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.
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 SWAA063870Skin · debondedDURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD AFT FLAP LOWER SKIN SURFACE DISBONDED AT INBOARD T/E. REPAIRED FLAP PER SRM.SDR DHL2006781003Repair · gougedLEFT O/B FORE FLAP O/B END EXISTING REPAIR GOUGED & CRACKED. REMOVED EXISING REPAIR AT LEFT WING O/B FORE FLAP O/B END, FAB NEW DOUBLER REPAIR FROM P/N 2024 T3, .040, PO 9003927, DIM 4.25" X 3", TREATED AND PRIMED NEW DOUBLER & BARE METAL, INSTALLED DOUBLER RSDR IXXA06SMN329SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER SKIN HAS NON STANDARD REPAIR AT STATION XW104.000. REMOVED EXISTING SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN (AL 2024 T3 0.040”). CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INTERNSDR DHL2006781002Flap · gougedLEFT WING I/B FOREFLAP O/B END GOUGED. EVAL AREA, BLENDED OUT, AREA FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA DIM 1" X 1", FAB DOUBLER REPAIR FROM P/N 2024 T3, .040, PO 9003927, DIM 5.75 X 4.25, TREATED, PRIMED 7 INSTALLED NEW FAB PART ALL IAW B727 SRMSDR AWXA200601700Skin · delaminatedPHX - MAJOR REPAIR - RIGHT WING OUTBOARD AFT FLAP INBOARD END IS DELAMINATED, WBL 204.40. REPLACED RIGHT WING OUTBOARD AFT FLAP IAW TASK CARD R3M27034.SDR SWAA063804Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP INBOARD LOWER CORNER DELAMINATED. REMOVED AND REPLACED T/E AFT FLAP PER MM.SDR USAA061203Skin · delaminatedLT OTBD MID FLAP. REMOVED DAMAGED, FABRICATED CORE AND LAYED UP PER SRM 51-70-10, DEFECT SIZE: 3" BY 5".SDR SWAA063792Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD FORE FLAP LOWER SURFACE DELAMINATED. REMOVED AND REPLACED RT FORE FLAP PER MM.SDR A6WA200640366Skin · dentedINBOARD LEFT FLAP LOWER SKIN HAS DENT WITH GOUGE LOCATED 3.75 INCH FROM INBOARD EDGE AND 8.5 INCH FORWARD OF T/E MEASURES 2 INCHES BY 2 INCHES BY .098 INCH DEEP. REPAIRED LEFT INBOARD FLAP LOWER SKIN BY INSTALLING EXTERNAL DOUBLER IAW BSC EO 601R-57-9969. (MSDR 06FDEA03578Skin · dentedLT OB FLAP, MID LOWER SKIN NUMEROUS DENTS DOT M5582 DENTS FOUND TO BE OUT OF LIMITS IAW DC/ MD -10 SRM 57-10-00 FIG 48 VOL 1. CUT OUT DAMAGED SKIN, FABRICATED DOUBLER AND FILLER IAW DC/ MD 10 SRM 57-10-00 FIG 85 VOL 1. ALODINED AND PRIMED IAW DC/ MD SRM 51-2SDR AWXA200601690Skin · debondedMCN - RIGHT WING OUTBOARD FORE FLAP, UPPER SURFACE HAS A DEBONDED AREA 4" FROM THE OUTBOARD END. REPAIRED RIGHT WING OUTBOARD FORE FLAP, UPPER SURFACE DEBONDED AREA 4" FROM THE OUTBOARD END IAW B737-300 SRM 51-70-10, FIGURE 202, REPAIR 4.SDR AWXA200601689Skin · debondedMCN - RIGHT WING OUTBOARD AFT FLAP, INBOARD AFT CORNER IS DEBONDED. REPAIRED RIGHT WING OUTBOARD AFT FLAP, INBOARD AFT CORNER IAW B737-300 SRM 51-70-10, FIGURE 