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 VNAA2025052711101Fairing · missingRH INBOARD 2ND FLAP FAIRING MISSING, LOST IN FLIGHT / REMOVED WHAT WAS LEFT OF PANEL 686BB ON RH WING INBD FLAP IAW CRJ 700 AMM 57-51-84-000-802-A01.May 24, 2025 · N516AE · Cndair CL6002C10SDR SWAA2025060274531Skin · delaminatedDELAMINATED LOWER SURFACE AFT TRAILING EDGE RH MAIN INB FLAP<[01] OK TO INSTALL;[02] REMOVED AFT TRAILING EDGE RH MAIN I/B FLAP AND INSTALLED NEW AFT TRAILING EDGE RH MAIN I/B FLAP (WEDGE ASSEMBLY) P/N 113A2500-14 IAW AIPC 27-51-11-01B AND AMM 20-50-11-910-801May 23, 2025 · N285WN · Boeing 7377H4SDR SWAA2025063074223Fairing · crackedCRACK ON INTERNAL SKIN OF ACCESS PANEL 644BB FLAP SUPPORT FAIRING 8 AT RT WING 2025-335582<[01] REPAIRED ACCESS PANEL 644BB FLAP SUPPORT FAIRING 8 AT RT WING IAW 25-157-01493-WIP. SEE INDIVIDUAL SIGNOFFS BELOW;[02] REPAIRED ACCESS PANEL 644BB FLAP SUPPORT FAIRMay 22, 2025 · N295WN · Boeing 7377H4SDR FDEA202505220792Skin · wornLEFT WING FLAP OUTBOARD ON EDGE BETWEEN ACCESS PANEL 573BB AND OUTBOARD SIDE WITH EROSION LH WING OUTBOARD FLAP BTW ACCESS PANEL 573BB AND OUTBOARD SIDE WAS REPAIRED IAW B767 SRM 57-53-01-2R AND SRM 51-70-30-0G PAR 5A FIG 5 SHEET 1 REV 90 AUG 15-2024May 22, 2025 · N178FE · Boeing 7673S2FSDR IPXA2025081263703Skin · dentedBIRD STRIKE OBSERVED ON L/H INBOARD FLAP. ALL STEPS OF EO-93777-REQ3. THIS REPAIR IS CONSIDERED PERMANENT, AND THIS DEFERRAL IS NOW CLOSED.May 19, 2025 · N582UP · Boeing 7474R7FSDR DALA2025052203941Hinge Fitting · corrodedSHIP 9577 AFTER SEALANT REMOVAL CORROSION WAS FOUND ON ( OTBD LOWER ATTACHING BOLT ) MID FLAP HINGE FITTING STA XW= 251.6 AT RH WING. CORRECTIVE ACTION: STUDS WERE REPLACED AND CENTER WING FLAP HINGE WAS REPLACED BY SERVICEABLE CENTER WING FLAP HINGE PER B717 May 19, 2025 · N921AT · Boeing 717200SDR DALA2025052203937Hinge Fitting · wornSHIP 9577 ELONGATED BORE OF INB LUG AND WEAR ON BUSHINGS AND HARDWARE OF OUTBD FLAP HINGE FITTING STA XRS 383 AT RH WING. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ERA 625998-14 REV ORIGINAL AND PRI 625998-14 REV 2. (0969698)May 16, 2025 · N921AT · Boeing 717200SDR 2026FA0000354Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF AND/OR CRACKEDMay 14, 2025 · N242AV · Cessna 172LSDR SWAA2025061669934Skin · delaminatedRIGHT WING OUTBOARD AFT FLAP HAS DELAM ON UPPER INBOARD AFT SURFACE.<[01] REMOVED R/H WING O/B AFT FLAP PER AMM 27-51-22.;[02] OK TO INSTALL RIGHT WING OTBD FLAP.;[03] INSTALLED SERVICEABLE R/H O/B AFT FLAP PER AMM 27-51-22.;[04] VERIFIED RII WORK ACCOMPLISHEDMay 12, 2025 · N8685B · Boeing 7378H4SDR UIEA2025051200602Skin · damagedLH INBOARD AFT FLAP DAMAGE OUT OF LIMITS 12" LENGTH AND 9" WIDTH UPPER SURFACE AND 10" LENGTH AND 5" WIDTH LOWER SURFACE.(<P>PERFORMED PERMANENT REPAIR IAW EA-1957A224, SRM 57-53-01-2R-1 AND SRM 51-70-07-0G-0. NO FURTHER DEFECTS NOTED.</P>)May 12, 2025 · N451PA · Boeing 74746NFSDR SWAA2025051968500Wedge · delaminatedRT. I/B MAIN FLAP T/E WEDGE DELAMINATED.<[01] VERIFIED ACTION ITEMS.;[02] ALL ACTIONS FOR REMOVAL AND INSTALLATION COMPLETED;[03] VERIFIED ACTION ITEMS.May 8, 2025 · N7858A · Boeing 73779PSDR SWAA2025051571256Flap Track · looseRIGHT WING I/B AFT FLAP O/B TRACK LOWER ATTACHED BEARING LOOSE FROM TRACK.