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 08FDEA01268Flap Track · wornLT FLAP VANE NR5 TRACK HAS WORN AREAS MARKED. REPAIRED NR 5 L/W FLAP VANE TRACK IAW AIRBUS CMM 57-52-15.SDR 08FDEA01265Flap Track · wornRIGHT WING INBD FLAP VANE MID TRACK INBD SIDE HAS WORN AREA. REPAIRED NR 3 R/W FLAP VANE TRACK IAW AIRBUS CMM 57-52-15.SDR 08FDEA01264Flap Track · wornLT FLAP VANE NR 2 TRACK HAS WORN AREAS MARKED REPAIRED NR 2 FLAP VANE TRACK IAW AIRBUS CMM 57-52-15.SDR 08FDEA01263Flap Track · wornRIGHT FLAP VANE TRACK NR 4 IS WORN REPAIRED R/W NR 4 FLAP VANE TRACK IAW AIRBUS CMM 57-52-15.SDR 08FDEA01262Flap Track · wornLEFT FLAP VANE NR 3 TRACK HAS WORN AREAS (MARKED). REPAIRED LEFT FLAP VANE NR 3 TRACK IAW AIRBUS CMM 57-52-15.SDR 08FDEA01261Flap Track · wornRIGHT FLAP VANE TRACK IS WORN, NR 5 TRACK. REPAIRED RIGHT WING NR 5 FLAP VANE TRACK IAW AIRBUS CMM 57-52-15.SDR 08FDEA01260Flap Track · wornRIGHT FLAP VANE TRACK NR 2 IS WORN. REPAIRED RIGHT WING NR 2 FLAP VANE TRACK IAW AIRBUS CMM 57-25-15.SDR 08FDEA01258Flap Track · wornRIGHT FLAP VANE TRACK NR 1 IS WORN. RECEIVED NEW TRACK FOR INSTALLATION; SEE FEDEX JOB CARD 46S5181CP. OLD TRACK IS OUT OF LIMITS. MAX LIMIT 0.0315; MEASURED 0.065.SDR 2008UALA01494Skin · puncturedFOUND PUNCTURE IN RT INBOARD TRAILING EDGE FORE FLAP UPPER SURFACE. PREVIOUS REPAIR DISBONDED AND TORN. HOLE IS .5 IN X .25 IN, LOCATION IS 4.5 FEET O/B 7.5 IN FROM TRAILING EDGE. FOUND PUNCTURE IN RT INBOARD TRAILING EDGE FORE FLAP UPPER SURFACE. REMOVED RSDR MALA080039Skin · debondedLT FLAP TRAILING EDGE UPPER SKIN HAS 6 DISBONDED DENTS. REPAIRED IAW EO S57179.SDR SWAA081459Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.SDR 08FDEA00976Skin · dentedDURING INSPECTION ON LT WING INBD FLAP UPPER SKIN FOUND 2 EA DENTS: 1) UPPER 1 INCH BY 1 INCH DEEP .074 INCH 2) LWR 2 INCH BY 1.50 INCH DEEP .050 INCH. REPAIRED SKIN IAW SRM 57-10-00 VOL I FIG 65.SDR USAA920080652Flap · delaminatedCLT - MAJOR REPAIR - C6 CHECK - RIGHT WING OUTBOARD TRAILING EDGE FLAP HAS AREA OF DELAMINATION. REPLACED RIGHT WING OUTBOARD TRAILING EDGE FLAP IAW B737 SRM 27-51-39.SDR DHL2008763509Skin · chafedRT I/B FORE FLAP I/B L/E CHAFED AT RWBL 73. DAMAGE BEYOND SERVICE LIMITS. REMOVED, FABRICATED, AND INSTALLED SKIN PANEL, 2024-T3 .050 INCH BY 14 INCH BY 14.5 INCH, PONR 9006586, PER B727 SRM 57-50-2 FIG 3, 51-20-1, AND 51-30-2.SDR 2008UALA01440Panel · wornRIGHT O/B FLAP, UPPER SKIN PANEL IS WORN AT OUTBOARD END. REPAIR PER EN-57- 0028-01 AND EVA-71269. THE REPAIR IS APPROVED BY MANUFACTURER. THE REPAIR IS 12 MONTH LIMITED REPAIR AND A NEW 8100-9 MUST BE ISSUED TO COMPLY WITH 14 CFR 25.5 71 AND 26.43(D). OK TO SDR 2008UALA01439Skin · wornLEFT O/B FLAP I/B END, 12 FROM FRONT END, SKIN IS WORN. REPAIR PER EN-27- 51-21-028--21 AND EVA-71266. THE REPAIR IS APPROVED BY BAC, 8 100-9. THE REPAIR IS 12 MONTH LIMITED REPAIR, AND A NEW 8100-9 MUST BE ISSUED TO COMPLY WITH 1 4 CFR 25.571 AND 26.43 (D)SDR IXXA08SMN101SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD FLAP LOWER PANEL SKIN HAS IMPROPER REPAIR AT STATION XW 18.