202, REPAIR 4.SDR AWXA200601688Skin · debondedMCN - LEFT WING OUTBOARD FORE FLAP UPPER SURFACE HAS A DISBONDED AREA 90" FROM INBOARD END. REPAIRED LEFT WING OUTBOARD FORE FLAP UPPER SURFACE DISBONDED AREA 90" FROM INBOARD END IAW B737-300 SRM 51-70-10, FIGURE 203, REPAIR 4.SDR AWXA200601687Skin · debondedMCN - FOUND LEFT WING OUTBOARD AFT FLAP LOWER SURFACE HAS DISBONDED AREA 33" - 42" FROM INBOARD SIDE. REPAIRED LEFT WING OUTBOARD AFT FLAP LOWER SURFACE DISBONDED AREA 33" - 42" FROM INBOARD SIDE IAW B737-300 SRM 51-70-10, FIGURE 201, REPAIR 4.SDR 06FDEA03525Skin · unknownEXISTING REPAIR, RT WING INBD FLAP UNDERSIDE AT STA XIFM 265.49 LOWER SECTION AS MARKED (FLAP ASSY P/N NRC6055-508), SNRM N01434: REPAIRED AS PER SRM 57-10-00 FIG2 VOL1 (MAJOR REPAIR).SDR 06FDEA03524Skin · unknownEXISTING REPAIR, LT WING INBD FLAP UNDERSIDE AT STA XIFM 195.3 MIDDLE SECTION AS MARKED (FLAP ASSY P/N NRC6055-507) SNRM N01433: NEW SKIN AND SPLICE INSTALLED AS PER SRM 57-10-00 FIG3 VOL1 AND 51-31-01 VOL2 (MAJOR REPAIR).SDR SWAA063747Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT LOWER CENTER T/E END. REMOVED AND REPLACED FLAP PER MM.SDR 2006UALA01900Skin · delaminatedRIGHT INBOARD AFT FLAP HAS DELAMINATION ON BOTTOM SIDE OUTBOARD CORNER, APPROX 10 X 6 INCHES. MAJOR REPAIR: REMOVED DAMAGE AND ACCOMPLISHED A PERMANENT REPAIR PER SM-95-57-53-05-JD.SDR DHL2006770502Skin · delaminatedLEFT INBOARD FORE-FLAP, INBOARD LWR SURFACE DELAMINATED. CUT OUT DELAMINATED AREA ON LEFT INBOARD FOREFLAP, LWR SURFACE APPOX 5 INCHES BY 13 INCHES. FAB FILLER APPROX 5 INCHES BY 13 INCHES AND DOUBLER APPROX 3 INCHES BY 15 INCHES FROM 2024-T3, .016, PO 90031SDR DHL2006770501Attach Angle · crackedASTAR NR 111384: LT IB MID FLAP T/E LOWER STRUCTURE, WBL 70 TO 134 IS CRACKED FOUR PLACES IN CUT OUTS. CUT OUT DAMAGED AREA IAW SRM 51-30-2 AND 51-40-3, FIG.1. FAB NEW FROM AC 1003-100046-7075-T6, SIZE 68.75 INCH PO NR 6295115 AND ONE SPLICE WITH AC 1003-100SDR QXEA200602627Vane · crackedC3 PDX - SUSPECTED CRACK ON UPPER SURFACE OF RIGHT OUTBOARD FLAP VANE AT FS79.46. REPAIRED IAW SRM 57-53-01, AND SRM 51-42-21.SDR SWAA063686Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER END. REPAIRED FLAP PER SWA EA.SDR 06FDEA03449Shim · corrodedLT NR2 FLAP TRACK AFT MOUNT TAPERED SHIM CORRODED REMOVED CORROSION FOUND OUT OF LIMITS REMOVED .035 FROM ORG MAT .045 REMAINING MAT .010 IAW SRM 57-10-6 AND 57-10-1 FIG 1 FABERICATED NEW SHIM ON MAE TRAVLER T6/ 631803.SDR 06FDEA03448Shim · corrodedLT NR 3 FLAP TRACK BEAM CENTER MOUNT TAPERED SHIM CORRODED REMOVED CORROSION FOUND OUT OF LIMITS, CORROSION EXFOLIATION IAW SRM 51-10-6 AND SRM57-10-1 FIG 1 DETAIL 1. FABRICATED NEW SHIM ON MAE TRAVLER T6/31804.SDR ASAA0681032Skin · chafedLEFT WING OUTBOARD FLAP INBOARD VANE CHAFED ON EXISTING LEADING