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.

SDR DHL2005748533Skin · delaminatedLT WING I/B FOREFLAP UPPER SURFACE DELAMINATED APPROX 16" O/B OF I/B END. CUT OUT DELAMINATED UPPER SKIN APPROX 6 1/2" BY 5". CUT OUT DAMAGED CORE APPROX 6 1/2" BY 5". FABED SEPTUM APPROX 6 1/2 BY 5 AND REPAIR CORE APPROX 6 1/2 BY 5 FROM DUR-5052-4.4-3/16 Aug 19, 2005 · N748DH · Boeing 727225SDR 05FDEA02547Fairing · crackedNR 8 FLAP TRACK MOVABLE FAIRING HINGE FITTING IS CRACKED. REPLACED FLAP TRACK FAIRING ON WC 76C001-04Aug 19, 2005 · N479FE · Boeing 727200SDR 05FDEA02546Stiffener · cutRT WING NR 5 FLAP TRACK FAIRING STIFFNER IS CUT. REMOVED AND REPLACED STIFFNER IAW SRM 51-30-2Aug 19, 2005 · N479FE · Boeing 727200SDR SWAA052511Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT LOWER INBOARD END. REMOVED AND REPLACED FLAP PER MM.Aug 18, 2005 · N644SW · Boeing 7373H4SDR ASAA0580471Vane · chafedOKC - FOUND LEFT WING OUTBOARD FLAP INBOARD VANE EXTERNAL DOUBLER IS CHAFED. REMOVED DOUBLER. INSTALLED REPLACEMENT DOUBLER. INSTALLED REPLACEMENT DOUBLER. (M)Aug 17, 2005 · N977AS · Doug DC983SDR DHL2005748524Skin · delaminatedRT WING INBD FORE FLAP DELAMINATED ON UPPER SURFACE 70" FROM OTBD END. CUT OUT DELAMINATED AREA RT I/B FORE FLAP UPPER SURFACE 70" FROM O/B END APPROX 4" DIA FAB FILLER APPROX 4" DIA AND DOUBLER APPROX 7" DIA FROM 2024 T3 .016 PO 9002273, CLEANED PREPPED APPLAug 16, 2005 · N748DH · Boeing 727225SDR DHL2005748523Angle · crackedANGLE CRACKED AT T/E OF RT WING INBD MID FLAP 36" FROM INBD END. CUT OUT CRACKED SECTION OF ANGLE 8 1/2" AND FAB DOUBLER FROM AND 10133-1401, 7075 T6 .063 EXTRUSION 17 3/8" PO501952 FILLER FROM BAC 1509-10861 .050 8 1/2" PO 5079108 IAW B727 SRM 57-50-2 FIG 5 Aug 16, 2005 · N748DH · Boeing 727225SDR DHL2005748518Skin · wornRT WING OTBD FORE FLAP WORN AT L/E 12" FROM INBD END. REMOVED EXISTING REPAIR ON RT WING O/B FORE FLAP L/E IAW B727 SRM 51-30-2 FAB NEW DOUBLER FROM 2024T3 .050 4" BY 5 1/2" PO9002507 IAW B727 SRM 57-50-4 FIG 1. TREATED AND PRIMED DOUBLER IAW B727 SRM 51-10-Aug 16, 2005 · N748DH · Boeing 727225SDR DHL2005748514Trunnion · crackedNR 6 K FLAP ACTUATOR TRUNNION BRACKETS SUPPORT 2EA BOTH L/R ARE CRACKED. NOT CONFIRMED. FAB LEFT AND RIGHT NR 6 K FLAP ACTUATOR TRUNNION BRACKET SUPPORT FROM 7075 T6 .063 PO 9001920 DIM FOR RIGHT SIDE 8" BY 3 1/2" DIM FOR LEFT SIDE 8" BY 3 1/2" IAW B727 SRM Aug 16, 2005 · N748DH · Boeing 727225SDR MALA050656Skin · damagedDURING 4Y/2Y INSPECTION IN BNA, FOUND LT FLAP, L/E HAS HEAT DAMAGE. DAMAGE HAS BEEN REPAIRED IAW MESABA EO#$57100. REF: EAMS WORK ORDER 212767, PN7257800-573, SN 1313.Aug 16, 2005 · N362PX · Saab 340BSDR DHL2005748508Skin · delaminatedL/WING I/B FORE FLAP I/B END DELAM. CUT OUT DELAMINATED AREA OF UPPER I/B END OF L/WING I/B FOREFLAP APPROX 3 1/2" BY 