JASC 5753

Service difficulty reports · 31,515

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 QXEA2010030900164Attach Fitting · damagedRFD - C CHECK - RT OTBD FLAP VANE ATTACH FITTINGS ARE DAMAGED. DAMAGE WAS FOUND TO BE IN LIMITS FOR ATTACH FITTING/BUTE DOOR CAM AT FS 296.07 IAW CRJ700 SRM 57-53-01-101-001-A01. ALLOWED TO HAVE A REMAINING MATERIAL THICKNESS OF .030. CURRENT MATERIAL THICKMar 8, 2010 · N601QX · Cndair CL6002C10SDR FDEA201003070662Skin · misrepairedEXISTING REPAIR - LT WING INBD FLAP OTBD UPPER SURFACE FOUND WITH REPAIR PATCH AT STA XIFH 279 TO YIFH 8.5. EXISTING REPAIR AT LT WING INBD FLAP OTBD UPPER SURFACE STA XIFH 279 TO YIFH 8.5 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY SRM REPAIR SCMar 7, 2010 · N601FE · Doug MD11FSDR FDEA201003070660Skin · misrepairedEXISTING REPAIR - RT WING INBD FLAP REPAIR PATCH FOUND AT LOWER SKIN AT XIFH 195 UPPER SEGMENT AREA. EXISTING REPAIR AT RT WING INBD FLAP LOWER SKIN AT XIFH 195 UPPER SEGMENT AREA EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY SRM REPAIR SCHEME. EMar 7, 2010 · N601FE · Doug MD11FSDR FDEA201003070659Skin · misrepairedEXISTING REPAIR - RT WING INBD FLAP REPAIR PATCH FOUND AT LOWER SKIN AT XIFH 183 UPPER SEGMENT AREA. EXISTING REPAIR AT RT WING INBD FLAP LOWER SKIN AT XIFH 183 UPPER SEGMENT AREA EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY SRM REPAIR SCHEME. EMar 7, 2010 · N601FE · Doug MD11FSDR FDEA201003070657Skin · misrepairedEXISTING REPAIR - LT WING INBD FLAP REPAIR PATCH FOUND AT UPPER SKIN AT XIFH 201 UPPER SEGMENT AREA. EXISTING REPAIR AT LT WING INBD FLAP UPPER SKIN AT XIFH 201 UPPER SEGMENT AREA EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. EXISTINMar 7, 2010 · N601FE · Doug MD11FSDR SWAA101356Flap · delaminatedDURING SCHEDULED HC1 CHECK, FOUND RT WING O/B TRAILING EDGE AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Mar 7, 2010 · N398SW · Boeing 7373H4SDR SWAA101296Flap Track · wornDURING SCHEDULED 12Y CHECK, FOUND RT WING NR 6 FLAP TRACK WORN. REPAIRED FLAP TRACK PER EA.Mar 7, 2010 · N710SW · Boeing 7377H4SDR IXXA10SMN035SSkin · misrepairedDURING ROUTINE C CHECK INSP FOUND LT WING OTBD FLAP AFT LOWER SKIN PANEL HAS IMPROPER REPAIR AT STA XF 304.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTAMar 6, 2010 · N820BX · Doug DC871FSDR IXXA10SMN030SSkin · misrepairedDURING ROUTINE C-CHECK INSP FOUND RT WING OTBD FLAP FWD LOWER SKIN IMPROPER REPAIR AT STA XF 227.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUND. FABRICATED NEWMar 6, 2010 · N820BX · Doug DC871FSDR DL76G100822Skin · delaminatedDAMAGE OCCURRED TO LOWER SKIN CAUSING DELAMINATION TO EXTENT THAT LOWER SKIN AND SOME LOW DENSITY HONEYCOMB CORE REQUIRED REPLACEMENT. C/A: COMPLY WITH ER/A 480754-14.Mar 6, 2010 · N155DL · Boeing 7673P6SDR IXXA10SMN036SSkin · misrepairedDURING ROUTINE C-CHECK INSP FOUND LT WING OTBD FLAP FWD UPPER SKIN HAS IMPROPER REPAIR AT STA XF 432.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH Mar 6, 2010 · N820BX · Doug DC871FSDR IXXA10SMN034SSkin · misrepairedDURING ROUTINE C CHECK INSP, FOUND LT WING OTBD FLAP FWD LOWER SKIN HAS IMPROPER REPAIR AT STA XF 193.