DUE TO A F/CTL FLAPS LOCKED ECAM MSG AND FLAPS INDICATING AT 2 WHEN COMMANDED UP. CORRECTIVE ACTION: REPLACED 41CV, 43CV, AND SFCC2 AND ADJUSTED FLAP SYSTEM AND ADJUSTED L/H TRACK 4 SENSOR STRUT. OK FOR SERVICE. (6841353)Feb 3, 2025 · N827NW · Airbus A330302SDR SWAA2025030492171Flap · delaminatedLEFT WING OUTBOARD AFT FLAP HAS A LARGE DELAM ON THE LOWER INBOARD CORNER. <[01] OK TO INSTALL L/H O/B AFT FLAP.; [02] COMPLIED WITH STEP #1. 1. LEMAS SANTO; YOSVANYS 07-FEB-2025 00:04:12. INSTALLED NEW SERVICEABLE L/H O/B AFT FLAP. REF AMM 27-51-22. RII;[Feb 1, 2025 · N8682B · Boeing 7378H4SDR FDEA202502010199Rib · crackedRH WING CENTER FLAP PERFORM EA NO.:6-5750-T0381883 P1 STEP 4.A. DVI FOUND RIB 27 FLANGE CRACK BETWEEN STRINGER 2.7 AND REAR SPAR AREA. PERFORMED CUT OUT DAMAGED FLANGES AND INSTALLED REPAIR ANGLES AT RH WING CENTER FLAP RIB27, S-2.7~REAR SPAR AND EXTERNAFeb 1, 2025 · N721FD · Airbus A300B4622RSDR DALA2025020600919Attach Bracket · damaged-AD- DURING BHEC ON PRI 622371-14AD, REV 2 HOLE #4 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. HOLE #4 OVERSIZED TO 0.363" ON STEP 41 OF PRI 622371-14AD, REV 9. FREEZE PLUG INSTALLED ON PART C, STEP 12 OF PRI 622371-14AD, REV 13. HOLE WILL BE Feb 1, 2025 · N932AT · Boeing 717200SDR DALA2025020600918Attach Bracket · damaged-AD- DURING BHEC ON PRI 622371-14AD, REV 2 HOLE #3 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS 2 CRACK INDICATIONS. HOLE #3 OVERSIZED TO 0.547" ON STEP 41 OF PRI 622371-14AD, REV 9. FREEZE PLUG INSTALLED IN HOLE #3 ON STEP 12, PART C OF PRI 622371-14AD, REV 13.Feb 1, 2025 · N932AT · Boeing 717200SDR DALA2025020300784Roller · wornSHIP 3411 L/H WING, OUTBD FLAP, OUTBD UP LOCK ROLLER WORN. CORRECTIVE ACTION: R/R ROLLER PER A330 AMM 27-54-73. OK FOR SERVICE. (0789520)Jan 31, 2025 · N411DX · Airbus A330941SDR FDEA202501300152Rib · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB11 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0332530 A P2 REPAIRED RH WING CENTER FLAP RIB UPR FLANGE 1EA CRACK AT RIB11 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WINGS - FLIGHT SURFACES - CJan 30, 2025 · N741FD · Airbus A300B4622RSDR FDEA202501300151Rib · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB18, RIB20 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0332530 A P2 REPAIRED RH WING CENTER FLAP RIB UPR FLANGE 2EA CRACKS AT RIB18,RIB20 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WINGS - FLIGJan 30, 2025 · N741FD · Airbus A300B4622RSDR IPXA2025030564688Hinge · corrodedAPG, AFTER REMOVAL OF RH WING OUTB FLAP INB HINGE FLAP SIDE, FOUND MOUNTING HOLES CORRODED, 57-57. ACCOMPLISHED REPAIR PER EO-92873-REQ1 AND VT-SAA EA 011-5757-01-B0374 I/R. REVIEWEDJan 29, 2025 · N255UP · Doug MD11FSDR SWAA2025030491266Skin · debondedCUSTOMER REQUEST - DEBONDED OB AFT FLAP ON IB SIDE AT RT WING 2025-93281<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189443; DUE DATE: 06/MAR/25.;[02] TOOL USED ON STEP 4 ULTRASONIC FLAW DETECTOR P/N: EPOCH 650; S/N: 190776902; CAL DUE DATE: 15-OCT-25;[03] TJan 29, 2025 · N7857B · Boeing 73779PSDR SWAA2025013190926Panel · cracked24-157-03570-TLD (N8747Q - SWA - REPAIR - AFT INBOARD FIXED TRAILING