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PARTS AS NEEDSDR IXXA08SMN103SSkin · deformedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER PANEL DEFORMED AT STATION XW 104.000 TO STATION XW 115.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PARTS AS NEEDEDSDR IXXA08SMN100SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD FLAP SKIN UPPER PART DENTED AT STATION XW 114.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTSDR IXXA08SMN099SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD FLAP SKIN UPPER PART HAS IMPROPER REPAIR AT STATION XW 114.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, BONDED DOUBLER. BONDED PARTS AS NEEDED SDR 08FDEA00963Panel · delaminatedRIGHT WING OUTBD FLAP INBD FAIRING PANEL NR 636 DR IS DELAMINATED. REPAIRED IAW DWG ARC 2232, TPS 1001 REV E & EA 8-5750-116970. RESTORED FINISH SRM 51-21-02; VOL II.SDR 08FDEA00962Panel · delaminatedRIGHT WING OUTBD FLAP; INBD PANEL NR 635 DL IS DELAMINATED. FABRICATED & BONDED PANEL IAW EA 8-5720-118478.SDR 08FDEA00961Panel · debondedLEFT WING INBD FLAP FAIRING NR 535HL HAS AREAS OF DISBOND. REPAIRED BY FABRICATING & BONDING THE INNER & OUTER SKINS; INNER & OUTER DOUBLERS & CORE IAW TPS 1001, REV E & EA 8-5720-118479,SDR 08FDEA00958Skin · gougedRIGHT WING OUTBD FLAP INBD HINGE FAIRING PANEL NR 635 BR INNER SKIN IS GOUGED. REPAIRED IAW SRM 51-71-00, VOL II, PARA 17. ALODINDE, PRIMED & PAINTED IAW SRM 51-71-00, VOL II.SDR UPS08851879Skin · puncturedINSPECTION TYPE:N/A RIGHT WING O/B FLAP UPPER SKIN HAS PUNCTURE DAMAGE 2 INCHES I/B OF CUTOUT (ACTUATOR) AND 18 INCHES AFT OF LEADING EDGE. DAMAGE MEASURES .375" X .250". ACCOMPLISHED REPAIR PER DC8 SRM 57-02-01-0 FIG 002Q. CLASS B REPAIR. RAN FLAPS, NO INTSDR 2008UALA01400Skin · wornLEFT O/B FLAP, NEAR MID POINT, 30" FROM AFT END, SKIN IS WORN. REPAIR PER EN57-0 028-03 AND EVA-71266. THE REPAIR IS APPROVED BY BAC, 8100-9. THE REPAIR IS 12 MONTH LIMITED REPAIR, NEW 8100-9 MUST BE ISSUED TO COMPLY WITH 14 CFR25.571 AND 26.43(D). OK TO CF PSDR 08FDEA00947Fairing · dentedFWD FLAP FAIRING 634 AB/BB LOWER AFT END IS DENTED. REPAIRED DENT BY REMOVING THE DAMAGE AND APPLYING A WET LAY UP.SDR 08FDEA00946Fairing · erodedFWD FLAP FAIRING 634 AB/BB; FWD END IS ERODED. REPAIRED ERROSION BY REMOVING THE DAMAGE AND APPLIED A WET LAY UP IAW A310 SRM 57-20-35.SDR 08FDEA00942Fairing · erodedNR 5 RT WING FLAP FAIRING HAS NUMEROUS SPOTS OF EROSION AND CHIPPED PAINT. PAINTED IAW AMM 51-75-10-8.SDR 08FDEA00927Flap Track · crackedCRACKS FOUND IN HOLE 15 FLAP TRACK BEAM 2 LT. REPAIR PERFORMED BY INSTALLING SB 57-6006 (OVERSIZING AND COLD WORKING OF HOLES), APPROVED BY EO 6-5750-7-3000 PT 1.SDR ASAA0842712Skin · dentedLT OUTBOARD AFT FLAP LWR SURFACE AT WBL 255 IS DENTED. DENT REPAIRED IAW B737 400 SRM CH 51 70 10.SDR DHL2008763508Rib · crackedPREVIOUS REPAIR ON L/WING O/B FORE FLAP UPPER SURFACE CHAFED, LWBL 400. REMOVED EXISTING REPAIR AND ASSOCIATED INTERNAL RIB. FABRICATED AND