<[01] R AND R RIGHT WING I/B AFT FLAP O/B TRACK IN REF AMM 27-51-16;[02] CORRECTED MEASUREMENT -FAILURE TYPE REPAIR FROM MINOR TO MAJOR; ON BEHALF OF AMT.May 8, 2025 · N563WN · Boeing 737752SDR VNAA202505080003Trunnion · corrodedFOUND CORROSION AROUND FASTENER HOLES (MARKED WITH RED TAPE) ON L/H FLAP VANE TRUNNION BODY (P#601R14261-1) @ F.L.S.102.9 CORRECTIVE ACTION: REFF. MWC HN00203957 FOR FABRICATION OF L/H FLAP VANE TRUNNION BODY (P#601R14261-1) @ F.L.S.102.9May 8, 2025 · N502AE · Cndair CL6002C10SDR SWAA2025052867661Fairing · debondedLEFT WING #3 TRAILING EDGE FLAP AFT SUPPORT FAIRING TAILCONE HAS ELONGATED FASTENERS HOLES.<[01] REMOVED AND INSTALLED SERVICEABLE LEFT WING #3 TRAILING EDGE FLAP AFT SUPPORT FAIRING TAILCONE IAW AMM 27-51-18.;[02] COMPLIED WITH STEP#2 AND CORRECTIVE ACTION#1.May 6, 2025 · N8687A · Boeing 7378H4SDR IXXA20250522002Fitting · crackedLH WING INBD FLAP HINGE ARM FOR THE AFT FLAP IS CRACKED AT THE ATTACH FLANGE COMMON TO THE LOWER SURFACE SKINMay 4, 2025 · N1049A · Boeing 76736NSDR DALA2025050503450Flap · damagedSHIP 3307 RIGHT WING OUTBOARD FLAP DAMAGED. CORRECTIVE ACTION: REPLACED AND ADJUSTED FLAP PER A330 AMM 27-54-72.May 4, 2025 · N807NW · Airbus A330323SDR DALA2025050503449Structure · damagedSHIP 3307 RIGHT WING INBOARD FLAP DAMAGED. CORRECTIVE ACTION: INSTALLED AND ADJUSTED FLAP PER A330 AMM 27-54-71-400-801-A01. THIS IS RELATED TO SDR DALA2025042203114. (7079156)May 4, 2025 · N807NW · Airbus A330323SDR SWAA2025050666934Fairing · delaminatedNUMBER 8 CANOE FAIRING FRONT (644AB) DAMAGED DELAMINATED.May 3, 2025 · N247WN · Boeing 7377H4SDR SWAA2025050666941Fairing · delaminatedNUMBER 7 CANOE FAIRING FRONT (643AB) DAMAGED DELAMINATED. OK TO CONTINUE PER MX NOTE.May 3, 2025 · N247WN · Boeing 7377H4SDR SWAA2025050666933Fairing · delaminatedNUMBER 6 CANOE FRONT TIP (642AB) DAMAGED DELAMINATED NUMBER 4 CANOE FAIRING FRONT TIP (642AB) DAMAGED DELAMINATED.May 3, 2025 · N247WN · Boeing 7377H4SDR SWAA2025050667021Skin · delaminatedLH INBD MAIN FLAP TE WEDGE IS DELAMINATED. LOCATED AND DRILLED NEW -603 WEDGE ASSY PER SRM 51-40-02; TREATED AND PRIMED BARE METAL PER SRM 51-20-01. APPLIED TOPCOAT PER AMM 51-21-99. INSTALLED NUT PLATES PER SRM 51-40-02May 3, 2025 · N474WN · Boeing 7377H4SDR 9WGA2025070154520Support · crackedDURING HEAVY CHECK MAINTENANCE LT FLAP HINGE SUPPORT WAS FOUND TO BE CRACKED. LT OTBD FLAP HINGE BRACKET ASSY WAS REMOVED AND REPLACED IAW MD-11 AMM 57-53-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 2, 2025 · N545JN · Doug MD11FSDR FDEA202505020709Skin · dentedDENT ON OUTBOARD FLAP LOWER SKIN LH WING. OTEF 184 L= 1" W= 0.600" D=0.004" A/Y=150 OUTBOARD FLAP LOWER SKIN LH WING OTEF 184 WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 FIG 201 (SHEET 3) AND SRM 51-70-10-2R REP 4 FIG 201 (SHEET 2) REV 90 AUG 15,2024May 2, 2025 · N176FE · Boeing 7673S2FSDR FDEA202505020708Skin · dentedDENT ON OUTBOARD FLAP LOWER SKIN LH WING.OTEF 171.75 L= 1.750" W= 1.300 D=0.008" A/Y= 162 OUTBOARD FLAP LOWER SKIN LH WING OTEF 171.75 WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 FIG 201 (SHEET 3) AND SRM 51-70-10-2R REP 4 FIG 