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 05FDEA04233Mount · corrodedRIGHT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG BORE CORRODED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 15750-94562.SDR 05FDEA04232Mount · corrodedFOUND LEFT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR OUTBOARD LUG BORE CORRODED.SDR 05FDEA04231Mount · corrodedFOUND LEFT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR INBOARD LUG BORE CORRODED. REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94563.SDR 05FDEA04230Mount · corrodedFOUND LEFT WING: WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD FORWARD HINGE LOWER INBOARD MOUNT BORE CORRODED. REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94563.SDR 05FDEA04229Mount · corrodedFOUND LEFT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP INBOARD FORWARD HINGE ACTUATOR OUTBOARD LUG BORE CORROSION. REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94564.SDR 05FDEA04228Mount · corrodedFOUND LEFT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP INBOARD FORWARD HINGE ACTUATOR INBOARD LUG BORE CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94564.SDR 05FDEA04227Mount · corrodedLEFT WING WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP INBOARD FORWARD HINGE LOWER MOUNT SURFACE CORRODED. CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-94564.SDR 05FDEA04226Mount · corrodedLEFT HAND WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP INBOARD FORWARD HINGE LOWER INBOARD MOUNT BORE CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94564.SDR 05FDEA04225Hinge · corrodedLEFT HAND WING INBOARD TRAILING EDGE FLAP OUTBOARD HINGE (FLAP SIDE) AT PIVOT BORE HOLE OUTBOARD SIDE FOUND CORROSION. CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-94560.SDR 05FDEA04224Structure · tool damageLEFT HAND WING INBOARD TRAILING EDGE FLAP OUTBOARD HINGE (FLAP SIDE) AT PIVOT BORE HOLE INBOARD SIDE FOUND TOOL MARK. TOOL MARK REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-94560.SDR 05FDEA04223Structure · corrodedRIGHT HAND WING INBOARD TRAILING EDGE FLAP OUTBOARD HINGE (FLAP SIDE) AT PIVOT BORE HOLE OUTBOARD SIDE FOUND CORROSION. CORROSION REMOVED AS PER FEDEX EA 1-5750-94561.SDR 05FDEA04222Structure · corrodedRIGHT HAND WING INBOARD TRAILING EDGE FLAP OUTBOARD HINGE (FLAP SIDE) AT PIVOT BORE HOLE INBOARD SIDE FOUND CORROSION. CORROSION REMOVED AS PER FEDEX EA 1-5750-94561.SDR AU510001868Bearing · wornRT WING FLAP TRACK BEAM ASSEMBLY FORWARD SUPPORT BEARING WORN.SDR AU510001867Bearing · wornLT WING TRAILING EDGE FLAP TRACK FORWARD SUPPORT BEARING WORN.SDR 05FDEA04201Flap Track · corrodedLEFT WING I/B FLAP O/B TRACK FWD MOUNT HOLE-D HAS PITTING IN INNER BORE. REMOVED PITTING AND CORROSION IAW BAC OHM 57-40-01. FABRICATED AND INSTALLED IAW BAC OHM 57-40-01 AND FED EX EA 7-5710-91314, LT INBOARD FLAP OUTBOARD TRACK OVERSIZE HOLE-D. MINOR REPASDR 05FDEA04194Hinge Bracket · corrodedLEFT HAND WING OUTBOARD FLAP INBOARD AFT HINGE BRACKET FORWARD FITTING ATTACH HOLE AT OUTBOARD AFT POSITION FOUND CORRODED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90702.SDR 05FDEA04193Hinge Bracket · corrodedRIGHT HAND WING OUTBOARD FLAP INBOARD AFT HINGE BRACKET AFT FITTING FORWARD ATTACH HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90699.SDR 05FDEA04192Hinge Bracket · corrodedRT WING OUTBOARD FLAP INBOARD AFT HINGE BRACKET FORWARD FITTING ATTACH HOLE AT OUTBOARD AFT POSITION FOUND