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.

SDR QXEA200500287Skin Panel · wornRT WING FLAP LEADING EDGE PANEL IS WORN. REPAIRED IAW CRJ700 SRM 57-52-01-001-001-A01, 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-01-001-001-A01.Feb 11, 2005 · N609QX · Cndair CL6002C10SDR QXEA200500259Vane · chafedYYC - LEFTHAND INBOARD FLAP VANE INBOARD LEADING EDGE PANEL HAS CHAFE MARK. REPAIRED IAW CRJ700 SRM 51-25-06-001-001-A01 AND SRM 51-25-01-001-001-A01.Feb 11, 2005 · N609QX · Cndair CL6002C10SDR SWAA050402Flap · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD T/E AFT FLAP PER MM.Feb 11, 2005 · N334SW · Boeing 7373H4SDR QXEA200500272Skin · dentedYYC - RIGHTHAND WING, INBOARD FLAP, LOWER SURFACE HAS PITTING AND DENTS. REPAIRED IAW CRJ700 SRM 57-52-01-101-001-A01 AND SRM 51-12-00-001-001-A01.Feb 10, 2005 · N609QX · Cndair CL6002C10SDR QXEA200500271Skin · chafedYYC - LEFTHAND INBOARD FLAP LOWER SKIN SURFACE HAS CHAFE MARK FROM INBOARD HINGE FAIRING. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01.Feb 10, 2005 · N609QX · Cndair CL6002C10SDR QXEA200500262Skin · damagedYYC - LEFT INBOARD FLAP LOWER SKIN, INBOARD SECTION, HAD FOD IMPACT DAMAGE. REPAIRED IAW CRJ700 SRM 57-52-01-101-001-A01 AND 51-12-00-001-001-A01.Feb 10, 2005 · N609QX · Cndair CL6002C10SDR IXXA0500191SVane · delaminatedDURING ROUTINE C-CHECK FOUND LEFT HAND OUTBOARD FLAP INBOARD FLAP VANE DELAMINATED. REMOVED AND REPLACED FLAP VANE, RIG CHECK GOOD IAW DC8 MM 27-51-14.Feb 8, 2005 · N820BX · Doug DC871FSDR 05FDEA00262Skin · damagedRIGHT I/B FLAP LWR T/E DELAMINATED. REMOVED EXISTING REPAIR. DRIED HONEYCOMB CORE IAW A310-200 SRM 51-77-10 PARA 2(G). INSTALLED DOUBLER ON UPPER AND LWR SKINS IAW A310-200 SRM 57-53-12 PARA 11. INSTALLED RIVETS IN T/E IAW A310-200 SRM 51-40-21.Feb 7, 2005 · N405FE · Airbus A310203SDR 05FDEA00257Stop Fitting · crackedRIGHT HAND WING, OUTBOARD FLAP STOP FITTING FOUND CRACKED. STOP FITTING REMOVED AND REPLACED PER DRAWING 4125 AND SRM 51-33-01 VOLUME II.Feb 6, 2005 · N620FE · Doug MD11SDR 05FDEA00252Spar · damagedLEFT HAND INBOARD FLAP WEDGE UPPER FORWARD ATTACH POINT AT OUTBOARD EDGE OF PANEL FIFTH (5) HOLE IS ELONGATED. FABRICATED AND INSTALLED BUSHING IAW FEDEX EA 8-5710-83968, WINGS- LEFT HAND INBOARD FLAP, INBOARD FLAP WEDGE OVERSIZE BOLT HOLE- REPAIR, AND DC10 SFeb 5, 2005 · N304FE · Doug DC1030FSDR 05FDEA00250Skin · corrodedLEFT WING INBOARD FLAP, LOWER SKIN AT TRACK LOWER FILLET FAIRING TRAILING EDGE AREA, HAS SURFACE CORROSION, XIFH 126.650-XIFH 120.908. REMOVED FAIRING AND WEDGE, FABRICATED AND INSTALLED REPAIR IAW FEDEX EA8-5710-83969, WINGS - LEFT HAND INBOARD FLAP, LOWER SFeb 5, 2005 · N304FE · Doug DC1030FSDR 05FDEA00249Hinge · corrodedLEFT HAND OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT BORE CORRODED. REMOVED CORROSION, FABRICATED OVERSIZED BUSHING, INSTALLED AND HONED TO FINAL INSIDE DIAMETER OF 0.8745-0.8755 INCHES, IAW DAC CMM 57-52-02 AND FEDEX EA 8-5710-83965, WINGS- LEFT HAND OUTBOARFeb 5, 2005 · N304FE · Doug DC1030FSDR 05FDEA00248Hinge · corrodedLEFT WING OUTBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE CORRODED. REMOVED CORROSION, FABRICATED OVERSIZED BUSHING, INSTALLED AND HONED BUSHING TO FINAL INSIDE DIAMETER OF 0.8745-0.8755 IAW DAC CMM 