201 (SHEET 2) REV 90 AUG 15,May 2, 2025 · N176FE · Boeing 7673S2FSDR NACA20250717002Skin · damagedLH INBD AFT FLAP HAS 2 DENTS ON LOWERSURFACE JUST BEHIND AND OTBD OF #5 TIRE. EVALUATED L/H I/B AFT FLAP AT LOWER SURFACE AT 2EA DENTS, FOUND DENTSTO BE NEAR EACH OTHER APPROX. .50", MINIMUM IS 3" TO OTHER DENT, AREASIS NOT WITHING ALLOWABLE LIMITS, DENTS AREMay 1, 2025 · N379CX · Boeing 767323SDR DALA2025051403723Hinge Fitting · worn-AD- LH WING, OUTBOARD FLAP HINGE POINT AC SIDE, IB FITTING WORN. COMPLIED WITH ERA 623200-14AD REV ORG. REPAIRED LH WING OUBOARD FLAP HINGE POINT AC SIDE PER ERA 623200-14AD REV ORIG. REWORKED AND BUSHED LH WING OUTBOARD FLAP HINGE POINT, INBOARD FITTING PER May 1, 2025 · N927AT · Boeing 717200SDR FDEA202505010701Skin · dentedFOUND RHW T/E O/B FLAP LOWER SURFACE DENT 01 EA AT THE CROSS OTEF 263 AND T/E 4 INCHES. REPAIRED RHW T/E O/B FLAP LOWER SURFACE DENT 01 EA AT THE CROSS OTEF 263 AND T/E 4 INCHES AS PER B777 SRM 57-53-01-2R-2 AND SRM 51-70-04-2R-1 REV 47.5 AND EA:G-5750-T0May 1, 2025 · N890FD · Boeing 777FS2SDR FDEA202505010700Skin · dentedFOUND RHW T/E I/B FLAP LOWER SURFACE DENT (LENGTH 15.5 INCHES AND WIDE 13.5 INCHES) AT THE CROSS ITEF 260 AND T/E 21 INCHES. REPAIRED RHW T/E I/B FLAP LOWER SURFACE DENT(LENGTH 15.5 INCHES AND WIDE 13.5 INCHES) AT THE CROSS ITEF 260 AND T/E 21 INCHES AS PMay 1, 2025 · N890FD · Boeing 777FS2SDR P5CA2025042100015Skin · damaged#18 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)Apr 30, 2025 · N855GT · Boeing 74787UFSDR P5CA2025042100016Skin · damaged#19 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)Apr 30, 2025 · N855GT · Boeing 74787UFSDR P5CA2025042100017Skin · damaged#20 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)Apr 30, 2025 · N855GT · Boeing 74787UFSDR P5CA2025042100018Skin · damaged#7 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)Apr 30, 2025 · N855GT · Boeing 74787UFSDR P5CA2025042100019Skin · damaged#8 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)Apr 30, 2025 · N855GT · Boeing 74787UFSDR P5CA2025042100020Skin · damaged#9 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)Apr 30, 2025 · N855GT · Boeing 74787UFSDR P5CA2025042300028Skin · damaged#21 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)Apr 30, 2025 · N855GT · Boeing 74787UFSDR REXA2025060900646Doubler · chafedINITIAL INSPECTION: SEVERAL NICKS AND WEAR AT RH WING INB FLAP LOWER SKIN PANEL LOCATED BTW FLS 15.00 AND FLS65.50. SEVERAL NICKS AND WEAR AT RH WING INB FLAP LOWER SKIN PANEL LOCATED BTW FLS 15.00 AND FLS65.50 WERE BLEND-OUT AND EVALUATED OUT OF LIMITS THEREFApr 29, 2025 · N903XJ · Cndair CL6002D24SDR REXA2025060900638Skin · chafedSEVERAL NICKS AND WEAR ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT LH WING. SEVERAL NICKS AND WEAR ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT LH WING WERE BLEND OUT PER CRJ900 SRM 51-12-00-001-001-A01, PREVIOUS REPAIR BTW FSL 15 TApr 29, 2025 · N903XJ · Cndair CL6002D24SDR SWAA2025051265576Fairing · damaged#6 CANOE FAIRING HAS ELONGATED SEAL FASTENER HOLES.