CORRODED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90700.SDR 05FDEA04191Hinge Bracket · corrodedRIGHT HAND WING OUTBOARD FLAP INBOARD AFT HINGE BRACKET FORWARD FITTING ATTACH HOLE AT INBOARD AFT POSITION FOUND CORRODED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90701.SDR SWAA053894Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND LT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA053892Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING OTBD T/E AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR QXEA200600259Guide · wornYYC - LT WING, O/B FLAP AFT GUIDE ROLLER FITTING IS WORN (RECEIVING END). BLENDED OUT DAMAGE ON ROLLER FITTING IAW CRJ700 SRM 57-51-02-201-001-A01. HEFC INSPECTION C/00N BLEND REPAIR AREA OF FITTING AS REQUIRED IAW NDTM PT 151-20-006. NO CRACKS FOUND. ROTASDR QXEA200600240Vane · damagedYYC - RT WING OUTBD FLAP - FLAP VANE, INBD UPPER L/E HAS BROKEN FASTENERS. REPLACE 6 EA RIVETS (CR3214-4-3) B/N 62151 IAW CRJ 700 SRM 51-42-13-001-001-A01.SDR QXEA200600262Vane · damagedYYC - RT OUTBD FLAP VANE L/E (LOWER SURFACE) HAS LOOSE FASTENER AT WS 218. REPLACED FASTENER IAW CRJ 700 SRM 51-42-13-001-001-A01.SDR DHL2005803548Plate · elongatedLT WING OTBD FLAP LWR PLATING RIVETS HOLES ELONGATED BETWEEN XF 210.000 AND XF 247.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 12-06-2005, DWG AA33-53-R10 REV IR DATE 11-22-05. REMOVED DAMAGED EXISTING SOLID PLATING, FABRICATED NEW PLATING (2024T3 0SDR ABXA050374Skin · corrodedSPOT OF CORROSION ON LOWER SIDE OF FLAP LEADING EDGE, AT OUTBOARD END OF INBOARD FIXED VANE. REPAIRED AREA IAW DC9 SRM 57-01.SDR ABXA050372Skin · corrodedUPPER AND LOWER SURFACES HAD CORROSION ON OUTBOARD REMOVEABLE TRAILING EDGE. REMOVED CORROSION, REMOVED AND REPLACED LOWER SKIN IAW DC9 SRM.SDR ABXA050371Vane · corrodedINBOARD FIXED VANE HAD 2 AREAS OF BULGING WITH POPPED RIVET HEADS. LOWER INBOARD AND UPPER OUTBOARD ALSO HAD WATER IN MOUNT ACCESS HOLE. REMOVED RIVETS, CHECKED CORROSION. REMOVED AND REPLACED FIXED VANE IAW DC9 SRM.SDR DHL2005765501Skin · gougedLEFT OUTBD FORE FLAP L/E SKIN GOUGED 26" INBD OF OUTBD FLAP TRACK. CUT OUT GOUGED AREA, FABRICATED AND INSTALLED REPAIR IAW B727 SRM 57-50-4 FIG 1, MATERIAL 2024-T3 .050" PO NR 801639.2.SDR SWAA053902Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA053883Flap Track · corrodedDURING SCHEDULED 1/4D CHECK, FOUND LT WING T/E FLAP NR 2 TRACK CORRODED AT AFT LOWER OTBD ATTACH FITTING. REMOVED AND REPLACED FLAP TRACK PER MM.SDR AWXA200600090Skin · delaminatedMCN - DURING C16 CHECK DISCOVERED LT OUTBOARD AFT FLAP DELAMINATED AT THE INBOARD TRAILING EDGE FROM WS 230.68L TO WS 234.68L. MAINTENANCE REMOVED DISBONDED SKIN AND CORE IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPLACEMENT CORE AND DOUBLER IAW BOEINGSDR DHL2005803532Fitting · brokenLT IB FLAP OB FITTING BROKEN STA 97.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0. REMOVED BROKEN FITTING IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-1SDR 05FDEA04145Flap Track · corrodedN01126 LT WING IB FLAP OB FLAP TRACK CORRODED ON AFT ATTACH POINT. ** SD ** COMING REPLACED FLAP TRACK IAW W/C 27X5705-03SDR 05FDEA04141Skin · gougedLEFT OUTBOARD MID FLAP OUTBOARD LEADING EDGE HAS 2 EACH GOUGES. REPAIRED FLAP LEADING EDGE IAW FEDEX EA7-5750-92591. WINGS - LEFT WING OUTBOARD MID FLAP LEADING EDGE SKIN HAS GOUGES. THIS IS A MINOR REPAIR BY TIMCO MECH 7153 AND QC303.SDR 05FDEA04129Repair · properDISCREPANCY LT WING INBOARD