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 SWAA043329Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Nov 12, 2004 · N508SW · Boeing 7375H4SDR SWAA043327Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LEFT T/E FLAP PER MM.Nov 12, 2004 · N627SW · Boeing 7373H4SDR UIEA200400189Rib · crackedDURING SCHEDULED MAINTENANCE. FOUND CRACK AT RT VARIABLE CAMBER FLAP HINGE RIB ASSEMBLY. TRIMMED THE FLANGE TO REMOVE THE DAMAGE. HFEC THE AFFECTED AREA TO ENSURE DEFECT FREE CONDITION. THE REPAIR AND RESTORATION WAS ACCOMPLISHED TO RESTORE TO THE ORIGINALNov 11, 2004 · N512MC · Boeing 747230BSDR 04FDEA03090Bracket · crackedLT WING OUTBOARD FLAP HINGE FWD FAIRING SUPPORT BRACKET FOUND CRACKED AT INBOARD LOWER. BRACKET REMOVED AND REPLACED PER SRM 51-05-01 VOLUME II.Nov 11, 2004 · N618FE · Doug MD11FSDR SWAA043310Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT T/E AFT FLAP PER MM.Nov 11, 2004 · N526SW · Boeing 7375H4SDR SWAA043309Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT T/E AFT FLAP PER MM.Nov 11, 2004 · N526SW · Boeing 7375H4SDR SWAA043307Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING FLAP PER MM.Nov 11, 2004 · N680AA · Boeing 7373A4SDR SWAA043293Skin · delaminatedDURING SCHEDULED A1 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD T/E FLAP PER MM.Nov 10, 2004 · N515SW · Boeing 7375H4SDR ASAA0410501Skin · chafedOKC - FOUND LEFT WING T/E OUTBOARD MID FLAP HAS TWO CHAFING AREAS IN SKIN, LOWR SURFACE, AREA AT SECOND TRACK FAIRING. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW EA. (M)Nov 9, 2004 · N747AS · Boeing 7372X6CSDR SWAA043277Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT AFT FLAP PER MM.Nov 9, 2004 · N371SW · Boeing 7373H4SDR MWEA040201Panel · bulgedBULGE ON THE TOP SURFACE OF THE RIGHT WING. FABRICATED AND INSTALLED TRAILING EDGE PANEL AND INSTALLED NEW BRACKET AT STATION 118.147.Nov 9, 2004 · N803ME · Doug DC981SDR ASAA0410507Skin · chafedOKC - FOUND RIGHT OUTBOARD MID FLAP CHAFED AT INBOARD LEADING EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOULER IAW SRM. (M)Nov 8, 2004 · N747AS · Boeing 7372X6CSDR DHL2004755518Skin · damagedDURING A "C" CHECK, REPLACE INTERIM REPAIR ON RT WING I/B MID FLAP UPPER SKIN I/B END WITH A PERMANENT REPAIR. REMOVED INTERIM REPAIR FROM RT I/B MID FLAP UPPER I/B T/E TRIMMED OUT DELAMINATED AREA APPROX 1INCH BY 12 INCHES. FABRICATED FILLER APPROX 1 X 12 ANNov 8, 2004 · N755DH · Boeing 727225SDR A6WA200440182Skin · dentedRT IB FLAP BOTTOM SKIN IS DENTED APPROX .7500 INCH LONG X .6250 INCH WIDE AND .040 DEEP WITH GOUGES IN CENTER OF DENT. DENT IS 1.7500 INCH FORWARD OF AFT EDGE AND 8 INCH OB FROM IB ENGINE. PERFORMED A MAJOR REPAIR BY CUTTING OUT DAMAGED SKIN AND INSTALLING DNov 8, 2004 · N440AW · Cndair CL6002B19SDR SWAA043242Skin · delaminatedDURING SCHEDULED A2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD T/E AFT FLAP PER MM.Nov 6, 2004 · N527SW · Boeing 7375H4SDR USAA040935Skin · delaminatedPIT - Q1 - FLAP, 4.5 INCHES BY 5 INCHES DELAMINATION, IB T/E. REMOVED TOP SKIN, CORE, INSTALLED INTERNAL DOUBLER, NEW CORE, EXT DBLR IAW SRM 51-70-10.Nov 5, 2004 · N435US · Boeing 7374B7SDR USAA040934Skin · delaminatedPIT - Q1 - FLAP, 3.5 INCH BY 5 INCH AREA, DELAMINATED, OB T/E. REMOVED TOP SKIN, CORE, INSTALLED INTERNAL DOUBLER, NEW CORE, EXT DBLR IAW SRM 51-70-10.Nov 5, 2004 · N435US · Boeing 7374B7SDR USAA040841Skin · delaminatedSKIN, 4 INCH BY 14 INCH AREA DELAMINATION, LT OB FOREFLAP T/E IB END. DEFECTIVE PART REPLACED WITH IDENT PN.Nov 5, 2004 · N776AU · Boeing 7374B7SDR ABXA040375Vane · damagedAIRFRAME RUMBLE/VIBRATION AT 285 KTS WITH AIRCRAFT CLEAN, VIBRATION CAN BE FELT THROUGH FLOOR AND RUDDER PEDALS. REPLACED RT FLAP FORWARD MOVABLE VANE IAW DC9 MM 27-51-02-4-0001. REPLACED BUSHING IN EYEBOLT ON RT WING T/E UPPER I/B PANEL SUPPORT. REPLACED SNov 5, 2004 · N971AX · Doug DC941SDR CA041116005Shaft · worn(CAN) UPON PERIODIC INSPECTION IT WAS NOTED THAT THERE WAS APPARENT CONTACT BETWEEN THE IB FLAP VANES ON BOTH LT AND RT ASSEMBLIES ONTO THE TORQUE SHAFT AND BEVEL HOUSING ASSY. THIS UNUSUAL CONTACT WAS DEDUCED TO OCCUR DURING FLIGHT LOADS AS THE CLEARANCE BETWNov 4, 2004 · Braero BAE125800ASDR ASOA04934Bracket · crackedDURING C-CHECK INSPECTION, THE BRACKET AT THE LEFT FLAP BEAM ACTUATOR (IB FLAP) WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE BRACKET AT THE LT FLAP BEAM ACTUATOR (IB FLAP) IAW SRM 51-25-02 AND 51-25-01.Nov 4, 2004 · N630AS · Aerosp ATR72212SDR ASOA04933Bracket · crackedDURING C-CHECK INSPECTION, THE OMEGA BRACKET ON THE RT IB FLAP, OB ARM WAS FOUND TO BE CRACKED BEYOND LIMITS.Nov 4, 2004 · N630AS · Aerosp ATR72212SDR SWAA043212Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT INBOARD T/E AFT FLAP PER MM.Nov 4, 2004 · N525SW · Boeing 7375H4SDR ASAA0410465Skin · chafedOKC - LT WING T/E FORE FLAP HAS CHAFING AREA IN OB EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM.Nov 3, 2004 · N747AS · Boeing 7372X6CSDR ASAA0410464Skin · chafedOKC- RT WING IB FORE FLAP UPPER SURFACE HAS 6 AREAS THAT ARE CHAFED TO BARE METAL. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM.Nov 3, 2004 · N747AS · Boeing 7372X6CSDR SWAA043206Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING TRAILING EDGE INBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT T/E INBOARD AFT FLAP PER MM.Nov 3, 2004 · N687SW · Boeing 7373Q8SDR SWIA200414045Roller · bindingCONTROL FAULT ON OUTBOARD PAIR OF FLAPS OCCURS AT TWO BARS OF FLAPS, WILL NOT RESET. REMOVED AND REPLACED ALL 4 ROLLERS OF LEFT OUTBOARD FLAP IAW 27-50-12. CLEANED CANNON PLUGS OF BOTH RIGHT AND LEFT OUTBOARD FLAPS. OPERATIONAL CHECKED GOOD.Nov 2, 2004 · N189SW · Emb EMB120ERSDR SWIA200414213Stringer · crackedLEFT NACELLE FLAP, UPPER SURFACE, INTERNAL