JASC 5753

Service difficulty reports · 31,513

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 JR2R20240427726Doubler · crushedRH O/B FLAP FAIRING 633BB CRUSHED RH O/B AFT FLAP O/B AFT DOUBLERApr 27, 2024 · N85320 · Emb ERJ170200LRSDR SWI2024F00529Vane · chafedLEFT WING INBOARD FLAP VANE HAS EVIDENCE OF CHAFFING ON LEADING EDGE AS MARKED (C-CHECK RO 6/19/2024) REPLACED LEADING EDGE SKIN ON LH WING INBOARD FLAP VANE PER REF CRJ 700 SRM 51-42-13-001-001-A01 AND DWG# CC670-14010 REV -F. M-337 AND SKYWEST TASK CAApr 26, 2024 · N742SK · Cndair CL6002C10SDR SWIA20240426Skin · erodedEROSION NOTED ON R/H INBD FLAP LOWER SKIN BETWEEN FLS15-FLS38 (MARKED (C-CHECK RO 6/17/2024) R/H I/B FLAP LWR SKIN REPAIRED REF CRJ 700 SRM 57-52-01-201-005-A01. REF CONTINUATION SHEET FOR DETAILS. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.Apr 26, 2024 · N722EV · Cndair CL6002C10SDR SWAA2024052879604Skin · delaminatedLT IB FLAP UPPER SURFACE OF TRAILING EDGE WEDGE HAS DELAMINATION 33' FROM OB END AND ON LOWER SURFACE 4' FROM OB END. 8-58<[01] FINAL STATEMENT: REMOVED AND REPLACED WEDGE AT LT WING I/B FLAP T/E REF B737-700 SRM 51-40-02-0G-0 AND DWG# 113A2100.;[02] VERIFIED Apr 26, 2024 · N473WN · Boeing 7377H4SDR IPXA2024052092058Skin · crackedTHE L/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 26, AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90269-REQ1 AND EA 300-5750-27-A3581 REV.Apr 26, 2024 · N159UP · Airbus A300F4622RSDR IPXA2024052092103Skin · crackedTHE L/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 27, AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90269-REQ1 AND EA 300-5750-27-A3581 REV.Apr 26, 2024 · N159UP · Airbus A300F4622RSDR AALA202404296731Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT WING OUTBOARD TRAILING EDGE FLAP LOWER TRAILING EDGE SKIN DELAMINATED 390 INCHES FROM THE INBOARD END BETWEEN FLAP TRACKS #3 AND #4 AT WS 8744. REPAIRED SKIN PER SRM 57-53-00-300-120.Apr 26, 2024 · N836AW · Airbus A319132SDR IPXA2024052075373Skin · crackedTHE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 18 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV -.Apr 25, 2024 · N159UP · Airbus A300F4622RSDR IPXA2024052075328Skin · crackedTHE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 13 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV -. MAJOR REPAIR.Apr 25, 2024 · N159UP · Airbus A300F4622RSDR IPXA2024052075065Skin · crackedTHE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 12 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV.Apr 25, 2024 · N159UP · Airbus A300F4622RSDR IPXA2024052075380Skin · crackedTHE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 19 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV.Apr 25, 2024 · N159UP · Airbus A300F4622RSDR IPXA2024052075365Skin · crackedTHE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 17 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV.Apr 25, 2024 · N159UP · Airbus A300F4622RSDR IPXA2024052075478Doubler · crackedMAJOR REPAIR, THE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 11 AFT SIDE. AREA MARKED IN RED. INSTALLED NEW REPAIR FLANGE AND REINFORCEMENT REPAIR ANGLE I.A.W. A300-600 S.R.M. 51-40-21.Apr 25, 2024 · N159UP · Airbus A300F4622RSDR IPXA2024052075469Skin · crackedTHE R/H CENTER FLAP ASSY HAS MULTIPLE CRACKS (2EA) AT RIB LOCATION 26 AFT & FWD SIDES. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV-.Apr 25, 2024 · N159UP · Airbus A300F4622RSDR IPXA2024052075428Skin · crackedTHE RT CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 25 AFT SIDE. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV -.Apr 25, 2024 · N159UP · Airbus A300F4622RSDR IXXA2024042503Skin · corrodedRW OB FLAP CORRODEDApr 25, 2024 · N389AZ · Boeing 767319SDR IPXA2024061056443Repair · damagedRIGHT WING INNER FLAP HAS A DAMAGED EXISTING REPAIR DOUBLER. INSTALLED REPAIR DOUBLER AT INNER FLAP IAW SRM 57-50-00-201. APPLIED TOP COAT AT REPAIR DOUBLER ON INNER FLAP IAW SRM 51-23-10-001. ACCOMPLISH A PERMANENT REPAIR PER SRM REV. 40, 57-50-00-201 PARAGRApr 24, 2024 · N160UP · Airbus A300F4622RSDR SWIA2024061900424Hinge Fitting · chafedLH WS264.00 OUTBOARD FLAP HINGE FITTING ATTACHMENT POINTS FOR ATTACHMENT BRACKET SH670-14508-1 IS CHAFED. (C-CHECK RO 6/17/2024) REPAIRED CHAFED DAMAGES ON LH WS264.00 OUTBOARD FLAP HINGE FITTING ATTACHMENT POINTS FOR ATTACHMENT BRACKET SH670-14508-1 PERApr 24, 2024 · N722EV · Cndair CL6002C10SDR IPXA2024043056443Repair · damagedOPEN, RW INNER FLAP HAS A DAMAGED EXISTING REPAIR DOUBLER AND FILLED OUT MEASUREMENTSApr 24, 2024 · N160UP · Airbus A300F4622RSDR UIEA2024041900289Flap Track · damagedLEFT WING TRAILING EDGE OUTBOARD FLAP, TRACK #2 ON INBOARD STAP AFT LOWER HOLE ELONGATED.(<P>FLAP TRACK #2 FITTING ASSY 1-3 WITH ELONGATED HOLES (2 EA) WERE REPAIRED PER CMA-TLS 24-0138-11B. NO FURTHER DEFECTS NOTED.</P>)Apr 24, 2024 · N1489A · Boeing 76731KSDR UIEA2024041900290Skin · dentedFOUR DENTS ON RH WING, INB AFT FLAP UPPER SKIN AT: 1) IFS 114.5 AND 7" FROM T/E 2) IFS 119.5 AND 5.5" FROM T/E 3) IFS 121.75 AND 3" FROM T/E 4) IFS 122.5 AND 5.8" FROM T/E(<P>DENTS (ITEM 2,3 AND 4) ON RH WING, INB AFT FLAP UPPER SKIN WERE REPAIRED PER SRM 57-5Apr 24, 2024 · N1489A · Boeing 76731KSDR UIEA2024041900291Flap Track · corrodedRH WING INB FLAP, TRACK #6 ATTACHMENT BOLT HOLES WITH CORROSION.(<P> </P> / <P>CORROSION ON RH WING INB FLAP, TRACK #6 BOLT HOLES (2 EA) WERE REPAIRED PER CMA-TLS 24-0132-06B. NO FURTHER DEFECTS NOTED.</P> / <P> </P>)Apr 24, 2024 · N1489A · Boeing 76731KSDR UIEA2024042900324Torque Tube · corrodedRH WING INB FLAP, INB RIB TORQUE TUBE SUPPORT UPPER ATTACHMENT BOLT HOLE WITH CORROSION.