JASC 5753
Service difficulty reports · 31,521
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 SWAA042918Skin · delaminatedDURING SCHEDULED RON, FOUND RT WING OUTBD FORE FLAP DELAMINATED AT UPPER SURFACE. REMOVED AND REPLACED FLAP ASSY PER MM.SDR 04FDEA02890Hinge · corrodedCOMPLY WITH EA 8-5750-82050 RT INBOARD FLAP MOUNTED HINGE PIVOT BORE REPAIR. COMPLIED WITH EA8-5750-82050.SDR IXXA060027SSkin · crackedDURING ROUTINE C-CHECK FOUND LT WING IB FLAP LEADING EDGE UPPER SKIN CRACKED AT STATION XW84. REMOVED FLAP VANE, AND NOSE PANEL TO FACILITATE REPAIR. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED DOUBLSDR IXXA060026SSkin · dentedDURING ROUTINE C-CHECK FOUND LT WING IB TRAILING EDGE FLAP UPPER SURFACE DENTED OUT OF LIMITS AT STATION XW35. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED FILLER AND DOUBLER WET WITH SEALANT FROM STSDR IXXA060025SSkin · dentedDURING ROUTINE C-CHECK FOUND LT WING IB TRAILING EDGE FLAP LOWER SURFACE DENTED OUT OF LIMITS AT STATION XW39 AFT AREA. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED FILLER AND DOUBLER WET WITH SEALANTSDR IXXA060024SSkin · dentedDURING ROUTINE C CHECK, FOUND LEFT WING INBOARD TRAILING EDGE FLAP LOWER SURFACE DENTED OUT OF LIMITS AT STATION XW39. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, REMOVED, TREATED, PRIMED, AND INSTALLED FILLER AND DOUBLER WET WITH SEALASDR IXXA060019SSkin · dentedDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP LOWER SKIN DENTED AT STATION XF208. REMOVED FASTENERS AS NEEDED TO REMOVE RIGHT WING OUTBOARD FLAP LOWER SKIN FROM STATION XF169 TO STATION XF213. FABRICATED, NEW SKIN AND FINGER DOUBLERS, LOCATED, DRILLSDR ASOA04822Bracket · crackedDURING A C-CHECK, THE OMEGA BRACKET ON THE LT WING IB FLAP FITTING AT RIB 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OMEGA BRACKET ON THE LT WING IB FLAP FITTING AT RIB 9 IAW SRM 51-25-04.SDR SWAA042894Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD FLAP PER MM.SDR SWAA042887Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD T/E FLAP PER MM.SDR 04FDEA02879Hinge · corrodedLT WING OB FLAP IB HINGE, LOCATION NR 6, OB BORE IS CORRODED. REMOVED CORROSION, BEGINNING BORE DIAMETER 1.240, FINAL 1.266, MATERIAL LOSS 0.026 IAW DAC CMM 57-44-08, ETCH INSPECTED IAW DAC CMM 57-44-08 AND 20-11-02. PEENED IAW DAC CMM 57-44-08 AND 20-11-01.SDR 04FDEA02874Support · corrodedLT/RT OB FLAPS-FLAP VANE SUPPORTS CORROSION REWORK. CLOSING ACTION ON 10/04/04. ON N/R S00018. COMPLIED WITH EA 8-5750-82049.SDR IXXA060094SSkin · dentedDURING ROUTINE C CHECK, FOUND RIGHT WING INBOARD FLAP TRAILING EDGE HAS SEVERAL DENTS BETWEEN STATIONS XW64 AND XW101. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS. IAW DC8SDR IXXA060093SSkin · dentedDURING ROUTINE C-CHECK FOUND RT WING OB FLAP UPPER LEADING EDGE SKIN DENTED AT STATION XF 418. REMOVED DAMAGED. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING OB FLAP UPPER LEADING EDGE ATSDR IXXA060092SSkin · dentedDURING ROUTINE C-CHECK, FOUND RIGHT WING INBOARD FLAP LOWER SURFACE HAS SEVERAL DENTS BETWEEN STATION XW15 AND XW45. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS. PERFORMED HOT BOND TO DAMAGED AREA IAW DC8 SRM 57-1-0, 51-1-9, 51-1-5 AND 51-1-8.SDR IXXA060018SSkin · dentedDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP LOWER SKIN DENTED BETWEEN STATION XF309 AND XF333. REMOVED FASTENERS AS NEEDED. REMOVED LOWER SKIN SECTION. FABRICATED NEW SKIN SECTION AND FILLERS. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTSDR IXXA060017SSkin · dentedDURING ROUTINE C CHECK, FOUND RIGHT WING OUT BOARD FLAP DENTED AT STATION XW384. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED TRIMMED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS AND NEW FASTENESR WET WITH SEALANT FSDR 2005FA0000262Rib · crackedLT WING IB FLAP TRACK RIB ASSY, PN 1221010-15, HAS 2 BRACKETS RIVETED TO EITHER SIDE OF IT TO ATTACH FLAP TRACK RIB ASSY TO WING LOWER IB T/E SKIN, REF TO AS FLAP WELL SKIN) PN 0720601-101. ONE OF BRACKETS HAD CRACKED ALLOWING BRACKET TO TWIST SLIGHTLY, DECRESDR SWAA042870Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND LT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.SDR SWAA042869Skin · delaminatedDURING SCHEDULED SERVICED CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT OUTBOARD AFT T/E FLAP PER MM.SDR AWXA200401170Skin · crackedDURING C-18 CHECK 11 EACH CRACKS WERE FOUND IN NR 3 SLAT LOWER SKIN BETWEEN SLAT STA. 51.75 AND 74.65 LT. MAINTENANCE CUTOUT DAMAGED SECTION OF NR 3 SLAT LOWER SKIN FROM S.S. 51.75 LT TO S.S. 74.65 LT; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PSDR AWXA200401109Skin · delaminatedDURING C-18 CHECK, FOUND THE RT OUTBOARD FLAP DELAMINATED ON THE LOWER INBOARD END BETWEEN WBL 230.68 AND WBL 234.68. MAINTENANCE REMOVED DELAMINATION ON RT OUTBOARD FLAP LOWER INBOARD END; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO FLAP IAW B737SDR USAA040831Skin · delaminatedTOP SKIN, CORE BOND, 2 INCH SQUARE AREA, DELAMINATION. LT OB FOREFLAP TOP SKIN SURFACE ON IB T/E. INSTALLED NEW CORE AND TOP DOUBLER, SEAL AND REFINISH IAW SRM.SDR 0401899607Skin · crackedDURING M-CHECK FOUND CRACK IN NR 3 INBOARD FLAP SKIN AT XLFS=255. REPAIRED PER EA 99-200363.SDR 04FDEA02863Structure · crackedLEFT WING, OUTBOARD FLAP, INBOARD AFT HINGE LOCATION MID ATTACHMENT FITTING SUSPECTED CRACKED. LEFT WING, OUTBOARD FLAP ASSEMBLY P/N NRC6753-503. REMOVED AND REPLACED PER AMM 27-50-30.SDR 04FDEA02862Fitting · corrodedCOMPLY WITH 8-5750-82047- RIGHT O/B HINGE LUG CORROSION REPAIR. COMPLIED WITH EA 8-5750-82047 RIGHT O/B FLAP O/B HINGE LUG CORROSION REPAIR (P/N ARC 1991-2). AT MAE ENT BY: 497234 RPT BY: 497234SDR 0401809607Skin · crackedDURING M-CHECK FOUND CRACKED IN RT WING TRAILING EDGE FLAP UPPER STRINGER AT WING STATION 235. REPAIRED IAW EA 96-200350.SDR 2004UALA00911Hinge · crackedRIGHT WING INBOARD FLAP CENTER EXTERNAL HINGE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLAP HINGE WITH REPAIR ANGLES AND FILLER.SDR SWAA042848Skin · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING T/E FLAP PER MM.SDR SWAA042845Wedge · separatedDURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD T/E MID FLAP WEDGE SEPARATED. REPAIRED WEDGE PER SRM.SDR CALA0400650Bracket · crackedINSPECTION FOUND RIGHT WING NR 6 FLAP TRACK FAIRING HORSE COLLAR BRACKET BENT AND CRACKED. THE CRACK WAS 1 INCH LONG. THE HORSE COLLAR BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR MALA040679Spar · crackedDURING 4K INSPECTION IN LAN, LT FLAP AFT SPAR CRACKED FOR WS 140.3 TO 142.3. MAINTENANCE REPAIRED IAW SAAB SRM 57-80-10. AIRCRAFT RETURNED TO SERVICE 9/29/04.SDR DHL2004801555Plate · wornRT OTBD FLAP L/E UPPER PLATING WORN AT XF 226.