EDGE PANEL 651FB DENT AND CRACK DAMAGES - PERMANENT) [TTG8Q00XW0SX]<[01] R&R R/H WING INBOARD FIXED TRAILING EDGE LOWER PANEL (651FB) REF AMM 57-50-02.Jan 29, 2025 · N8747Q · Boeing 7378SDR FDEA202501280143Wedge · dentedFOUND RHW T/E O/B FLAP LOWER SURFACE WEDGE 1EA DENT AT THE CROSS OTEF76.96 AND FROM T/E TO FWD 22 INCHS LONG . REPAIRED RH WING T/E O/B FLAP LOWER SURFACE WEDGE 1EA DENT AT THE OTEF STA 76.96 AS PER B777 SRM 57-53-01-2R REPAIR 3 AND SRM 51-70-05-2R REPAIR1Jan 28, 2025 · N885FD · Boeing 777FS2SDR SWAA2025012890115Skin · delaminatedL/H INBOARD MAIN FLAP DELAMINATED AT TRAILING EDGE DELAMINATION IS 22.5 LENGTH 9.5 WIDTH 3.5 INCHES FROM OUTBOARD EDGE OF LH INBOARD MAIN FLAP<[01] COMPLIED WITH EA 25-157-00209. REINSPECT DUE EVERYDAY 8 DAYS WITH PERMANENT REPAIR DUE WITHIN 131 DAYS. REF FAULJan 27, 2025 · N7845A · Boeing 73771BSDR SWAA2025021389763Wedge · delaminatedLH INBD MAIN FLAP OUTBD WEDGE T/E IS DELAMINATED.<[01] DUPLICATE FAULT REFER TO FAULT LEFT HAND WING I/B MAIN FLAP TRAILING EDGE WEDGE HAS AREAS OF DELAMINATION ON LOWER SIDE. [TTG8Q00YAQ18] FOR ORIGINAL FAULT.;[02] DUPLICATE FAULT REFER TO FAULT LEFT HAND WINJan 26, 2025 · N8681M · Boeing 7378H4SDR IPXA2025020995016Pin · corrodedFAULT: APG/ RH WING CENTER FLAP TRACK 3 PIN FLAP AND SLEEVE-LOCKING CORRODED REVIEWEDJan 26, 2025 · N137UP · Airbus A300F4622RSDR FDEA202501240135Skin · delaminatedRIGHT WING, INBOARD MAIN FLAP LEADING EDGE WITH DELAMINATION AT 10" FROM OUTBOARD EDGE RIGHT WING, INBOARD MAIN FLAP LEADING EDGE WAS REPAIRED I.A.W. B767 S.R.M. 57-53-01-2R REP 1 FIG 201 (SHEET 5) TABLE I PAGE 1,2,5 AND S.R.M. 51-70-03-06 FIG 5 PAR 5.A REJan 24, 2025 · N114FE · Boeing 7673S2FSDR SWAA2025021388974Wedge · delaminatedLEFT HAND WING I/B MAIN FLAP TRAILING EDGE WEDGE HAS AREAS OF DELAMINATION ON LOWER SIDE.<[01] REMOVED DAMAGED T/E WEDGE PER SRM 51-40-02.;[02] LOCATED AND PICKED UP MOUNTING BOLT HOLES IN NEW WEDGE IAW SRM 51-40-02.;[03] INSPECTED WORK ACCOMPLISHED IN C/A #1.Jan 23, 2025 · N8681M · Boeing 7378H4SDR SWI2025F00622Guide Fitting · chafedRH OUTBOARD WING TRAILING EDGE, INBOARD FLAP ROLLER GUIDE FITTING IS CHAFED. (C-CHECK RO 04/30/2025)CLEANED UP CHAFE DAMAGE & EVALUATED. DAMAGE FOUND TO BE WITHIN LIMITS OF REO 670-57-51-594 REV. -- DATED: 2025-04-18.OPS CHECK GOOD AT THIS TIME. REF. CRJ 700 Jan 22, 2025 · N765SK · Cndair CL6002C10SDR AALA202502053668Wedge · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND WING INBOARD FLAP TRAILING EDGE WEDGE LOWER SURFACE IS DELAMINATED. REMOVED AND INSTALLED NEW WEDGE ASSEMBLY ON LEFT HAND WING INBOARD FLAP. PER B737-NG SRM 51-40-02-0G.Jan 22, 2025 · N823NN · Boeing 737823SDR UIEA2025011600078Skin · delaminatedLH WING, L/E OUTBD FLAP, FROM INBD EDGE TO 58 INCHES TO OUTSIDE WITH DELAMINATION.