14" AFTER RUBSTEP REMOVAL CUT OUT DAMAGED CORE APPROX 8 1/2" BY 2 3/4" FABBED SEPTUM APPROX 8 1/2" BY 2 3/4" REPAIR SKIN APPROX 3 1/2" BY 14"Aug 15, 2005 · N748DH · Boeing 727225SDR DHL2005748507Skin · dentedL/WING O/B AFT FLAP DENTED ON L/E I/B END. CUT OUT DAMAGED AREA DIM 1" BY 2 1/4" FABRICATED NEW PART PO NR 9001938 2024T3 .050 IAW SRM 57-50-4 FIG 9 5" BY 3 1/2" TREATED AND PRIMED NEW PART IAW B727 SRM 51-10-2. INSTALLED NEW PART IAW SRM 57-50-4.Aug 15, 2005 · N748DH · Boeing 727225SDR USAA051003Wedge · delaminatedCLT - FOUND WEDGE SKIN AND CORE DELAMINATED 2 INCHES BY 3 INCHES, RT L/B T/E FLAP WEDGE AT LB END. REMOVED AND REPLACED SKIN AND CORE AS REQUIRED IAW SRM 51-70-10. (M)Aug 15, 2005 · N449US · Boeing 7374B7SDR SWAA052465Roller · missingDURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD T/E FOREFLAP MID-TRACK ROLLER MISSING. INSTALLED ROLLER PER MM.Aug 15, 2005 · N699SW · Boeing 7373Y0SDR SWAA052458Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.Aug 15, 2005 · N310SW · Boeing 7373H4SDR 05FDEA02464Vane · delaminatedLT WING - DELAMINATION FOUND AT LOWER SURFACE, INBOARD FLAP VANE 17 INCHES FROM INBOARD FLAP, CENTER TRACK. COMPLIED WITH FEDEX EA 1-5750-89965Aug 14, 2005 · N601FE · Doug MD11SDR MALA050649Tab · wornWHILE ACCOMPLISHING C1 INSPECTION, FOUND WEAR MARKS ON THE UNDERSIDE OF THE RIGHT INBOARD FLAP TAB AT THE INBOARD HINGE.Aug 13, 2005 · N522XJ · Bac AVRO146RJ85ASDR SWAA052435Skin · delaminatedRIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.Aug 12, 2005 · N625SW · Boeing 7373H4SDR CA050812003Mount · cracked(CAN) ON THE RT WING IB MOST FLAP MOUNT THERE ARE SEVERAL SMALL CRACKS PROTRUDING OUT OF THE LOWER BOLT HOLE WHICH IS USED TO ATTACH THE BRACKET TO THE REAR SPAR OF THE WING.Aug 11, 2005 · Bbavia 8GCBCSDR 05FDEA02418Skin · dentedLT I/B T/E FLAP, LWR SURFACE SKIN DENTED/GOUGED BEHIND NR 2 LT FLAP JACK SCREW. MEASURED DEPTH OF DENT AT .162 OUT OF LIMITS IAW SRM 57-50-00 FIG 101. INSTALLED REPAIR IAW SRM 57-52-12. REVIEW OF REPAIR REVEALS IT AS UNSAT DUE TO UNAPPLICABLE SRM SCHEME. SAug 11, 2005 · N671FE · Airbus A300F4605RSDR ASAA0540386Skin · chafedYXX: DURING C-CHECK FOUND RT WING OB MIDFLAP T/E LOWER SIDE AT WBL 262, AHS CHAFFE DAMAGE. REPAIRED IAW SRM. (K)Aug 10, 2005 · N778AS · Boeing 7374Q8SDR ASAA0540383Fairing · chafedYXX: DURING C-CHECK FOUND LT OB MID FLAP TRACK FAIRING LOWER SURFACE CHAFED. REPAIRED IAW SRM. (K)Aug 10, 2005 · N778AS · Boeing 7374Q8SDR ASAA0540382Skin · dentedYXX: DURING C-CHECK FOUND LT OB FORE FLAP LOWER SKIN IN LINE WITH NR2 FLAP TRACK HAS 2 DENTS. REPAIRED IAW SRM. (K)Aug 10, 2005 · N778AS · Boeing 7374Q8SDR IXXA05SMN161SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, LT WING NR 4 VANE FLAP LWR SKIN DELAMINATED. REMOVED AND REPLACED NR 4 FLAP VANE (LT WING) IN