<[01] A NEW #6 CANOE FAIRING WAS ORDERED FOR A/C. NEW CANOE FAIRING WILL BE INSTALLED ON FAULT # TTG8Q00ZVLVW.;[02] C/WApr 29, 2025 · N8684F · Boeing 7378H4SDR AALA202505099070Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND WING, OUTBOARD AFT FLAP INBOARD UPPER SURFACE HAS SIGNS OF DELAMINATED. ACCOMPLISHED PERMANENT REPAIR ON RIGHT HAND WING OUTBOARD AFT FLAP INBOARD UPPER SURFACE. PER B737-NG SRM 57-53-01-2R-14 REPAIR 14 AND PER B737-NGApr 29, 2025 · N845NN · Boeing 737823SDR SWAA2025052965199Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 271 RT WING. REPLACED SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 271 RT WING IAW SRM 51-40-02-0G-0 AND DWG 115A2982; SHEET: 4; REV: -.Apr 28, 2025 · N291WN · Boeing 7377H4SDR ASAA2025042857768Skin · dentedLH INBOARD FLAP LOWER SEGMENT, UNDER SURFACE SKIN HAS ONE DENT ON THE INBOARD SIDE AND MULTIPLE NICKS AROUND, IDENTIFIED WITH ORANGE STICKER # 118-001. GROUNDED - YES. ACCOMPLISHED "A" PERMANET REPAIR TO DENT ON THE I/B, L/H, AFT FLAP, LWR SKIN IAW B737-SRM 57Apr 28, 2025 · N291BT · Boeing 7379SDR 2025F00100Attach Fitting · corrodedFOUND 1 SMALL AREA OF CORROSION ON LH WING OUTBD FLAP, INBD FLAP ATTACH FITTING AND 2 SMALL AREAS OF CORROSION ON LH WING MIDDLE FLAP, INBD FLAP ATTACH FITTING. MECHANICALLY BLENDED 1 AREA ON LH WING OUTBD FLAP, INBD FLAP ATTACH HINGE FITTING/BRACKET AND 2 AREApr 28, 2025 · N307QS · Cessna 680ASDR IPXA202507316268Rib · crackedMAJOR REPAIR, CRACK FOUND ON RIB 27 AFT (RH) FLAP, MARKED IN RED VERIFIED ACCOMPLISHED E.A.#: 300-5750-27-A3921, PRELIMINARY 1, STEP# 32:Apr 27, 2025 · N139UP · Airbus A300F4622RSDR IPXA202507316163Rib · crackedMAJOR REPAIR, CRACK FOUND ON RIB 13 AFT (RH) FLAP VERIFIED STEP#33 E.A.#: 300-5750-27-A3921, PRELIMINARY 1 REPAIR IS ACCOMPLISHEDApr 27, 2025 · N139UP · Airbus A300F4622RSDR IPXA202507316270Rib · crackedMAJOR REPAIR, 2 CRACKS FOUND ON RIB 26 AFT (RH) FLAP, MARKED IN RED ACCOMPLISHED E.A.#: 300-5750-27-A3921, PRELIMINARY 1, STEP# 32.Apr 27, 2025 · N139UP · Airbus A300F4622RSDR IPXA2025052576323Rib · cracked**SDR FILED OPEN** FAULT: 2 CRACKS FOUND IN RIB 26 AFT (LH) FLAP, MARKED IN RED ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-93680-REQ1 AND VT-MAE EA 300-5750-27-A3920, REV. -.<BR><BR>CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN Apr 27, 2025 · N139UP · Airbus A300F4622RSDR IPXA2025052576327Rib · cracked**SDR FILED OPEN** FAULT: 2 CRACKS FOUND IN RIB 27 AFT (LH) FLAP, MARKED IN RED ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-93680-REQ1 AND VT-MAE EA 300-5750-27-A3920, REV. -.<BR><BR>CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN Apr 27, 2025 · N139UP · Airbus A300F4622RSDR IPXA2025050876268Rib · crackedCRACK FOUND ON RIB 27 AFT (RH) FLAP, MARKED IN RED E.A.#: 300-5750-27-A3921, PRELIMINARY 1,Apr 27, 2025 · N139UP · Airbus A300F4622RSDR IPXA2025050876270Rib · cracked2 CRACKS FOUND ON RIB 26 AFT (RH) FLAP, MARKED IN RED ADD TO STEP #23 E.A.#: 300-5750-27-A3921, PRELIMINARY 1,Apr 27, 2025 · N139UP · Airbus A300F4622RSDR IPXA2025050876163Rib · cracked**SDR FILED OPEN**FAULT: CRACK FOUND ON RIB 13 AFT (RH) FLAP VERIFIED STEP#33 E.A.#: 300-5750-27-A3921, PRELIMINARY 1 REPAIR IS ACCOMPLISHED PER. THE ABOVE REQUIREMENTSApr 27, 2025 · N139UP · Airbus A300F4622R
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