STRINGER CRACKED, ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW EMB 120 SRM 51-25-00, 51-12-02, 51-30-01, 51-40-02, 57-50-02.Nov 1, 2004 · N57734 · Emb EMB120ERSDR ASAA0480546Skin · delaminatedC-CHECK- RT IB FLAP VANE HAS DELAMINATION ON LOWER SURFACE. REMOVED DAMAGED SECTION, AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM.Oct 30, 2004 · N969AS · Doug DC983SDR ASAA0480545Skin · dentedC-CHECK- RT IB FLAP LOWER SURFACE IS DENTED 24 INCHES FROM THE T/E AND 17.5 INCHES FROM IB FAIRING SEAL. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER IAW SRM.Oct 30, 2004 · N969AS · Doug DC983SDR ASAA0480544Skin · dentedC-CHECK- RT IB FLAP LOWER SURFACE IS DENTED 11.5 INCHES FROM T/E AND 19.25 INCHES FROM IB FAIRING SEAL. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER IAW SRM.Oct 30, 2004 · N969AS · Doug DC983SDR QXEA200400763Skin · delaminatedPDX - LEFT HAND OUTBOARD FLAP STARTING TO DELAMINATE AT THE INBOARD UPPER CORNER. REPAIRED IAW Q400 SRM TASK 51-22-20-340-801.Oct 30, 2004 · N405QX · Bombdr DHC8401SDR QXEA200400757Skin · chafedPDX - LEFT HAND INBOARD FLAP YW STATION 60.90 THE UPPER FLAP SURFACE HAS A 1 INCH DIAMETER FOULING MARK INTO THE METAL FROM CHAFING WITH THE UPPER SHROUD. REPAIRED IAW HORIZON AIR EA 6-57-244 AND RD 8/4-57-375, STEPS 3-6.Oct 30, 2004 · N405QX · Bombdr DHC8401SDR QXEA200400758Skin · chafedPDX - RIGHT HAND INBOARD FLAP YW STATION 60.90, THE UPPER FLAP SURFACE HAS A 1 INCH DIAMETER FOULING MARK INTO THE METAL FROM CHAFING WITH THE UPPER SHROUD. REPAIRED IAW HORIZON AIR EA 6-57-245 AND RD 8/4-57-375, STEPS 3-6.Oct 30, 2004 · N405QX · Bombdr DHC8401SDR CA041110006Flap Track · worn(CAN) ON INSPECTION FLAP TRACK GROOVES FOUND BADLEY WORN,PARTS WERE REPLACED AS REQUIRED.Oct 29, 2004 · Cessna 150LSDR CA041110005Flap Track · worn(CAN) ON INSPECTION FLAP TRACK GROOVES WERE FOUND BADLEY WORN. PARTS WERE REPLACED AS REQUIRED.Oct 29, 2004 · Cessna 150LSDR QXEA200400765Skin · delaminatedPDX - RIGHT HAND OUTBOARD FLAP HAS TWO AREAS OF DELAMINATION ON THE LOWER SURFACE. REPAIRED IAW RD 8/4-57-383 AND HORIZON AIR EA 6-57-247.Oct 29, 2004 · N405QX · Bombdr DHC8401SDR UPS04843519Support Fitting · corrodedRT FUSELAGE FLAP HINGE STA 3 SUPPORT FITTING CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT ASSY REF SRM 51-1-20D, 51-1-21, UPS EO DC8-5740-21256A.Oct 28, 2004 · N798UP · Doug DC871FSDR USAA040945Skin · delaminatedPIT - Q5 - SKIN TO CORE, 7 INCHES BY 2.5 INCH AREA DELAMINATED, IB RT AFT FLAP TOP SURFACE 34.5 INCHES- 42 INCHES FROM OB END. REMOVED UPPER SKIN AND CORE, INSTALLED NEW CORE AND TOP DOUBLER IAW SRM 51-70-10.Oct 27, 2004 · N516AU · Boeing 7373B7SDR QXEA200400764Flap Track · damagedPDX - EXTERIOR PLATING DAMAGED ON THE RIGHT HAND NR 4 FLAP TRACK INBOARD SIDE ALONG THE SIDE ROLLER PATH. REPAIRED IAW HORIZON AIR EA 6-57-246 AND RD 8/4-57-379.Oct 27, 2004 · N405QX · Bombdr