57-52-02 AND FEDEX EA 8-5710-83967, PRIMED BORE IAW DC10-3Feb 5, 2005 · N304FE · Doug DC1030FSDR 05FDEA00247Hinge · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD SUPPORT, PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION, FABRICATED, INSTALLED AND HONED BUSHING TO FINAL DIAMETER OF .8745 - .8755 INCHES IAW DAC CMM 57-52-02, PRIMED BORE IAW DC10-30 SRM 51-21-01 VOL II, AND FEFeb 5, 2005 · N304FE · Doug DC1030FSDR IXXA0500192SVane · delaminatedDURING ROUTINE C-CHECK FOUND LEFT HAND FLAP STATION 219 FLAP VANE DELAMINATED. REMOVED AND REPLACED FLAP VANE, RIG CHECK GOOD IAW DC8 MM 27-51-14.Feb 4, 2005 · N820BX · Doug DC871FSDR SWAA050322Skin · delaminatedDURING SCHEDULED RON, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT T/E AFT FLAP PER MM.Feb 4, 2005 · N634SW · Boeing 7373H4SDR SWAA050313Skin · delaminatedDURING SCHEDULED CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING T/E AFT FLAP PER MM.Feb 3, 2005 · N696SW · Boeing 7373T5SDR 05FDEA00233Skin · damagedRIGHT HAND WING INBOARD FLAP TOP SKIN COMPLY WITH EA 6-5750-85635. REMOVED AND REINSTALLED SKIN WITH REPLACEMENT FASTENERS PER SB 300-57-6098 FIG 3 SHEET 2, IAW FEDEX EA 6-5750-85635 REV-A AND DRAWING A579600005.Feb 3, 2005 · N716FD · Airbus A300B4622SDR 05FDEA00232Stop Fitting · crackedLEFT HAND WING, OUTBOARD FLAP STOP FITTING FOUND CRACKED. REMOVED AND REPLACED PER DRAWING ARC4102 AND SRM 51-33-01 VOLUME II.Feb 3, 2005 · N620FE · Doug MD11SDR ASAA0540080Skin · gougedPAE - LT IB FORE FLAP IS GOUGED 44 INCHES FROM IB END, 8 INCHES FROM T/E ON UPPER SURFACE. CUTOUT UPPER SKIN AND CORE (APPROX 56 SQ INCHES) AND REPAIRED WITH HOT BOND IAW SRM. (K)Feb 2, 2005 · N772AS · Boeing 7374Q8SDR QXEA200500373Shroud · chafedYYC - RIGHTHAND INBOARD FLAP IS CHAFING THE UPPER WING SHROUD. REPAIRED IAW RD 8/4-57-001, PAGE 7, NOTE 9.Feb 2, 2005 · N539DS · Bombdr DHC8401SDR QXEA200500374Skin · chafedYYC - RIGHTHAND OUTBOARD FLAP IS CHAFING THE UPPER WING SHROUD. REPAIRED IAW DHC-8 SRM 51-21-12 AND 51-25-10.Feb 2, 2005 · N539DS · Bombdr DHC8401SDR QXEA200500372Skin · chafedYYC - LEFTHAND INBOARD FLAP IS CHAFING THE UPPER WING SHROUD. REPAIRED IAW RD 8/4-57-001, ISSUE 6, PAGE 4, NOTE 9.Feb 2, 2005 · N539DS · Bombdr DHC8401SDR 05FDEA00227Skin · crackedAFTER REMOVAL OF CHAFF PLATE ON RIGHT I/B FLAP, DID HIDDEN DAMAGE INSP FOR N00064, AND FOUND I/B FLAP TOP SKIN HAS 2 EA CRACKS. REPLACED SKIN IAW DWG A57960007 AND EA 6-5750-85635.Feb 2, 2005 · N716FD · Airbus A300B4622SDR 05FDEA00226Rib · crackedAFTER REMOVAL OF I/B FLAP TOP SKIN, PERFORMED HIDDEN DAMAGE INSPECTION AND FOUND NR 2 AIRFOIL RIB AFT SECTION HAS CRACKED APPROX 8.5 INCHES LONG AND NR 3 RIB ON TOP SIDE ANGLE SUPPORT STRUCTURE HAS CRACKED APPROX 2.5 INCHES LONG AND 2 EA STIFFENERS WITH CRACFeb 2, 2005 · N716FD · Airbus A300B4622SDR 0500159985Stringer · crackedDURING H-CHECK FOUND CRACK IN RT FLAP LEADING EDGE STRINGER. REPAIRED PER EA 99-201832.Feb 2, 2005 · N985US · Doug DC932SDR CA050204004Support · worn(CAN) THE DAMAGE OCCURED AROUND THE AFT IB BEARING. THE BEARING WAS FOUND WORN INTO BOTH THE SUPPORT ARMS 0523901-13 AND -14. MFG OFFERS A SERVICE KIT TO REPLACE THESE BRACKETS. SK180-44-1. THIS KIT WAS ISSUED TO REPAIR A DEFECT OCCURING ON THE FRONT ROLLEFeb 1, 2005 · Cessna 