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 QXEA200500743Arm · gougedYYC - RIGHTHAND WING INBOARD FLAP INBOARD HINGE ARM IS GOUGED ON OUTBOARD SIDE OF THE ATTACH LUG RADIUS. REPAIRED IAW REO 67-57-54-005, HORIZON AIR EA R-57-117, CRJ700 SRM 51-24-11-001-001-A01 AND SRM 51-21-16.Apr 19, 2005 · N614QX · Cndair CL6002C10SDR QXEA200500742Arm · gougedYYC - RT WING INBOARD FORWARD FLAP HINGE ARM AFT EDGE IS GOUGED. REPAIRED IAW REO 57-54-005, HORIZON AIR EA R-57-117 AND CRJ700 SRM 51-24-11-001-001-A01.Apr 19, 2005 · N614QX · Cndair CL6002C10SDR QXEA200500721Flap Track · wornPDX - RIGHTHAND INBOARD FLAP OUTBOARD LOWER FLAP TRACK IS WORN IN THREE PLACES ON THE TOP SURFACE BY THE FLAP ROLLERS. REPAIRED IAW RD 8-57-986 AND DHC-8-200 NDTM PART 6, 51-00-02, PAGES 1-4.Apr 19, 2005 · N346PH · Dhav DHC8202SDR 05FDEA01052Skin · bulgedCOMPLY WITH EA 8-5750-55478,WINGS-LT INBD FLAP-UPPER SKIN BULGE REPAIR AT XIFH=183.3 (P/N ARC2369-503). BFM R COMPLIED WITH EA8-5750-55478-WINGS LT INBOARD FLAP, UPPER SKIN BULGE REPAIR AT XIFH 183.3 (P/N ARC2369-503).Apr 19, 2005 · N370FE · Doug MD1010FSDR ASAA0580210Skin · chafedFOUND RT OUTBOARD FLAP VANE CHAFED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M)Apr 18, 2005 · N972AS · Doug DC983SDR MALA050410Flap · wornDURING C1, C2 INSPECTION IN YYC FOUND RT IB FLAP TAB BOTTOM HAS WEAR MARKS FROM TAB FAIRINGS.Apr 18, 2005 · N503XJ · Bac AVRO146RJ85ASDR QXEA200500701Doubler · chafedPDX - LEFTHAND OUTBOARD FLAP HAS .5 INCH CHAFE MARK ON PREVIOUS REPAIR PATCH ON TOP EXTERIOR SKIN AT WS YW 176.000, 20 INCH FORWARD OF TRAILING EDGE AND 2 INCH INBOARD FROM FLAP EDGE. REPAIRED IAW DHC-8 200 SRM 51-20-16, SRM 51-20-36 AND SRM 51-40-00.Apr 16, 2005 · N346PH · Dhav DHC8202SDR 05FDEA01027Vane · damagedRT WING I/B FLAP VANE I/B T-FITTING FOUND OUT OF LIMIT. REMOVED AND REPLACED AS PER CMM 57-52-03.Apr 16, 2005 · N576FE · Doug MD11SDR 05FDEA01026Vane · corrodedRT WING I/B FLAP VANE O/B T-FITTING FOUND CORRODED. RT WING I/B FLAP VANE O/B TEE FITTING REMOVED AND REPLACED AS PER CMM 57-52- 03, REFER WORK CARD E1-5750-7-5005 A2 PT 2.Apr 16, 2005 · N576FE · Doug MD11SDR QXEA200500734Housing · gougedYYC - LT WING TRAILING EDGE OUTBOARD FLAP GUIDE ROLLER HOUSING GOUGED AT WING STATION 147.50. REPAIRED IAW CRJ700 SRM 57-51-02-201-001-A01 AND 51-24-11-001-001-A01.Apr 15, 2005 · N614QX · Cndair CL6002C10SDR QXEA200500759Skin · chafedYYC- LEFT INBOARD FLAP LOWER EXTERNAL SURFACE HAS CHAFE MARKS UNDER INBOARD HINGE ARM FAIRING. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, 57-52-01-101-001-A01, AND 51-25-01-001-001-A01.Apr 14, 2005 · N614QX · Cndair CL6002C10SDR QXEA200500730Skin · damagedYYC - LT INBOARD FLAP LOWER SKIN HAS GRAVEL DAMAGE. REPAIRED IAW HORIZON AIR EA R-57-113, REO 670-57-52-024 AND CRJ700 SRM 51-25-101-001-001-A01.Apr 14, 2005 · N614QX · Cndair CL6002C10SDR MALA050356Flap Track · wornDURING C2 INSPECTION FOUND LEFT AND RIGHT FLAP TRACK SHUTTERS WORN.Apr 14, 2005 · N503XJ · Bac AVRO146RJ85ASDR SWAA051116Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND LT WING T/E OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.Apr 14, 2005 · N678AA · Boeing 7373A4SDR SWAA051114Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING T/E INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.Apr 14, 2005 · N665WN · Boeing 7373Y0SDR 05FDEA00999Flap Track · damagedCOMPLY WITH EA 6-5720-86138 REV NO POS P2 WING INSPECTION FLAP TRACK MOVABLE FAIRING. LT NR 2, 4, 5 AND RT NR 3,5. COMPLIED WITH EAN 6-5720-86138 AND REPORTED FINDINGS TO FED EX VIA MAXI MERLIN.Apr 14, 2005 · N402FE · Airbus A310SDR QXEA200500796Fitting · corrodedYYC - RIGHT OUTBOARD FLAP INBOARD ROLLER FITTING HAS FRETTING CORROSION. REPAIRED IAW REO 670-57-53-015, SRM 51-25-16-001-001-A010 AND SRM 51-24-11.Apr 13, 2005 · N614QX · Cndair CL6002C10SDR QXEA200500791Skin · damagedYYC - RIGHT INBOARD FLAP LOWER SKIN HAS GRAVEL DAMAGE. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01 AND SRM 51-25-01-001-001-A01.Apr 13, 2005 · N614QX · Cndair CL6002C10SDR QXEA200500733Fitting · corrodedYYC - RIGHTHAND OUTBOARD FLAP INBOARD ROLLER FITTING HAS FRETTING CORROSION. REPAIRED IAW REO 670-57-53-015 AND CRJ700 SRM 51-25-16-001-001-A01.Apr 13, 2005 · N614QX · Cndair CL6002C10SDR QXEA200500698Skin · chafedPDX - RIGHTHAND WING, OUTBOARD FLAP, CHAFE ON TOP SURFACE 2.25 INCH FROM INBOARD EDGE X20 AND 20 1/4 INCH UP FROM TRAILING EDGE. REPAIRED IAW RD 8-57-1734.Apr 13, 2005 · N346PH · Dhav DHC8202SDR QXEA200500699Skin · chafedPDX - RIGHTHAND WING, OUTBOARD FLAP, CHAFE ON TOP SURFACE STARTING 32.5 INCH FROM INBOARD END AND RUNNING OUTBOARD TO 83.5 INCH FROM INBOARD END. REPAIRED IAW RD 8-57-1022.Apr 13, 2005 · N346PH · Dhav DHC8202SDR 05FDEA00997Hinge · corrodedLT WING O/B FLAP O/B REAR SPAR MOUNTED HINGE ACTUATOR HOLE EVIDENT OF CORROSION. LT WING O/B FLAP O/B REAR SPAR MOUNTED HINGE ACTUATOR CORROSION REMOVED & FOUND I/B & O/B LUG HOLES EXCEED LIMITS AS PER CMM 57-44-09 .I/B & O/B LUG SPOTFACES THK W/I LIMITS AS PApr 13, 2005 · N576FE · Doug MD11SDR 05FDEA00992Fitting · corrodedCOMPLY WITH EA8-5750-55470, WINGS-RT OUTBD FLAP INBD HINGE LUG CORROSION REPAIR P/N ARC1984. CLOSING ACTION ON 04/12/05. ON N/RS00012. COMPLIED WITH EA 8-5750-55470.Apr 13, 2005 · N370FE · Doug MD1010FSDR ASAA0540211Skin · dentedIB FORE FLAP HAS NUMEROUS DENTS IN LOWER SKIN SURFACE. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM. (K)Apr 11, 2005 · N795AS · Boeing 737490SDR 2005UALA00341Attach Angle · crackedRT WING INBOARD FLAP, INBOARD HINGE SUPPORT ATTACH ANGLE CRACKED OUTBOARD SIDE. THE SUBJECT HINGE SUPPORT FITTING CRACKED DUE TO FATIGUE LOAD. THE CRACKED AREA WAS REPAIRED PER 767-300 SRM 57-53-02.Apr 11, 2005 · N665UA · Boeing 767322SDR SWAA051051Skin · delaminatedDURING SCHEDULED 5Y CHECK, FOUND RIGHT WING INBOARD AFT T/E FLAP LOWER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.Apr 11, 2005 · N769SW · Boeing 7377H4SDR SWAA051048Flap · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Apr 11, 2005 · N634SW · Boeing 7373H4SDR 05FDEA00921Skin · damagedRIGHT WING O/B MID FLAP UPPER SKIN FWD EDGE IS GOUGED AND BENT AT NR 7 CARRIAGE. REPAIRED RIGHT WING O/B MID FLAP UPPER SKIN FWD EDGE AT NR 7 FLAP CARRIAGE PER EA 7-5710-86274.Apr 10, 2005 · N272FE · Boeing 727200SDR 2005UALA00316Fairing · contaminatedSMOKE NOTICED EMANATING FROM LEFT WING AREA. INSPECTED LT IB FLAP TRACK FAIRING. FOUND NO SIGNS OF HYD LEAKS. HYD QTY CHECKED OK. RAN NR 1 ENGINE AND OPERATED FLAPS. ALL OPS NORMAL NO SMOKE OR VAPORS FOUND. FLIGHT CREW REPORTED THAT IT HAD RAINED HARD IN GApr 9, 2005 · N841UA · Airbus A319131SDR 05FDEA00909Hinge · corrodedLEFT WING O/B FLAP, O/B FLAP MOUNTED HINGE ACTUATOR HOLE EVIDENT OF CORROSION. CORROSION REMOVED AS PERCMM 20-11-02.Apr 8, 2005 · N576FE · Doug MD11SDR 05FDEA00908Hinge · corrodedLT WING O/B FLAP, O/B FLAP MOUNTED HINGE PIVOT HOLE EVIDENT OF CORROSION. CORROSION REMOVED AS PER CMM 20-11-02.Apr 8, 2005 · N576FE · Doug MD11SDR 05FDEA00907Hinge · corrodedLT WING O/B FLAP, I/B FLAP MOUNTED HINGE PIVOT HOLE EVIDENT OF CORROSION. CORROSION REMOVED AS PER CMM 20-11-02.Apr 8, 2005 · N576FE · Doug MD11SDR 05FDEA00906Hinge · corrodedLEFT WING O/B FLAP, I/B FLAP MOUNTED HINGE ACTUATOR HOLE EVIDENT OF CORROSION. REMOVAL & REPAIR. REFER TO EO E1-5750-7-5002 CI. PT 1.Apr 8, 2005 · N576FE · Doug MD11SDR 05FDEA00905Hinge · corrodedRIGHT WING O/B FLAP MOUNTED HINGE PIVOT HOLE EVIDENT OF CORROSION. CORROSION REMOVED AS PER CMM 20-11-00.Apr 8, 2005 · N576FE · Doug MD11SDR 05FDEA00904Hinge · corrodedRIGHT WING O/B FLAP MOUNTED HINGE ACTUATOR HOLE EVIDENT OF CORROSION. CORROSION REMOVED AS PER CMM 20-11-02.Apr 8, 2005 · N576FE · Doug MD11SDR ASAA0540209Wedge · dentedLT WING IB MID FLAP WEDGE IS DENTED. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM. (K)Apr 7, 2005 · N795AS · Boeing 737490SDR QXEA200500797Flap Track · gougedYYC - RIGHT WING OUTBOARD FLAP INBOARD GUIDE ROLLER TRACK GOUGED. REPLACED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.Apr 7, 2005 · N614QX · Cndair CL6002C10SDR 05FDEA00877Hinge · corrodedRIGHT WING O/B FLAP I/B FLAP MOUNTED HINGE ACTUATOR HOLE EVIDENT OF CORROSION. CORROSION REMOVED AS PER CMM 20-11-02.Apr 6, 2005 · N576FE · Doug MD11SDR 05FDEA00876Hinge · corrodedRIGHT WING O/B FLAP I/B FLAP MOUNTED HINGE PIVOT HOLE EVIDENT OF CORROSION. CORROSION REMOVED AS PER CMM 20-11-02.Apr 6, 2005 · N576FE · Doug MD11SDR SWAA051020Wedge · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING INBOARD MAIN FLAP OUTBOARD T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SWA EA.Apr 6, 2005 · N788SA · Boeing 7377H4SDR 