FLAP FOUND A FLUSH DOUBLER 7.75" BY 4.75" ON LOWER SKIN AT STA XIFH 133. PERFORMED A GVI OF REPAIR IAW EA NR 8-5710-90133 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 AND TREATED STRIPPED AREA IAW SRM 51-21-SDR 05FDEA04125Support Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CORROSION AT OUTBOARD NR 3 BOLT HOLE. RT WING OUTBD FLAP REMOVED & REPLACED AS PER AMM 27-50-30-4. VANE ADJUSTMENT CARRIED OUT AS PER AMM 27-50-32-5 FOUND SATIS. OUTBD FLAP OPERATIONAL TEST & SDR 05FDEA04124Support Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CORROSION AT OUTBOARD NR 2 BOLT HOLE. REFER TO SNRM NO. N0830 FOR RIGHT HAND WING OUTBOARD FLAP REPLACEMENT.SDR 05FDEA04123Hinge Fitting · corrodedFOUND RIGHT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CORROSION AT INBOARD NR 2 BOLT HOLE. REFER TO SNRM NR N00830 FOR RIGHT HAND WING OUTBOARD FLAP REPLACEMENT.SDR 05FDEA04122Hinge Fitting · corrodedFOUND LEFT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CORROSION AT OUTBOARD NR 3 BOLT HOLE.SDR SWAA053867Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING OTBD T/E AFT FLAP DELAMINATED. REPAIRED FLAP PER SWA EA.SDR DHL2005362AA1Rib · crackedDURING "A" CHECK ACCOMPLISHED INSPECTION OF RT WING INBD. FLAP NOSE RIB NR 7 ON FLAP ASSY. S/N FD 1074 PER S/B A-300-59-240. REMOVED AND REPLACED RIB RN 7 RT AT RT INB. FLAP IAW S/B A-300-57-0240.SDR 05FDEA04113Block · icedDURING FLAP RETRACTION RECEIVED ECAM WARNING FLAP 2 FAULT, FLAP VANE JAM, FLAPS RETRACTION LIMITED, THIS ALL OCCURRED WHEN FLAP HANDLE WAS MOVED FROM 15/0 TO 0/0. FLAPS INDICATED UP, WITH NO VIBRATIONS IN FLIGHT CONTROLS. REMOVED AND REPLACED RT INBD FLAP, SDR 05FDEA04103Repair · misinstalledPREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (TRAILING EDGE WEDGE SECTION - TOP SIDE - COMPOSITE) AT WS 115 TO WS 200. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPRSDR 05FDEA04102Repair · misinstalledPREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (TRAILING EDGE WEDGE SECTION - TOP SIDE - COMPOSITE) AT WS 60 TO WS 110. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROSDR 05FDEA04101Repair · misinstalledPREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (TRAILING EDGE WEDGE SECTION - LOWER SIDE - COMPOSITE) AT WS 40 TO WS 50. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPRSDR AWXA200600091Skin · delaminatedMCN - DURING C16 CHECK DISCOVERED RT OUTBOARD AFT FLAP DELAMINATED AT THE INBOARD TRAILING EDGE FROM WBL 289R TO WBL 309R. MAINTENANCE REMOVED DISBONDED SKIN AND CORE IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPLACEMENT CORE AND DOUBLER IAW BOEING 737SDR DHL2005803528Panel · wornLT IB FLAP UPPER PANEL PLATING WORN 1 INCH APPROX AT STA XW 92.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 12-02-05, DWG AA33-53-R03 REV. JR DATE 11-11-05. REMOVED DAMAGED EXISTING SOLID SEGMENT PLATING IAW SRM 51-1-21. FABRICATED NEW SSDR DHL2005362AA2Rib · crackedDURING "A" CHECK, LT INBD. FLAP NOSE RIB NR 7 CRACKED, REMOVED NOSE SKIN AND RIB NR 7 FROM LT IB FLAP IAW A-300 S/B A-300-57-0242. INSTALLED NEW RIB AND REINSTALLED NOSE SKIN PER S/B A-300-57-0242SDR 05FDEA04085Flap Track · corrodedLEFT WING INBOARD FLAP OUTBOARD TRACK FORWARD MOUNT HOLES (BORES) HAVE CORROSION. REMOVED CORROSION BY REAMING BORES C, D AND E. MAGNETIC PAR- TICLE INSPECTION AND FABRICATED BUSHINGS FOR BORES C, D AND E IAW FEDEX EA NR 7-5710-92592. ALSO, HEAT TREATED,
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