INSTALLED NEW REPAIR SKIN SECTION, 2024-T3 .050 INCH BY 14.125 INCH BY 5.875 INCH, PO NR 9005554; AND SPLICE, 2024-T3 SDR ASAA0842880Wedge · dentedLEFT I/B MID FLAP T/E WEDGE DENTED SEVERAL AREAS. REMOVED DAMAGED SECTIONS OF WEDGE, FABBED AND INSTALLED REPAIR DOUBLERS IAW B737 400 SRM 51 70 10 REPAIR 2.SDR ASAA0842878Skin · dentedLEFT WING I/B FORE FLAP LOWER SIDE HAS MULTIPLE DENTS. PREPPED DENTED AREAS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW B737 400 SRM 51 70 10 REPAIR 2.SDR DHL2008754001Wedge · delaminatedUPON INSPECTING THE EXTERIOR OF THE AIRCRAFT, FOUND THE RIGHT INBOARD TRAILING EDGE MID FLAP WEDGE DELAMINATED AT THE INBOARD END. ABOUT 20 INCHES FROM THE INBOARD END HAS A DELAMINATION APPROX 6 INCHES LONG SPANWISE AND THE WIDTH OF THE WEDGE. PART REPAIREDSDR ASAA0842753Skin · dentedDENTS FOUND ON INBD RT FOREFLAP UPPER SURFACE. DENTS ON UPPER SURFACE OF RT INBOARD FOREFLAP 8" FROM T/E APPROX 48" AND 77" FROM 18 END REPAIRED IAW B737 400 SRM 51 70 10 REPAIR 3.SDR 2008UALA01374Support Fitting · wornNR 2 FLAP SUPPORT FITTING 2V JOINT OUTBOARD END BUSHING BORE IS WORN.SDR 2008UALA01373Support Fitting · wornNR 8 FLAP SUPPORT FITTING JOINT 8V, BOTH INBOARD AND OUTBOARD END BUSHING BORE HOLE IS WORN.
SDR 2008UALA01372Support Fitting · wornNR 1 FLAP SUPPORT FITTING, JOINT 1V INBOARD BUSHING BORE IS WORN.
SDR 08FDEA00908Skin · gougedLEFT WING, INBOARD FLAP LOWER SURFACE FOUND GOUGE AT XIFH 191. REPAIRED AS PER SRM 57-10-00 FIG.2 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR SWAA081359Flap · delaminatedDURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.SDR USAA920080684Skin · delaminatedMCM - MAJOR REPAIR-C18- RIGHT T/E INBOARD FORE FLAP IS DELAMINATED UPPER SURFACE, WBL 117.00. CUT OUT DAMAGED SKIN AND CORE, INSTALLED NEW CORE AND DOUBLER IAW SRM 51-70-10-2R4 FIG 203.SDR USAA920080683Skin · delaminatedMCM - MAJOR REPAIR-C18-NR 6067164, RIGHT T/E OUTBOARD FORE FLAP IS DELAMINATED UPPER SURFACE, WBL 292.69 - 295.69. INSTALLED REPAIR DOUBLER IAW SRM 51-70-10-2R3 & 2R4, FIG 201.SDR SWAA081351Flap · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR SWAA081352Guide · looseDURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD FORE FLAP GUIDE LOOSE. REMOVED AND REPLACED FLAP PER MM.SDR 08FDEA00851Rub Strip · damagedLT OUTBD FLAP UPPER SURFACE CENTER CHAFE STRIP IS WRINKLED AND BULGING. REMOVED & REPLACED THE CHAFE STRIP IAW SRM 57-53-12; FIG 201.SDR 08FDEA00850Rub Strip · debondedLT OUTBD FLAP UPPER EXTERNAL SKIN HAS THE METAL CHAFE STRIP DISBONDED. REMOVED & REPLACED CHAFE STRIP IAW SRM 57-53-12 FIG 201.SDR 08FDEA00849Skin · delaminatedLT OUTBD FLAP AFT EDGE OF THE FLAP IS DELAMINATED ON THE UPPER SURFACE. PREPARED & RESEALED IAW SRM 57-53-12 FIG 209.SDR 2008UALA01299Support Fitting · wornNR 7 FLAP UNDER WING SUPPORT FITTING IS WORN ON OUTBD SIDE, IB END, NR 7V JOINT.SDR 2008UALA01298Bushing · wornNR 7 FLAP SUPPORT UNDERWING LINK, IB JOINT 7V BUSHING. WORN IS BEYOND LIMIT.
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