REPAIRED CONDITION IAW DC8 MM 27-51-14 PAGE 201-202.Aug 9, 2005 · N603AL · Doug DC873FSDR IXXA05SMN160SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, RT WING, NR 3 VANE FLAP LWR. SKIN DELAMINATED. REMOVED AND REPLACED NR 3 FLAP VANE ON RT WING (REPAIRED CONDITION) IAW DC8 MM 27-51-14 PAGES 201-202.Aug 9, 2005 · N603AL · Doug DC873FSDR CA050812004Mount · cracked(CAN) ON THE LT WING IB MOST FLAP MOUNT THERE ARE SEVERAL SMALL CRACKS AND ONE LARGE CRACK PROTRUDING OUT OF THE LOWER BOLT HOLE WHICH IS USED TO ATTACH THE BRACKET TO THE REAR SPAR OF THE WING.Aug 9, 2005 · Bbavia 8GCBCSDR 05FDEA02361Skin · damagedRIGHT WING T/E OUTBOARD FLAP I/B HINGE XORS 562 EXISTING EXTERNAL REPAIR DOUBLER ON LWR SKIN. REPAIR PER SRM 57-00-01 FIG 4 SHEET 2 VOL 1.Aug 9, 2005 · N564FE · Doug MD1010FSDR 05FDEA02334Skin · damagedLEFT WING O/B FLAP XOF 513 EXT REPAIR DOUBLER ON LWR SKIN. REPLACE REPAIR PER SRM 57-10-00 FIG 85 VOL 1.Aug 9, 2005 · N564FE · Doug MD1010FSDR ASAA0580462Skin · damagedOKC - FOUND DURING C-CHECK, LEFT WING OUTBOARD FLAP T/E OUTER SECTION DAMAGED, DENTED. BOND REPAIRED. (M)Aug 8, 2005 · N935AS · Doug DC982SDR ASAA0580459Vane · gougedOKC - DURING C-CHECK, FOUND LEFT INBOARD FLAP VANE GOUGED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER AND FILLER. (M)Aug 8, 2005 · N935AS · Doug DC982SDR SWIA200515391Flap · crackedLEFT NACELLE FLAP IS IN THE DOWN POSITION ROUGHLY 10 DEGREES IN THE FLAPS 0 DEGREE SETTING. REPLACED LT NACELLE FLAP ASSY IAW MM 27-50-02.Aug 7, 2005 · N576SW · Emb EMB120ERSDR SWAA052349Bearing · wornVIBRATION FELT DURING FLAPS OPERATION. FOUND 5 EACH RIGHT INBOARD T/E FOREFLAP TRACK BEARINGS WORN & ONE BEARING BROKEN. REMOVED AND REPLACED BEARINGS PER MM.Aug 5, 2005 · N680AA · Boeing 7373A4SDR ABXA050193Vane · crackedRIGHT FLAP INBOARD FIXED VANE SKIN CRACKED ADJACENT TO REPAIR. REMOVED AND REPLACED INBOARD FIXED VANE IAW DC-9 SRM.Aug 4, 2005 · N965AX · Doug DC941SDR SWAA052342Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM.Aug 4, 2005 · N390SW · Boeing 7373H4SDR ASAA0540375Skin · delaminatedYXX - LT WING OB FORE FLAP, OB END DAMAGED. REMOVED DAMAGE, INSTALLED LWR FILLER, INSIDE DOUBLER ( FOR LOWER SKIN), CORE AND UPPER DOUBLER. (K)Aug 3, 2005 · N778AS · Boeing 7374Q8SDR ASAA0540374Wedge · dentedYXX - LT WING IB T/E MID FLAP WEDGE PANEL NR 7220L HAS 2 EACH DENTS ON THE OB EDGE. REMOVED DAMAGED FIBERS - POTTED PUNCTURE FLUSH AND REPAIRED PLIES INSTALLED AND CURED. (K)Aug 3, 2005 · N778AS · Boeing 7374Q8SDR ASAA0540377Skin · dentedYXX - RT IB FORE FLAP DENT FOUND ON UPPER SURFACE AT WBL 107. REPAIRED DENT IAW SRM. (K)Aug 3, 2005 · N778AS · Boeing 7374Q8SDR A6WA200540282Vane · wornRIGHT OUTBOARD FLAP VANE, OUTBOARD FLAP VANE FITTING WORN EVEN WITH LEADING EDGE OF VANE .030 INCH IS MINIMUM CLEARANCE ALLOWED