EDGE REPAIR DOUBLER AT INBOARD END. REMOVED EXISTING DOUBLER. INSTALLED REPAIR DOUBLER PER SRM 51-70-2.SDR SWAA063668Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD T/E AFT FLAP, DELAMINATED AT OUTBOARD LOWER SKIN. REMOVED AND REPLACED FLAP PER MM.SDR 06FDEA03440Flap Track · corrodedLT NR 3 FLAP TRACK BEAM FWD MOUNT SUPPORT FITTING CORRODED. REMOVED AND REPLACED BUSHNG IAW SR 27-57-020 AND SOPM 20-50-03. REMOVED CORROSION FROM FITTING ORIGINAL MATERIAL .750 AFTER REWORK .740. FOUND TO BE WITHIN LIMITS IAW SRM 51-106 AND SR 27-51-020 TRESDR 06FDEA03432Hinge Fitting · crackedRT WING I/B FLAP I/B HINGE FITTING FOUND CRACK. REPAIR CARRIED OUT AS PER AMM 27-50-20. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR IXXA06SMN325SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD FLAP LEADING EDGE UPPER SKIN WITH NON STANDARD REPAIR AT STATION XF211.000. REMOVED SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED TREATED AND PRIMED AREA AND NEW SKIN INTERNAL SURFACSDR IXXA06SMN326SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT WING OUTBOARD FLAP UPPER SKIN WITH NON STANDARD REPAIR AT STATION XF445.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED AND PSDR IXXA06SMN327SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD FLAP UPPER SKIN WITH NON STANDARD REPAIR AT STATION XF360.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN, AND DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED ANDSDR IXXA06SMN328SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD FLAP UPPER SKIN HAS NON STANDARD REPAIR AT STATION XW105.000. REMOVED EXISTING SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN (AL 2024 T3 0.050”), AND DOUBLER (AL 2024 T3 0.032”). BONDED SKIN AND DOSDR SWAA063645Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED INBOARD FORE FLAP PER MM.SDR SWAA063644Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED INBOARD FORE FLAP PER MM.SDR TRAX200600787Bracket · crackedRIGHT INBOARD FLAP OMEGA BRACKET CRACKED ON RIB 9 (INBOARD SIDE) FABRICATION COVER ON W/C 2000-41. RT INBD FLAP RIB 9 OMEGA BRACKET FABRICATED AS PER SRM 57-52-40 AND INSTALLED IAW SRM 51-25-01 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP663 AND FAR 43 ASDR 06FDEA03392Strap · crackedRIGHT WING, OUTBOARD FLAP INBOARD FORWARD FLAP HINGE TENSION STRAP FOUND CRACKED. RIGHT WING, OUTBOARD FLAP INBOARD FORWARD FLAP HINGE TENSION STRAP REMOVED AND REPLACED AS PER FEDEX EA NR 1-5750-104780, TITLE: WINGS, RIGHT WING, OUTBOARD TRAILING EDGE FLAPSDR 2006UALA01818Clevis · corrodedNR 6 FLAP TRACK CLEVIS LUG (OTBD) HAS BORE CORROSION. NR 6 FLAP TRACK CLEVIS LUG (OTBD) CORROSION ON THE INNER SURFACE. CARRY FORWARD ITEM NR 9123 WAS CREATED TO MONITOR CONDITION. BORE HAS FINAL DIA. 1.5030 IN. REPAIR PER KAL FRR 747-UAL-0187 AND