(<P>LH WING, L/E OUTBD FLAP, FROM INBD EDGE TO 58 INCHES WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 10 AND SRM 51-70-17-17-0G-0 PAR.4.A REV 127. NO FURTHER DEFECTS NOTED</P>)Jan 22, 2025 · N1399A · Boeing 767306SDR FDEA202501220119Rib · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND CRACK AT RIB27 BETWEEN STGR2.6 AND STGR2.7. REPAIRED RH WING CENTER FLAP RIB UPR FLANGE CRACK AT RIB27 BETWEEN STGR2.6 AND STGR2.7 PER A300-600F SRM57-50-00-201 FIG201 & FIG205. THIS IS CAT A REPAIR. EA:6-5750- T0Jan 22, 2025 · N650FE · Airbus A300F4605RSDR WRXR20250122001Skin · gougedLH WS128.00 FLAP SKIN HAS GOUGING DUE TO AFT FAIRING 586BB SEAL. COMPLIED WITH REO 670-57-52-590 REV: -- DATED: 2025-01-07 NO DEVIATION FROM THE REO - FABRICATED 1 (EA) EXTERNAL STRAP AND 2 (EA) INTERNAL STRAPS FROM 2024 T3 AL ALLOY ALCAD .063". FABRICATED 1 (Jan 22, 2025 · N540EG · Cndair CL6002C10SDR SWAA2025022688270Skin · debondedCUSTOMER REQUEST - DEBONDED OB AFT FLAP LOWER SURFACE AT LT WING. 2025-81322<[01] TOOL USED ON STEP 3 ULTRASONIC FLAW DETECTOR P/N: EPOCH 650; S/N: 190776902; CAL DUE DATE: 15-OCT-25;[02] TOOL USED: HOTBONDER: P/N: HCS9200B S/N: 16122983 DUE DATE: 15-FEB-25;[0Jan 21, 2025 · N8612K · Boeing 7378H4SDR SWIA2025012000119Skin · dentedTRANSFER FROM EAML 1516947 : DENTS TO R/H OUTBD FLAP LOWER SKIN (DWG: 601R14536, AL ALLOY 2024-T3, 0.040€? POCKET THICKNESS, 0.050€? PAD-UP THICKNESS, REF). DENTS ARE LOCATED BETWEEN FS235.965- FS254.96 AND 10.00€? FWD OF FLAP TRAILING EDGE (BETWEEN FRONT SJan 19, 2025 · N612QX · Cndair CL6002C10SDR AALA202502101157Structure · bentAIRCRAFT IN BASE MAINTENANCE: BENT OB FLAP TRAILING EDGE AREA ON LH WING L=8.289 INCH W=2.96 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON LOWER SURFACE BTW INNER RIB14 TO RIB16 O/B FLAP T/E AREA ON LH WING IAW A319 SRM 57-53-00-300-119.Jan 18, 2025 · N773XF · Airbus A319112SDR DXTA2025012202024Structure · damagedDURING THE MAINTENANCE THE RIGHT HAND OUTBOARD FLAP WAS DAMAGED. CORRECTIVE ACTION: REPLACED FLAP. OPS CHECK GOOD. EMBRAER AMM 27-51-05.Jan 18, 2025 · N469QS · Emb EMB505SDR IPXA2025020455060Rib · crackedFAULT: LH CENTER FLAP CRACK FOUND IN RIB 13 AFT, AREA CIRCLED IN RED.ACCOMPLISHED REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A3777.Jan 17, 2025 · N137UP · Airbus A300F4622RSDR IPXA2025020455143Rib · crackedFAULT: RH CENTER FLAP - FOUND 2 CRACKS IN RIB 27 AFT, AREAS CIRCLED IN RED.ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A3776.Jan 17, 2025 · N137UP · Airbus A300F4622RSDR IPXA2025020455141Rib · crackedFAULT: RH CENTER FLAP - FOUND 2 CRACKS IN RIB 26, AREA CIRCLED IN RED.ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A3776Jan 17, 2025 · N137UP · Airbus A300F4622RSDR FDEA202501170198Rib · cracked1EA CRACK (15MM) WAS FOUND AT R/H WING CENTER FLAP RIB26 AFT AREA OF TOP SURFACE RIB FLANGE. PERFORMED CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR ANGLE AT RH WING CENTER FLAP RIB26, S-2.8~REAR SPAR AND EXTERNAL PLATE AT RIB26~27,S-2.2~REAR SPAR FOR REPAIRJan 17, 2025 · N721FD · Airbus A300B4622RSDR DALA2025012000442Track · corrodedSHIP 3147 CORROSION ON BORE BEARING TRACK 3 O/B FLAP ON RH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A # 623039-14. (0765951)Jan 17, 2025 · N347NB · Airbus A319114SDR DALA2025012000440Plate · corrodedSHIP 3136 CORROSION WAS FOUND AFFECTING THE OB AL PLATE (FACE AND BORE) AT TRACK #4 LEVEL, SPECIFICALLY AT PENDULUM SUPPORT.CORRECTIVE ACTION: REPAIRED ERA 622710-14. (0765737)Jan 17, 2025 · N336NB · Airbus A319114
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