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W51-R05 FAA FORM 8110-3 DATED 09-28-04. REMOVED DAMAGED SKIN SEGMENT IAW SRM 51-1-21, SRM 51-3-0. FABRICATED NEW SKIN SEGMENT (2024-T3AL 0.071) INTERNAL SPLICE SDR ASAA0480523Vane · damagedOKC - C-CHECK, RT IB FLAP VANE LOWER SKIN HAS DINGS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-2.SDR ASAA0480522Vane · dentedOKC - C-CHECK, RT OB FLAP VANE IB END LOWER SKIN HAS NUMEROUS SMALL DENTS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-2.SDR ASAA0480520Skin · dentedOKC, C-CHECK, RT WING T/E IB FLAP DENTED AT LOWER SURFACE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-03, FIG 7.SDR 2004UALA00914Hinge · crackedLEFT WING INBOARD FLAP CENTER EXTERNAL HINGE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED HINGE WITH REPAIR ANGLES.SDR DHL2004801553Skin · wornITEM REF. NR. 1130: LT OB FLAP L/E UPPER PART PLATING WORN, XF 345.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG R51-R08, FAA FORM 8110-3 DATED 09-24-2004. REMOVED FASTENERS IAW SRM 51-1-21. TRIMMED OUT DAMAGED SKIN SEGMENT IAW DWG W51-R08. FABRICATED NESDR DHL2004801554Plate · wornRT OTBD FLAP L/E UPPER PLATING WORN, XF 213.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W51-R03, FAA FORM 8110-3 DATED 09-24-2004. REMOVED DAMAGED SKIN SEGMENT IAW SRM 51-1-21, DWG W51-R03. FABRICATED NEW SKIN SEGMENT (2024-T3AL 0.040), INTERNAL SPLISDR 04FDEA02822Hinge · corrodedLEFT HAND INBOARD FLAP OUTBOARD SUPPORT PIVOT ATTACH POINT OUTBOARD BORE CORRODED. CORROSION EXCEEDS CMM 57-52-01 LIMITS. REPAIRED IAW FEDEX EA 8-5750-77622. REFERENCE NON ROUTINE N00490.SDR DHL2004801552Doubler · damagedITEM REF. NR. 1131: LT IB FLAP L/E UPPER PLATING HAS INTERIM REPAIR, XW 85.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W51-R07, FAA FORM 8110-3 DATED 09-24-2004. REMOVED INTERIM REPAIR IAW SRM 51-1-21. TRIMMED OUT DAMAGED AREA IAW DWG W51-R07. FABRICASDR ABXA040344Vane · delaminatedRIGHT FLAP INBOARD FIXED VANE UPPER SURFACE AT XRS 164, LOCATED BETWEEN CHAFE STRIPS WAS DELAMINATED BEYOND LIMITS OF 15 SQ INCHES. REMOVED AND REPLACED INBOARD FIXED VANE IAW DC-9 SRM.SDR ASAA0480513Vane · puncturedOKC - C-CHECK, RT IB FLAP OB FLAPVANE HAS A PUNCTURE ON THE IB END. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-2, PARA 18.SDR SWAA042787Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT AFT T/E FLAP PER MM.SDR 04FDEA02809Hinge · corrodedLT WING, IB FLAP, OB AFT HINGE PIVOT HOLE IB SPOTFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS PER CMM 57-52-03.SDR 04FDEA02808Hinge · corrodedLT WING, IB FLAP, OB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMTS PER CMM 57-52-03, PAGES 442 TO 443. ORIGINAL DIAMETER= 1.289, FINAL DIAMETER= 1.291. COMPLIED WITH FEDEX EA 1-5750-79749SDR 04FDEA02807Hinge · corrodedRT WING, IB FLAP, OB AFT HINGE PIVOT HOLE OB SPOTFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS PER CMM 57-52-03.SDR 04FDEA02806Hinge · corrodedRT WING, IB FLAP, OB AFT HINGE OB PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMTS PER CMM 57-52-03, PAGES 442 TO 443. ORIGINAL DIAMETER = 1.249, FINAL DIAMETER = 1.257. COMPLIED WITH FEDEX EA 1-5750-79749,SDR 04FDEA02805Hinge · corrodedRT WING, IB FLAP, OB AFT HINGE PIVOT HOLE IB SPOTFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS PER CMM 57-52-03 PAGES 442 TO 443.SDR 04FDEA02804Hinge · corrodedRT WING, IB FLAP, OB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMTS PER CMM 57-52-03, PAGES 442 TO 443. ORIGINAL DIAMETER= 1.251, FINAL DIAMETER= 1.314. COMPLIED WITH FEDEX EA 1-5750-79749,
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