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITHMar 6, 2010 · N820BX · Doug DC871FSDR DALA1011830661Skin · chafedCHAFING MARKS ON LT WING INBD MAIN FLAP L/E SKIN OTBD END APPROX 30" LONG. ACCOMPLISHED ER/A 482402-14, REF ORIGINAL, REF NON ROUTINE 159370 (DL757101359).Mar 5, 2010 · N661DN · Boeing 757232SDR A6WA201040212Structure · chafedLT WING T/E INBD SIDE OF OTBD FLAP HAS CHAFING DAMAGE. REO 601R-57-51-447.Mar 5, 2010 · N435AW · Cndair CL6002B19SDR FDEA201003050645Support · gougedLT WING T/E INBD FLAP OTBD CARRIAGE FOUND GOUGE ON OTBD EDGE OF THE ARM. GOUGED ARM OF LT INBD FLAP OTBD CARRIAGE REPAIRED IAW EA NR F-5750-135811 (LT INBD MAIN FLAP OTBD CARRIAGE FWD ROLLER SUPPORT GOUGE REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100Mar 5, 2010 · N936FD · Boeing 7572T7SDR AALA20100304TUL05Vane · wornRIGHT WING WORN AREAS OUTBOARD FLAP INBOARD VANE INBOARD LEADING EDGE. DID HOT BOND REPAIR PER SRM 51-70-02.Mar 4, 2010 · N7537A · Doug DC982SDR SWAA101302Skin · delaminatedDURING SCHEDULED CV CHECK, FOUND RT WING O/B TRAILING EDGE AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Mar 4, 2010 · N355SW · Boeing 7373H4SDR DHLA201000050Vane · delaminatedNR 4 LT FLAP VANE DELAMINATED. R & R NR 4 LT FLAP VANE IAW MM 27-51-14, PG 201-203. REFER TO NR 225817 FOR OPS CHECK.Mar 3, 2010 · N802DH · Doug DC873SDR DHLA201000048Skin · delaminatedRT WING FLAP JOINT DELAMINATED. REMOVED DELAMINATED JOINT FLAP IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED JOINT FLAP (REPAIRED CONDITION) IAW SRM 51-3-0 SRM 51-3-1 (TORQUE) (TORQUE WRENCH: SNAP ON, MODEL: QC1R200, SN 089620045Mar 3, 2010 · N802DH · Doug DC873SDR FDEA201003030610Skin · noneEXISTING REPAIR - LT WING INBD FLAP REPAIR PATCH FOUND AT UPPER SKIN AT XIFH 149 LOWER SEGMENT AREA. EXISTING REPAIR - LT WING INBD FLAP REPAIR PATCH FOUND AT UPPER SKIN AT XIFH 149 LOWER SEGMENT AREA EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-00-0Mar 3, 2010 · N601FE · Doug MD11FSDR A6WA201040194Vane · chafedLT WING INBD FLAP VANE IS CHAFING AT 3 (EA) LOCATIONS AT STOP AREA. R & R UNSERVICEABLE 3 (EA) INBD FLAP VANE CHAFED SKIN PANEL IAW SRM 51-42-13 + B/A REO 601R-57-52-004 REV C.Mar 1, 2010 · N401AW · Cndair CL6002B19SDR A6WA201040195Vane · chafedRT INBD FLAP VANE L/E IS CHAFED AT 3 LOCATIONS. R & R UNSERVICEABLE INBD FLAP VANE CHAFED SKINS (3EA) PANELS IAW SRM 51-42-13, +B/A REO NR 601R-57-52-004 REV C.Mar 1, 2010 · N401AW · Cndair CL6002B19SDR IPXA10158822Skin · gougedINSPECTION TYPE:5 YR, RT INBD FLAP UPPER SKIN GOUGED IN SEVERAL PLACES APPROX 24 INCHES FWD OF RUB STRIP AN INBD OF NR 2 FLAP TRACK. REPAIRED IAW SRM 57-50-00, FIG. 205,Mar 1, 2010 · N165UP · Airbus A300F4622RSDR IPXA10658748Fairing · delaminatedINSP TYPE:C- LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-03 PAR 5A (1) FIG 5 REV 46.Mar 1, 2010 · N313UP · Boeing 76734AFSDR IPXA10658747Fairing · delaminatedINSP TYPE:C - RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-03 PAR 5A (1) FIG 5 REV 46.Mar 1, 2010 · N313UP · Boeing 76734AFSDR IPXA10658734Fairing · delaminatedINSPECTION TYPE:C LT WING OTBD T/E FLAP INBD L/E FAIRING DELAMINATION COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 46.Mar 1, 2010 · N313UP · Boeing 76734AFSDR SWAA101240Panel · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING I/B MIDFLAP T/E WEDGE PANEL DELAMINATED. REMOVED AND REPLACED PANEL PER SRM.Mar 1, 2010 · N386SW · Boeing 7373H4SDR IPXA10B58709Wedge · crackedINSPECTION TYPE:1C LT WING INBD AFT FLAP T/E WEDGE LWR SKIN, COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5A, FIG 5, REV 53.Mar 1, 2010 · N576UP · Boeing 74744AFSDR SWAA101197Flap · delaminatedDURING SCHEDULED OTS CHECK, FOUND RT WING O/B FORE FLAP T/E DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.Mar 1, 2010 · N522SW · Boeing 7375H4SDR UIEA201000024Fitting · crackedLT WING INBD MIS FLAP TRACK CARRIAGE FITTING SAFE LINK ATTACH BOLT BORE HOLE CRACKED. LT WING INBD MID FLAP REPLACED IAW 27-51-01.Mar 1, 2010 · N499MC · Boeing 74747UFSDR FDEA201003010570Skin · damagedLT WING OTBD FLAP UPPER SURFACE HAS SEVERAL WEEPING RIVETS. REMOVED FASTENERS. FABRICATED BEARING STRIPS. INSTALLED BRG STRIPS IN REF TO SRM 57-20-00; VOL I. ALODINE AND PRIMED BEARING STRIPS IN REF TO SRM 51-21-01; VOL II.1Mar 1, 2010 · N570FE · Doug MD1010FSDR FDEA201003010563Skin · dentedRT WING OTBD FLAP LOWER SURFACE IS DENTED AT RSS 740. FOUND DENT OUT OF LIMITS IAW SRM 57-10-00, FIG 48, VOL I. REMOVED AND REINSTALLED WEDGE IAW SRM 51-31-01, VOL II. FABRICATED DOUBLER IAW SRM 57-00-01, PG 12. APPLIED ALODINE AND PRIMER IAW SRM 51-21-01,Mar 1, 2010 · N570FE · Doug MD1010FSDR FDEA201003010553Skin · dentedLT WING T/E INBD FLAP LOWER SKIN IS DENTED AND GOUGED. LT WING T/E INBD FLAP LOWER SKIN DENT CHECKS OUT OF LIMITS IAW SRM 57-10-00, FIG 48. REMOVED DAMAGE IAW SRM 57-10-00, FIG 85. MATERIAL ID 2024-T3 0.050, PO NR 6713573 IAW SRM 57-52-01, PG 3. LOCATED ANMar 1, 2010 · N570FE · Doug MD1010FSDR FDEA201003010552Skin · dentedRT WING INBD FLAP BOTTOM SKIN IS DENTED AT XIFH 177.3 TO 183.3; 1.5 " TO 15.0 ". AFT OF THE RT WING INBD FLAP REAR SPAR.Mar 1, 2010 · N570FE · Doug MD1010FSDR FDEA201003010551Skin · dentedRT WING INBD FLAP BOTTOM SKIN IS DENTED AT XIFH 195.3 TO 207.3; 1.5 " TO 6.0 " FWD OF THE RT WING INBD FLAP REAR SPAR. DENT ID CREASED AND FOUND TO BE OUT OF LIMITS IAW SRM 57-10-00; FIG 48; VOL I. REPAIRED DAMAGED AREA IN REF TO SRM 57-10-00; FIG 85. ALODIMar 1, 2010 · N570FE · Doug MD1010FSDR AALA20100227TUL04Panel · corrodedSEVERAL AREAS OF CORROSION ON TOP INBOARD PANEL AT RIVET HEADS ALONG PANEL LEADING EDGE AND RIB LOCATED 18 INCHES FROM INBOARD. INSTALLED DOUBLER PER EA B 757-57-009242 REV B.Feb 27, 2010 · N679AN · Boeing 757223SDR AALA20100227TUL03Panel · corrodedPREVIOUSLY BLENDED AREA ON TOP INBOARD PANEL ALONG ROW OF RIVETS AFT EDGE. INSTALLED DOUBLER PER EA B757-57-009242 DATED 2/25/10.Feb 27, 2010 · N679AN · Boeing 757223SDR AALA20100227TUL02Panel · corrodedTEMPORARY REPAIR DOUBLER ON TOP INBOARD PANEL ON FORWARD INBOARD PANEL. REMOVED OLD DOUBLER AND REPAIRED AREA PER EA NUMBER B575-57-009242 REV B DATED 2-25-10.Feb 27, 2010 · N679AN · Boeing 