EVA-6SDR UIEA200600266Skin · delaminatedRT INBOARD MID FLAP, BOTTOM SIDE SKIN AT WBL 195.750 HAS 1.250 BY 5.0 INCH AREA OF DELAMINATION. ACCOMPLISHED PREPREG LAYUP 250 DEGREES CURE PERMANENT REPAIR AS PER 747 SRM 51-40-09 FIG 2 AND 51-40-12.SDR QXEA200602576Vane · chafedC3 PDX - LEFT OUTBOARD FLAP VANE LOWER SURFACE LEADING EDGE HAS CHAFE AT WS 282 OUTBOARD END. REPAIRED IAW SRM 57-53-01 AND SRM 51-25-06.SDR 06FDEA03379Hinge Fitting · crackedRT WING O/B FLAP I/B HINGE SUPPORT FITTING SUSPECT CRACKED. RT WING O/B FLAP REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-830-805 AND AMM 27-50-00-830-806, FOUND SATIS. REPAIR CLASSIFIED AS MINOR AS PER GSDR 06FDEA03375Hinge Bracket · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE) PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04 PG.621-622. BUSHING FABRICATED AND INSTALLED AS PER EA1-5750-104709 TEE REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-1SDR 06FDEA03352Hinge · corrodedRT WING I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG 442-444. ORIGINAL THK 1.1875" FINAL 1.257" MAX ALLOWABLE 1.220". BUSHING FABRICATED AND INSTALLED AS PESDR 06FDEA03350Hinge · corrodedLEFT WING I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG.442-444. ORIGINAL THK 1.187" FINAL 1.257" MAX ALLOWABLE 1.220". BUSHING FABRICATED AND INSTALLED AS PERSDR SWAA063511Bolt · loosePUT FLAPS DOWN AT 210 AND GOT UNUSUAL RUMBLE. AS AIRCRAFT SLOWED TO 180 RUMBLE STOPPED. RUMBLE CAME BACK IN 30 DEGREE BANK AND THEN QUIT. SECURED NR 6 T/E FLAP DRIVE UNIT BOLT PER MM.SDR MALA060556Skin · damagedDURING 2 YEAR CHECK IN BNA FOUND DAMAGE TO LT FLAP UPPER SURFACE TRAILING EDGE AT WS145.17. APPLIED COMPOSITE REPAIR IAW EO NR S51031.SDR UIEA200600263Skin · delaminatedDURING VISUAL INSPECTION ON LHW I/B AFT FLAP LWR SURFACE T/E FOUND DELAMINATED AT 15" - 25" FROM I/B SIDE CAUSED BY TIRE BLOWN. COMPOSITE REPAIR CARRIED OUT AS PER SRM 51-40-12 FIG 9.SDR UIEA200600262Fairing · delaminatedDURING VISUAL INSPECTION ON LHW I/B AFT FLAP LWR SURFACE L/E FAIRING FOUND DELAMINATED AT 10" - 20" FROM I/B SIDE CAUSED BY TIRE BLOWN. COMPOSITE REPAIR CARRIED OUT AS PER SRM 51-40-12 FIG 9.SDR UIEA200600260Skin · dentedDURING VISUAL INSPECTION FOUND, LHW I/B AFT FLAP LWR SURFACE PANEL WITH DENT MARKS CAUSED BY TIRE BLOWN AT NR 4 CANOE FAIRING AREA. FILLER REPAIR CARRIED OUT AS PER SRM 51-40-01.SDR SWAA063486Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.SDR 06FDEA03272Bracket · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) FORWARD MOUNT OUTBOARD AFT BORE FOUND CORRODED. RIGHT WING, OUTBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) FORWARD MOUNT OUTBOARD AFT BORE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-103514, TITLE: WING
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