05FDEA00842Strap · crackedLEFT WING, OUTBOARD FLAP INBOARD HINGE TENSION STRAP SUPPORT CRACKED, FOUND ON THE SPOTFACE OF THE UPPER BOLT HOLE AT 3 O'CLOCK AND LOWER BOLT HOLE AT 6 O' CLOCK POSITIONS (VIEW LOOKING INBOARD) WITH CRACK. LENGTH APPROXIMATELY ONE-FOURTH (1/4) INCH AND ONE-EApr 5, 2005 · N583FE · Doug MD11SDR 05FDEA00846Hinge · corrodedFLAP MOUNTED HINGE PIVOT BORE CORROSION REPAIR P/NARC2513-1. COMPLIED WITH EA 8-5750-55462.Apr 5, 2005 · N301FE · Doug DC1030FSDR 05FDEA00843Strap · crackedRT WING, OUTBOARD FLAP INBOARD HINGE, TENSION STRAP SUPPORT FOUND CRACKED. KIT P/N 1575075004-0. REPLACED PER FEDEX EO 1-5750-7-5004 PART 2.Apr 5, 2005 · N583FE · Doug MD11SDR DHL2005783521Skin · gougedRT WING INBD FOREFLAP LE IS GOUGED AT OB END WBL 240. REMOVED EXISTING DOUBLER REPAIR IAW B727 SRM 51-30-2 FABRICATED DOUBLER USING 2024T3 .063 PO NR 9002149 DIM. 4 1/2" BY 4 1/2" IAW B727 SRM 57-50-2 AND 57-50-4 FIG 1. ALODINE AND PRIMED DOUBLER AND AREA IAApr 4, 2005 · N783DH · Boeing 727227SDR DHL2005783517Skin · delaminatedRT WING I/B FOREFLAP PREVIOUS REPAIR IS DISBONDED ON LOWER SURFACE WBL 220. REMOVED RT I/B TE FOREFLAP FOR REPAIR IAW B727 MM. REMOVED PREVIOUS REPAIR AND CUTOUT DAMAGE AREA APPROX 4 INCH DIAMETER IAW SRM. FABRICATED ONE FILLER APPROX 4 INCH ROUND AND ONE DApr 4, 2005 · N783DH · Boeing 727227SDR DHL2005783506Skin · damagedLT OB AFT FLAP LOWER SURFACE, WBL 432 HAS A LARGE SMOOTH DENT. CUT OUT DAMAGED AREA APPROX 3 INCH DIAM L/W O/B FLAP LOWER SKIN IAW B727 SRM 51-40-20 FIG 31. FABRICATED ONE FILLER APPROX 3 INCH ROUND AND ONE DOUBLER APPROX 6 INCH ROUND USING 2024T3 .016 PO NRApr 3, 2005 · N783DH · Boeing 727227SDR AWXA200500490Skin · chafedMCN - MAJOR REPAIR - DURING C-19 CHECK THE LEFT INBOARD MID-FLAP LOWER SKIN WAS FOUND CHAFED AT WS 100. MAINTENANCE BLENDED OUT DAMAGE ON LEFT INBOARD MID-FLAP LOWER SKIN AT WS 100; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5753-05112-RC2.Apr 2, 2005 · N174AW · Boeing 73733ASDR AWXA200500493Skin · chafedMCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE LOWER CENTER SECTION SKIN OF THE LEFT OUTBOARD FORE-FLAP CHAFED AT WBL 298. MAINTENANCE CUT OUT CHAFED SKIN ON LOWER CENTER LT OUTBOARD FORE-FLAP AT WBL 298; FABRICATED NEW SKIN SECTION AND A DOUBLER; BONDED REApr 1, 2005 · N174AW · Boeing 73733ASDR AWXA200500491Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK THE LT OUTBOARD FORE-FLAP WAS FOUND DELAMINATED AT THE UPPER AFT OUTBOARD CORNER. MAINTENANCE CUT OUT DAMAGE ON LT OUTBOARD FORE-FLAP AT UPPER AFT OUTBOARD CORNER BETWEEN WBL 410.11 AND WBL 413.6; FABRICATED A FILLER ANDApr 1, 2005 · N174AW · Boeing 73733ASDR SWAA050980Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND RT WING OUTBOARD T/E FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.Mar 31, 2005 · N670SW · Boeing 7373G7
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