(<P>CORROSION ON RH WING INBOARD MAIN FLAP END RIB AT TORQUE TUBE SUPPORT HOLES (2 EA) WERE REPAIRED PER CMA-TLS 24-0152-02B. NO FURTHER DEFECTS NOTED. </P>)Apr 24, 2024 · N1489A · Boeing 76731KSDR UIEA2024042900326Flap Track · damagedRIGHT WING TRAILING EDGE OUTBOARD FLAP, TRACK #8 ON INBOARD STRAP AFT LOWER HOLE ELONGATED.(<P>(3 EA) ELONGATED HOLES, HOLE WITH GOUGE AND HOLE WITH CORROSION ON RH WING FLAP TRACK #8 FITTING ASSY 1-3 WERE REPAIRED PER CMA-TLS 24-0137-11B. NO FURTHER DEFECTS NApr 24, 2024 · N1489A · Boeing 76731KSDR UIEA2024042900327Flap Track · damagedLEFT WING TRAILING EDGE OUTBOARD FLAP, TRACK #1 ON INBOARD STAP AFT LOWER HOLE ELONGATED(<P>TWO (2 EA) ELONGATED HOLES ON LH WING FLAP TRACK #1 FITTING ASSY 1-3 WERE REPAIRED PER CMS-TLS 24-0139-17B. NO FURTHER DEFECTS NOTED.</P>)Apr 24, 2024 · N1489A · Boeing 76731KSDR AALA202404268420Strut · out of adjustAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED ON APPROACH INTO ELP DUE TO FLIGHT CONTROL FLAPS LOCKED ECAM MESSAGE WHEN SELECTING FLAPS 3. FLIGHT CREW ACCOMPLISHED A GO AROUND AND ACCOMPLISHED THE CHECKLIST. THE AIRCRAFT LANDED SAFELY AT ELP WITH THE FLAPS Apr 24, 2024 · N747UW · Airbus A319112SDR DALA2024042404681Enclosure · crackedSHIP 180 HFEC OPEN HOLE INSPECTION OF THE RH WING TRAILING EDGE - INBOARD FLAP BOX AT SUPPORT NO.5 - INBOARD CLOSURE RIB - LOWER CHORD, INBOARD FLAP STATION 108.5 REAR SPAR FOUND 02EA HOLES CRACKS. CORRECTIVE ACTION: THE 02EA CRACK HOLE ON RH WING INBOARD FLAPApr 24, 2024 · N180DN · Boeing 767332SDR FDEA202404240276Skin · delaminatedL/H WING INBD FLAP LEADING EDGE OTBD POSITION CAP PANEL #555DB IS DELAMINATED, MPN 113T2201-413G. REPAIRED, INSTALLED, AND SEALED L/H WING INBD FLAP LEADING EDGE OTBD POSITION CAP PANEL #555DB IS DELAMINATED, MPN 113T2201-413G. IAW E.A. # H-5750-T0378910 AApr 24, 2024 · N188FE · Boeing 7673S2FSDR SWAA2024052978584Wedge · debondedDEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE OB SIDE AT LT WING. PERFORMED PERMANENT REPAIR ON I/B MAIN FLAP WEDGE PANEL LOWER SURFACE AT LT WING IAW SRM 57-53-01-2R-7 REPAIR 7.Apr 23, 2024 · N250WN · Boeing 7377H4SDR SWAA2024042978288Fairing · damagedLH AFT FLAP FAIRING TAILCONE #3 CANOE. 2EA HOLES AT THE 2 OCLOCK POSTION ENLARGED IN INTERIOR STRUCTURE OF CANOE.<[01] 01 - REMOVED AND REPLACED PER [AMM 27-51-18-400-802-NG (INBOARD FLAP SUPPORT AFT FAIRING INSTALLATION - PERMANENT)] R&R?D #3 INBD FLAP SUPPORApr 23, 2024 · N8635F · Boeing 7378H4SDR DALA2024042404680Support · wornSHIP 171 RHW TE I/B FLAP OUTBOARD LINKAGE SUPPORT NO.6 I/B FLANGE FOUND WORN. CORRECTIVE ACTION: THE REWORKED AREA BLEND OUT REPAIR AS PER PRI: 617238- 14. (0305860)Apr 22, 2024 · N171DN · Boeing 767332SDR AALA202408159229Strut · wornAIRCRAFT WAS IN BASE MAINTENANCE: WEAR ON INTERCONNECTING STRUT OB FLAP ON LH WING. REPLACED LH WING INTERCONNECTING STRUT ASSY I.A.W. AMM 27-51-44-000-001-A ANDAMM 27-51-44-400-001-A.