757223SDR IPXA10558836Skin · damagedINSPECTION TYPE:C2, AFTER REMOVAL OF TEE CHORD ON CARD NR 841337 FOUND RT WING INBD MAIN FLAP OTBD UPPER SKIN PANEL 2 EA FASTENERS AT INBD AFT EDGE TO HAVE OVERSIZED HOLES AND DAMAGED COUNTERSINKS. REPAIRED DAMAGE HOLES IAW ER NR10-1818 DATED 11MAR10.Feb 27, 2010 · N408UP · Boeing 75724APFSDR IPXA10M58793Skin · delaminatedINSP TYPE:C1, LT INBD FOREFLAP INBD AFT CORNER IS CHAFED AND DELAMINATED PERFORMED WET LAY-UP REPAIR REF SRM 57-50-80 REPAIR 2.Feb 27, 2010 · N251UP · Doug MD11FSDR IPXA10M58792Skin · dentedINSPECTION TYPE:C1, LT INBD FLAP LOWER SURFACE IS DENTED. OTBD OF SPRING CARTRIDGE CTR OF FLAP CUT OUT DAMAGED SKIN BETWEEN XIFH 231.23 & XIFH 238.32. FABRICATED & INSTALLED DOUBLER AND REPAIR SKIN SECTION REF SRM 57-50-01 REPAIR 2, FIGURE 201.Feb 27, 2010 · N251UP · Doug MD11FSDR USAA2010030190476Flap · delaminatedPIT - C11 - MAJOR REPAIR - DELAMINATION ON LEFT WING FLAP 11 FEET 10 INCHES FROM INBOARD EDGE ALONG TRAILING EDGE. REPAIRED LEFT WING FLAP 11 FEET 10 INCHES FROM INBOARD EDGE ALONG TRAILING EDGE IAW A320 SRM 57-53-00.Feb 27, 2010 · N102UW · Airbus A320214SDR IPXA10658711Hinge Fitting · crackedINSPECTION TYPE:C RT - INBD MAIN FLAP INBD HINGE FTG FOUND CRACKED. RT INBD FLAP INBD HINGE FTG AT IFS179.75 REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 REV 46 ORG MAT'L IS FORGING 7075T73, CRACK LENGTH AT INBD FLANGE IS 1.375 INCH AND OTBD FLANGE IS 0.5 INCH DAFeb 26, 2010 · N313UP · Boeing 76734AFSDR IPXA10558859Skin · chafedINSPECTION TYPE:C2, RT WING OTBD MAIN FLAP L/E INBD END CHAFED. DAMAGE FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 57-53-01-1A 1, FIG 101, DETAIL VI, ER 10-1845. EO NR: B757-5750-37029-A.Feb 25, 2010 · N408UP · Boeing 75724APFSDR IPXA10558858Skin · gougedINSPECTION TYPE:C2, RT WING OTBD MAIN FLAP L/E BULLNOSE IS GOUGED 5.5" FROM INBD END FROM INBD END. DAMAGE FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 57-53-01-1A 1, FIG 101, DETAIL VI, SRM 51-40-02-0G, ER 10-1845 UPS EO NR: B757-5750-37029-A.Feb 25, 2010 · N408UP · Boeing 75724APFSDR IPXA10558857Skin · gougedINSPECTION TYPE:C2, RT WING OTBD MAIN FLAP LE BULLNOSE IS GOUGED 5.5" FROM INBD END DAMAGED, FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 57-53-01-1A 1, FIG 101, DETAIL VI, SRM 51-40-02-0G, ER 10-1845 UPS EO NR: B757-5750-37029-AFeb 25, 2010 · N408UP · Boeing 75724APFSDR SWAA101099Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Feb 25, 2010 · N386SW · Boeing 7373H4SDR AALA20100224TUL09Rib · corrodedLEFT INBOARD AFT TRAILING EDGE FLAP ASSEMBLY HAS CORROSION INTERNALLY IN TORQUE TUBE AREA OF INBOARD RIB. REPLACED CORRODED RIB WITH NEW RIB PER ESO 90252.Feb 24, 2010 · N677AN · Boeing 757223SDR AALA20100224TUL03Vane · gougedLEFT WING NUMBER 5 VANE TRAILING EDGE HAS GOUGE. INSTALLED HOT BOND DOUBLER PER SRM 51-70-2.Feb 24, 2010 · N7530 · Doug DC982SDR AALA20100224TUL02Doubler · gougedLEFT WING NUMBER 3 VANE LEADING EDGE HAS A GOUGE ON DOUBLER. INSTALLED DOUBLER WITH HOT BOND PER SRM 51-70-02.Feb 24, 2010 · N7530 · Doug DC982
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