DHC8401SDR SWAA043123Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED LT WING FOREFLAP PER MM.Oct 27, 2004 · N344SW · Boeing 7373H4SDR SWAA043136Carriage · shearedDURING T/E FLAP EXTENSION, HEARD LOUD THUD, NEEDED RT AILERON TO FLY LEVEL. FOUND LT WIN INBD T/E FLAP CARRIAGE SPINDLE SHEARED. REMOVED AND REPLACED LT INBD T/E FLAP CARRIAGE ASSY PER MM.Oct 26, 2004 · Boeing 7372H4SDR SWAA043115Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RIGHT WING T/E INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED RT WING FOREFLAP PER MM.Oct 26, 2004 · N647SW · Boeing 7373H4SDR HL2004755516Skin · dentedDURING A C-CHECK, RIGHT O/B AFT FLAP LOWER SURF WBL 475 HAS LARGE SMOOTH DENT. CUT OUT DENTED AREA OF AFT FLAP LWR SKIN APPROX 5 INCHES ROUND IAW B727 SRM 51-40-20 FIG 32. FABRICATED ONE FILLER APPROX 5 INCHES ROUND & ONE DOUBLER 8 INCHES ROUND FROM 2024 T3 Oct 24, 2004 · N755DH · Boeing 727225SDR DHL2004755515Fairing · crackedDURING A C-CHECK, NR 5 FLAP TRACK MID FAIRING T/E CRACK. REMOVED CRACK MEMBER FROM NR 5 FLAP TRACK MID FAIRING IAW B727 SRM 51-30-2, FABRICATED STRAP 2024-T3 .040 PO 9001298, 20 X 4 INCH IAW B727 SRM 51-20-2. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLOct 22, 2004 · N755DH · Boeing 727225SDR 04FDEA02971Bracket · corrodedRIGHT WING INBOARD FLAP VANE, INBOARD TEE FITTING HOLES HAVE CORROSION AND FORWARD HOLE BORE IS NOT WITHIN EO LIMITS. CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 AND REPAIRED AS PER FEDEX EA 1-5750-81569 TITLE: WINGS TRAILING EDGE FLAPS, RIGHT HAND I/B FLAP VOct 22, 2004 · N602FE · Doug MD11SDR 04FDEA02979Tee Fitting · corrodedLEFT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING BORES FOUND CORROSION ARE NOT WITHIN EO LIMITS. TEE FITTING REPLACED AS PER AMM27-50-22 AND OPERATIONAL TEST CARRIED OUT AS PER AMM 27-50-00.Oct 22, 2004 · N602FE · Doug MD11SDR 04FDEA02978Support Fitting · corrodedRT WING - INBOARD FLAP VANE, OUTBOARD SUPPORT FITTING INBOARD HOLES (03 OFF) ARE CORRODED. ALL BORES ARE NOT WITHIN EO LIMITS. SUPPORT FITTING REPLACED AS PER AMM27-50-24 AND FUNCTIONAL TEST CARRIED OUT AS PER AMM 27-50-00-860-801.Oct 22, 2004 · N602FE · Doug MD11SDR 04FDEA02976Support · corrodedLT WING - INBOARD FLAP VANE, OUTBOARD SUPPORT FITTING INBOARD HOLES (03 OFF) ARE CORRODED AND OUTBOARD HOLES FWD AND CENTER ARE CORRODED. ALL BORES ARE NOT WITHIN EO LIMITS. SUPPORT FITTING REPLACED AS PER AMM27-50-24 AND FUNCTIONAL TEST CARRIED OUT AS PER Oct 22, 2004 · N602FE · Doug MD11SDR 04FDEA02975Support Fitting · corrodedLT WING INBOARD FLAP VANE INBOARD SUPPORT FITTING INBOARD HOLES (03 OFF) ARE CORRODED AND OUTBOARD AFT HOLE IS CORRODED. ALL BORES ARE NOT WITHIN EO LIMITS. SUPPORT FITTING REPLACED AS PER AMM27-50-24 AND FUNCTIONAL TEST CARRIED OUT AS PER AMM 27-50-00-860-Oct 22, 2004 · N602FE · Doug MD11F
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