**Apr 21, 2024 · N756US · Airbus A319112SDR IPXA2024051808924Attach Angle · brokenFLAP SIDE O/B FLAP I/B HINGE CAGE O/B "S" PANEL ATTACHED ANGLE BROKEN ATA 57-50 ACCOMPLISH EO-90304-REQ1 (VT-SAA EA 011-5753-01-B0201 I/R). ANGLE BRACKET INSTALLATION ON EA : 011-5753-01-B0201 REVISION P1 STEP 5.Apr 21, 2024 · N276UP · Doug MD11FSDR FDEA202404210650Skin · crackedPFM EA#: 6-5750-T0378801 P1 FOUND NEW CRACK AT LH WING CTR FLAP RIB26 BTWN STGR 2.7-2.8 ACCOMPLISHED THE CAT.A FLANGE REPAIR AT RIB 26 UPPER FLANGE S-2.7~S-2.8, THE REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5750-T0378801 P1, SEQ NO:1119Apr 21, 2024 · N661FE · Airbus A300F4605RSDR SWAA2024042577644Skin · pulledL/H WING; MID FLAP SUPPORT FAIRING #3; INBOARD FLAP; OUTBOARD RIVETS PULLED THROUGH. LARGEST HOLE SIZE IS .323. REFERENCE SRM 57-53-70-2R-2 REPAIR INSTRUCTIONS ALT. 1. ENGINEERING APPROVES TO INSTALL HARDWARE TO RUBSTRIP ON #3 TRAILING EDGE FLAP FAIRING PER Apr 21, 2024 · N8635F · Boeing 7378H4SDR AALA202404229229Strut · wornWEAR ON INTERCONNECTING STRUT OB FLAP ON LH WING (1 EA)E-SIG: 66256C247AAE6FE2B5779BFF - 21APR2024T1942ZApr 21, 2024 · N756US · Airbus A319112SDR FDEA202404210485Skin · delaminatedL/H WING INBOARD FLAP ASSY - THE FORE FLAP LEADING EDGE OUTBOARD POSITION CAP PANEL # 555DB IS DELAMINATED, MPN 113T2201-413G. REPAIRED L/H WING INBOARD FLAP ASSY, FORE FLAP LEADING EDGE OUTBOARD POSITION CAP PANEL # 555DB, MPN 113T2201-413G. IAW E.A. # HApr 21, 2024 · N188FE · Boeing 7673S2FSDR IPXA2024052395849Hinge Bracket · corrodedFLAP EO - R/H O/B FLAP O/B FWD HINGE #4 LUG BORE HAS CORROSION (114-79) ATA 57 REMOVE AND REPLACE HINGE BRACKET ASSEMBLY P/N ARC0503-504 PER MD11 AMM 57-53-01 REV 96.Apr 20, 2024 · N276UP · Doug MD11FSDR IPXA2024052395650Hinge Bracket · corrodedFLAP EO - R/H O/B FLAP I/B FWD HINGE #4 LUG BORE HAS CORROSION (114-75) ATA 57 REMOVE AND REPLACE HINGE BRACKET ASSEMBLY, ARC0502-508, PER MD11 AMM 57-53-01/401 REV 96.Apr 20, 2024 · N276UP · Doug MD11FSDR AALA202405076300Bracket · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING TRAILING EDGE INBOARD FLAP INTERCONNECTING STRUT ATTACH FITTING / BRACKET WORN AND BEARING HAS EXCESSIVE PLAY BETWEEN WY5238.0 AND WY5753.0, AT RIB 14. REPLACED INTERCONNECTING STRUT ATTACH FITTING / BRACKET PER SRM 51-Apr 20, 2024 · N745VJ · Airbus A319112SDR AALA202405070408Bracket · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING TRAILING EDGE INBOARD FLAP INTERCONNECTING STRUT ATTACH FITTING / BRACKET WORN AND BEARING HAS EXCESSIVE PLAY BETWEEN WY5238.0 AND WY5753.0, AT RIB 14. REPLACED INTERCONNECTING STRUT ATTACH FITTING / BRACKET PER SRM 51-4Apr 20, 2024 · N745VJ · Airbus A319112SDR SWAA2024052477056Skin · delaminatedLH INB MAIN FLAP AFT EDGE OUTB SECTION 24 INCH LENGHT DELAMINATION.