PER BOMBARDIER, INC REO 601R-57-53-195. REMOVED OLD VANE FITTING FROM RIGHT OUTBOARD FLAP AS WS 296.073 AND INSTALLED NEW VANE FITTAug 3, 2005 · N405AW · Cndair CL6002B19SDR A6WA200540276Vane · wornRT OB FLAP VANE, OB FLAP VANE FITTING WORN EVEN WORN LEADING EDGE OF VANE .030 INCH IS MINIMUM CLEARANCE ALLOWED IAW REO. REMOVED OLD VANE FITTING FROM RT OB FLAP AS WS296.073 AND INSTALLED NEW VANE FITTING IAW REO. (K)Aug 3, 2005 · N405AW · Cndair CL6002B19SDR SWAA052347Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM.Aug 3, 2005 · N671SW · Boeing 7373G7SDR SWAA052318Flap · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Aug 3, 2005 · N305SW · Boeing 7373H4SDR 05FDEA02215Skin · corrodedRIGHT HAND WING UPPER SURFACE TRAILING EDGE FORWARD OF OUTBOARD AILERON SKIN BULGE FOUND AT XORS 850.33. RHW UPPER SURFACE T/E FWD OF O/B AILERON XORS 850.33 SKIN BULGE AREA CORROSION REMOVED. MAT'L REMOVED: 0.023"; ORIG. THK:0.150"; MAT'L REMAINED: 0.127Aug 3, 2005 · N579FE · Doug MD11SDR 05FDEA02212Skin · damagedLEFT WING I/B FLAP BOTTOM SKIN HAS CREASE AT MID SECTION REPAIRED DAMAGED SECTION OF LEFT I/B TRAILING EDGE FLAP LOWER SURFACE SKIN AND 2 EA STRINGERS IAW SRM 57-50-00 FIG 206. PREPPED AND PAINTED IAW MM 51-75-10-8.Aug 2, 2005 · N671FE · Airbus A300B4605RSDR SWAA052293Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.Aug 1, 2005 · N673AA · Boeing 7373A4SDR MALA050624Access Panel · chafedRT FLAP IB END ACCESS PANEL S41AT IS CHAFED AND HAS BEEN REPAIRED IAW MESABA EO 57098 REF EAMS WORK ORDER 212638 TASK 6502.Jul 31, 2005 · N452XJ · Saab 340BSDR MALA050627Access Panel · chafedLT FLAP IB END ACCESS PANEL S41AT IS CHAFED AND HAS BEEN REPAIRED IAW MESABA EO 57098 REF EAMS WORK ORDER 212638 TASK 5504.Jul 31, 2005 · N452XJ · Saab 340BSDR CALA0500251Flap Track · corrodedINSPECTION FOUND THE NR 1 FLAP TRACK CORRODED IN THE AFT UPPER HOLE WHERE THE TRANSMISSION IS ATTACHED. THE AREA WAS REWORKED IAW CMM 57-53-15.Jul 31, 2005 · N19621 · Boeing 737524SDR CALA0500250Flap Track · corrodedINSPECTION FOUND THE NR 2 FLAP TRACK CORRODED IN THE AFT LOWER HOLE WHERE THE TRANSMISSION IS ATTACHED. THE AREA WAS REWORKED IAW CMM 57-53-15.Jul 31, 2005 · N19621 · Boeing 737524SDR CALA0500249Flap Track · corrodedINSPECTION FOUND THE NR 8 FLAP TRACK CORRODED IN AFT O/B HOLE WHERE THE TRANSMISSION IS ATTACHED. THE AREA WAS REWORKED IAW CMM 57-53-15.Jul 31, 2005 · N19621 · Boeing 737524SDR 05FDEA02142Skin · damagedLT WING I/B T/E FLAP LWR SKIN MID O/B SECTION HAS CREASE. FOUND CREASE TO BE OUT OF LIMITS IAW SRM 57-50-00 FIG 101. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS ON MAE TRAVELER T5/532877 LOCATED, DRILLED, AND INSTALLED IAW SRM 57-50-00 FIG 206. TREATED/PRJul 29, 2005 · N671FE · Airbus A300F4605R
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