172MSDR WRLA2005008Skin · damagedITEM: DURING "C2" CHECK IN TPE, FOUND RIGHT WING INBD FLAP VANE SKIN DISBAND. CUT OUT DAMAGED SKIN AREA WITH 0.5" MIN RADIUS PER MD11 SRM 57-90-00 VOL I AND FAA FORM 8100-9 DATED 01/27/05. ACCOMPLISHED CO-CURE REPAIR USING FM300-2 AT 250DEG "F" FOR 90 TO 100Feb 1, 2005 · N273 · Doug MD11SDR 05FDEA00213Beam · wornLEFT WING NR 2 FLAP TRACK BEAM OUTBOARD SIDE ROLLER PATH HAS THREE WEAR MARKS. REF FED EX EA 6-5720-85940, LT WING NR 2 FLAP TRACK BEAM O/B 3 EA AREAS FOUND TO BE ACCEPTABLE AS IS TO CONTINUE SERVICE, AND TO BE CHECKED AT NEXT C-CHECK.Feb 1, 2005 · N716FD · Airbus A300B4622SDR ASAA0580079Skin · gougedOKC - FOUND DURING C-CHECK, LEFT WING OUTBOARD FLAP VANE HAS GOUGED ON OUTBOARD EDGE. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER. (M)Jan 31, 2005 · N948AS · Doug DC983SDR 2005FA0000386Flap Track · wornDURING PREFLIGHT, THE LT OB FLAP TRACK WAS NOTICED TO HAVE DAMAGE. AIRCRAFT WAS IMMEDIATELY GROUNDED AND THE FLAP TRACKS AND ROLLERS WERE REPLACED WITH NEW PARTS. NO FURTHER DAMAGE HAD OCCURRED TO THE FLAP ASSY. SINCE MFG DOES NOT HAVE LIMITATIONS ON THEIR Jan 31, 2005 · N4992R · Cessna 172HSDR 2005FA0000385Flap Track · wornWHILE FLAPS WERE BEING RETRACTED, THE LT IB FLAP ATTACH BRACKET CAUGHT ON THE WING COVE PANEL SUPPORT. THIS CAUSED SUBSTANTIAL DAMAGE TO THE COVE PANEL SUPPORT AS WELL AS THE ATTACH BRACKET. CAUSE WAS DETERMINED TO BE WORN FLAP TRACKS. THE FLAP TRACKS AND RJan 31, 2005 · N4989R · Cessna 172HSDR AWXA200500326Support · corrodedMCN - FLIGHT CONTROL - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON RT INBOARD MID FLAP OUTBOARD GIMBAL OUTER SUPPORT WBL 185.0. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP OUTBOARD GIMBAL OUTER SUPPORT IAW T/C I3R57057.Jan 31, 2005 · N326AW · Boeing 737301SDR AWXA200500325Gimbal Joint · corrodedMCN - FLIGHT CONTROL - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON RT INBOARD MID FLAP OUTBOARD GIMBAL INDEX PLATE WBL 185.0. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP OUTBOARD GIMBAL ASSEMBLY IAW T/C I3R57057.Jan 31, 2005 · N326AW · Boeing 737301SDR AWXA200500324Support · corrodedMCN - FLIGHT CONTROL - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MID FLAP INBOARD GIMBAL OUTER SUPPORT WBL 71.24. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP INBOARD GIMBAL OUTER SUPPORT IAW BOEING SOPM 20-50-01.Jan 31, 2005 · N326AW · Boeing 737301SDR 2005FA0000198Spar · crackedWHILE REPLACING THE FLAP TRACK ASSY, A CRACK APPROX 2 INCHES IN LENGTH AND RUNNING THROUGH THE LOWER RIVET HOLES WAS FOUND UNDER THE IB FLAP TRACK. PROBABLE CAUSE IS FATIGUE. RECOMMEND THESE AC WITH MORE THAT 8,000 HOURS TT BE INSPECTED BY BORESCOPE OR OTHERJan 31, 2005 · N4992R · Cessna 172HSDR AWXA200500191Gimbal Joint · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MIDFLAP OUTBOARD GIMBAL INDEX PLATE AT WBL 184. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP OUTBOARD GIMBAL ASSEMBLY IAW SOPM 20-50-01.Jan 31, 2005 · N326AW · Boeing 737301SDR AWXA200500190Gimbal Joint · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MIDFLAP OUTBOARD GIMBAL OUTER SUPPORT AT WBL 184. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP OUTBOARD GIMBAL OUTER SUPPORT IAW SOPM 20-50-01.Jan 31, 2005 · N326AW · Boeing 737301SDR WRLA2005011Skin · dentedDURING "C2" CHECK, FOUND RT INBD FLAP LOWER SKIN DENT AT XIFH 139 ABOVE T/E 58" L=0.5" W=0.75" D=0.065". CUTOUT DENT AREA 1.5' BY 1", FABRICATED REPAIR DOUBLER 6" BY 6" (2024-T3 .063" ALU SHEET) AND USED RIVET CR3224-5 TO REPAIR THE DENT. CONDITION CHECK SATJan 31, 2005 · N273 · Doug MD11SDR WRLA2005010Skin · dentedDURING "C2" CHECK, FOUND DENT LOCATED AT RT INBD FLAP LOWER SKIN XIFH193 ABOVE T/E 9" L=1.5" W=0.066". CUTOUT AREA 2 INCH BY 1 INCH AND REPAIRED DAMAGE AREA WITH DOUBLER (2024-T3 .050 ALU SHEET) AND RIVET(CR3224-5). CONDITION CHECK SATISFACTORY REF MD11 SRM Jan 31, 2005 · N273 · Doug MD11SDR WRLA2005009Skin · canningDURING "C2" CHECK FOUND RIGHT INBD FLAP UPPER SKIN HAVE ONE OIL-CANNING AT XIFH 286 ABOVE T/E 24" L=3" W=3". CUTOUT DAMAGED SKIN AND REPAIRED WITH EXTERNAL DOUBLER (2024-T3 .050 CLAD, L=5.625" W=5") AND RIVET (CR32245-4) REF MD11 SRM 57-20-00 VOL I REV 36 FIGJan 31, 2005 · N273 · Doug MD11SDR SWAA050254Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD T/E AFT FLAP PER MM.Jan 29, 2005 · N378SW · Boeing 7373H4SDR AWXA200500201Plate · corrodedMCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON RT INBOARD MID FLAP OUTBOARD GIMBAL INDEX PLATE. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP OUTBOARD GIMBAL INDEX PLATE IAW B737-300 OHM 57-53-22.Jan 28, 2005 · N303AW · Boeing 7373G7SDR AWXA200500200Gimbal Joint · corrodedMCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON RT INBOARD MID FLAP INBOARD GIMBAL OUTER SUPPORT. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP INBOARD GIMBAL OUTER SUPPORT IAW B737-300 OHM 57-53-22.Jan 28, 2005 · N303AW · Boeing 7373G7SDR AWXA200500199Gimbal Joint · corrodedMCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON LT INBOARD MID FLAP INBOARD GIMBAL OUTER SUPPORT. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP INBOARD GIMBAL OUTER SUPPORT IAW B737-300 OHM 57-53-22.Jan 28, 2005 · N303AW · Boeing 7373G7SDR AWXA200500198Gimbal Joint · corrodedMCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON LT INBOARD MID FLAP OUTBOARD GIMBAL SHAFT OUTER SUPPORT. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP OUTBOARD GIMBAL SHAFT OUTER SUPPORT IAW B737-300 OHM 57-53-22.Jan 28, 2005 · N303AW · Boeing 7373G7SDR AWXA200500197Gimbal Joint · corrodedMCN - MAJOR REPAIR - DURING C-16 CHECK GALVANIC CORROSION WAS FOUND ON LT INBOARD MID FLAP OUTBOARD GIMBAL SHAFT INDEX PLATE. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP OUTBOARD GIMBAL SHAFT INDEX PLATE IAW B737-300 OHM 57-53-22.Jan 28, 2005 · N303AW · Boeing 7373G7SDR AWXA200500196Gimbal Joint · corrodedMCN - MAJOR REPAIR - DURING C-16 CHECK GALVANIC CORROSION WAS FOUND ON RT INBOARD MID FLAP OUTBOARD GIMBAL SHAFT OUTER SUPPORT. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP OUTBOARD GIMBAL SHAFT OUTER SUPPORT IAW B737-300 OHM 57-53-22.Jan 28, 2005 · N303AW · Boeing 7373G7SDR SWAA050233Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING T/E AFT FLAP PER MM.Jan 27, 2005 · N502SW · Boeing 7375H4SDR SWAA050227Panel · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD MIDFLAP WEDGE PANEL DELAMINATED. REPAIRED MIDFLAP WEDGE PANEL PER SRM.Jan 27, 2005 · N337SW · Boeing 7373H4
Back to JASC 5753