<[01] DUE TO DAMAGE FOUND OUT OF ALLOWABLE DAMAGE LIMITS; REMOVED AND INSTALLED A SERVICIABLE TE WEDGE ASSY AT LT I/B MAIN FLAP AS PER B737-700 SRM 51-40-02-0G-0 PARAGRAPH 9 AND BOEING DWG 113AApr 19, 2024 · N928WN · Boeing 7377H4SDR VNAA20240524003Skin · nickedSEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT LH WING. LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 45 AT LH WING WAS REPAIRED PER CRJ900 SRM 57-52-01-201-005-A01 AND LOWER SKIN OF LH INBOARD FLAP FLS 45 TO FLS 65.5 WAS EVALUATED WApr 19, 2024 · N576NN · Bombdr CL6002D15SDR IPXA2024052389264Hinge · corrodedFLAP EO - L/H O/B FLAP OB FWD HINGE O/B #8 LUG BORE IS WORN (114-53) ATA 57 REPAIR ACCOMPLISHED TO L/H WING O/B FLAP O/B FWD HINGE REF SREO-87943-REQ001 REF LINE#1451.Apr 19, 2024 · N276UP · Doug MD11FSDR IPXA2024052389256Hinge · corrodedFLAP EO - L/H O/B FLAP O/B FWD HINGE I/B #8 LUG BORE HAS CORROSION (114-51) ATA 57 REPAIR ACCOMPLISHED TO L/H WING O/B FLAP O/B FWD HINGE REF SREO-87943-REQ001 REF LINE#1450.Apr 19, 2024 · N276UP · Doug MD11FSDR SWAA2024050977006Skin · delaminatedLEFT INBD FLAP WEDGE DELAMINATED AT OUTBD CORNER<[01] REMOVED AND REPLACED FLAP WEDGE AT LEFT I/B WING PER REF. 51-40-02-0G-0 AND DRAWING #113A2500.<BR>TOOL USED SCREW GUN 176023 CAL. DUE DATE 16-JUN-24;[02] RII...VERIFIED REMOVED AND REPLACED FLAP WEDGE AT LEApr 19, 2024 · N923WN · Boeing 7377H4SDR VNAA20240513008Flap · nickedSEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP BTW FLS 15.00 TO FLS 65.50. SEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP BTW FLS 15.00 TO FLS 65.50 WERE BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND WERE EVALUATED BTW FLS15 TO FLS42 OUT OF LIMITS Apr 18, 2024 · N574NN · Bombdr CL6002D15SDR VNAA20240513007Skin · dentedDENTS (3 LOCATIONS) ON LOWER SKIN OF RH INBOARD FLAP BTW FLS 75.60 TO FLS 92.80. DENTS ON LOWER SKIN OF RH INBOARD FLAP BTW FLS 75.60 TO FLS 92.80 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 57-52-01-101-001-A01 AND WERE REPAIRED PER CRJ900 SRM 57-52-01-201-Apr 18, 2024 · N574NN · Bombdr CL6002D15SDR VNAA20240513006Skin · nickedSEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP BTW FLS 15.00 TO FLS 65.50. SEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP BTW FLS 15.00 TO FLS 65.50 WERE BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND WERE EVALUATED BTW FLS15 TO FLS42 OUT OF LIMITS AND BApr 18, 2024 · N574NN · Bombdr CL6002D15SDR AALA202405077849Bracket · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD TRAILING EDGE FLAP INTERCONNECTING STRUT ATTACH FITTING / BRACKET WORN AND BEARING HAS EXCESSIVE PLAY. REPLACED NTERCONNECTING STRUT ATTACH FITTING / BRACKET PER SRM 51-42-11.Apr 18, 2024 · N738US · Airbus A319112
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