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 06FDEA1636Flap · corrodedLT WING IB FLAP LOWER SURFACE FOUND SURFACE CORROSION. CORROSION CLEANED AS PER AMM 12-26-02 AND TREATED AS PER SRM 51-21-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Apr 28, 2006 · N618FE · Doug MD11SDR QXEA200601303Skin · chafedYYC - C4 RIGHT HAND INBOARD FLAP TOP SKIN HAS CHAFED MARK FROM TRAILING EDGE. REPAIRED IAW SRM 51-20-11, SRM 57-50-16, AND SRM 51-20-51.Apr 27, 2006 · N355PH · Dhav DHC8202SDR MALA060278Access Panel · dentedDURING 2 YEAR CHECK IN BNA, FOUND LT FLAP ACCESS PANEL 541AT, IS DENTED AND HAS BEEN REPAIRED IAW MESABA EO#S57060. REF: EAMS WORK ORDER 213767 TASK 5504.Apr 27, 2006 · N441XJ · Saab 340BSDR ASAA0640513Skin · dentedFOUND RT IB FORE FLAP HAS SHARP DENT ON LWR SURFACE 28" FM IB END. REPAIRED PER SRM 51 70 10 REPAIR 4.Apr 27, 2006 · N782AS · Boeing 7374Q8SDR ABXA060246Skin · corrodedRIGHT INBOARD FLAP TRAILING EDGE PANEL BULGED AROUND NUMEROUS FASTENERS. REPLACED RIGHT INBOARD FLAP ON NR 0121 IAW B767 SRM.Apr 26, 2006 · N784AX · Boeing 767281SDR 06FDEA1605Fitting · damagedLEFT INBOARD FLAP AFT UPPER ROLLER SUPPORT STRUCTURE CENTER BOLT HOLE FOUND DAMAGED.Apr 26, 2006 · N526FE · Doug MD11SDR 06FDEA1604Wedge · severedLT INBOARD FLAP TRAILING EDGE WEDGE ATTACH CHANNEL OUTBOARD REMOVABLE SEGMENT FOUND SEVERED AT THE OUTBOARD MOST 12 INCH (MATERIAL CLAD 2024-T42 SHEET 0.04 INCH).Apr 26, 2006 · N526FE · Doug MD11SDR SWAA061405Failsafe · corrodedDURING SCHEDULED 10Y CHECK, FOUND RT WING T/E FLAP INBOARD FAIL SAFE STRAP CORRODED. R&R FAIL SAFE STRAP PER SRM.Apr 25, 2006 · N629SW · Boeing 7373H4SDR SWAA061403Torque Tube · corrodedDURING SCHEDULED 10Y CHECK, FOUND LT WING T/E INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED LT WING MID FLAP INBOARD TORQUE TUBE PER SRM AND CMM.Apr 25, 2006 · N629SW · Boeing 7373H4SDR CA060424006Spar · damaged2 HOLES FOR MOUNTING INBD FLAP HINGE BRACKET LWR ATTACH AND INBD BOLT FOR SHIM PLATE BOTH FOUND CRUDELY DRILLED AND VERY OVAL.Apr 24, 2006 · Bbavia 8GCBCSDR AWXA200600724Fitting · crackedDURING C11 CHECK DISCOVERED THE LEFT WING, OUTBOARD TRAILING EDGE FLAP, CENTER/OUTBOARD AFT FLAP SUPPORT TRACK, OUTBOARD FITTING WAS CRACKED 6.7 INCHES. MAINTENANCE REMOVED AND INSTALLED NEW LEFT WING, OUTBOARD TRAILING EDGE FLAP, CENTER/OUTBOARD AFT FLAP SUPApr 24, 2006 · N903AW · Boeing 7572S7SDR 06FDEA1589Hinge · corrodedCORROSION PIVOT BORE AT RT WING INBOARD FLAP OUTBOARD HINGE ON THE WING SIDE. REPAIRED AS PER CMM 57-44-07 PAGE 403-404 AND EA 1-5750- 94700.Apr 24, 2006 · N526FE · Doug MD11SDR 06FDEA1586Hinge · corrodedFOUND CORROSION, SIDE LINK ATTACHMENT SPOT FACE AT LT WING OUTBD FLAP OUTBD HINGE ON THE WING SIDE. CORROSION REMOVED AS PER CMM 57-44-09 PAGE 402-407 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0503 AND REPAIRED AS PER CMM 57-44-09.Apr 24, 2006 · N526FE · Doug MD11SDR 06FDEA1585Hinge · corrodedFOUND CORROSION, LOWER ATTACHMENT INBD BORE AT LT WING OUTBD FLAP OUTBD HINGE ON THE WING SIDE. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94681.Apr 24, 2006 · N526FE · Doug MD11SDR 06FDEA1584Hinge · corrodedFOUND CORROSION, ACTUATOR ATTACHMENT OUTBD BORE AT LT WING OUTBD FLAP OUTBD HINGE ON THE WING SIDE. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94681.Apr 24, 2006 · N526FE · Doug MD11SDR 06FDEA1583Hinge · corrodedFOUND CORROSION, ACTUATOR ATTACHMENT INBD BORE AT LT WING OUTBD FLAP OUTBD HINGE ON THE WING SIDE. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94681.Apr 24, 2006 · N526FE · Doug MD11SDR 06FDEA1582Hinge · corrodedFOUND CORROSION, SIDE LINK ATTACHMENT SPOT FACE AT LT WING OUTBD FLAP INBD HINGE ON THE WING SIDE. CORROSION REMOVED AS PER CMM 57-44-08 PAGE 612-615 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0502 AND REPAIRED AS PER CMM 57-44-08.Apr 24, 2006 · N526FE · Doug MD11SDR 06FDEA1581Hinge · corrodedFOUND CORROSION, LOWER ATTACHMENT SPOT FACE AT LT WING OUTBD FLAP INBD HINGE ON THE WING SIDE. CORROSION REMOVED AS PER CMM 57-44-08 PAGE 602-607 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0502 AND REPAIRED AS PER CMM 57-44-08.Apr 24, 2006 · N526FE · Doug MD11SDR 06FDEA1580Skin · dentedEXISTING DENT FOUND AT LT WING INBD FLAP ASSY UPP SURFACE LOCATED 37 INCH FROM INBD AND 30 INCH FROM AFT. FOUND EXCEED LIMIT AND REPAIRED AS PER SRM 57-10-00 FIG. 34 VOL.I. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.Apr 24, 2006 · N526FE · Doug MD11SDR 2006UALA00765Stiffener · crackedRT NR 6 FLAP TRACK FAIRING AFT INBD STIFFENER CRACKED IN UPPER RADIUS THRU FASTENER HOLE AND CRACKED IN HALF, THRU CENTER OF PART. REMOVED AND REPLACED THE STIFFENER REF SRM 51-40-02Apr 22, 2006 · N932UA · Boeing 737522SDR SWAA061362Flap · delaminatedDURING SCHEDULED 10Y CHECK, FOUND RT WING T/E AFT FLAP DELAMINATED. REPAIRED RT WING FLAP PER SRM, SB AND CMM.Apr 21, 2006 · N632SW · Boeing 7373H4SDR SWAA061361Flap · delaminatedDURING SCHEDULED 10Y CHECK, FOUND LT WING T/E AFT FLAP DELAMINATED. REPAIRED LT WING FLAP PER SRM, SB AND CMM.Apr 21, 2006 · N632SW · Boeing 7373H4SDR UPS06246882Carriage · corrodedINSPECTION TYPE:C T/E FLAP CARRIAGE NR 4 PITTING CORROSION IN BORE OF SPINDLE CARRIAGE ASSY REPLACED IAW OHM 27-58-02.Apr 20, 2006 · N954UP · Boeing 727185CSDR SWAA061349Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING T/E INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED LT WING FOREFLAP PER MM.Apr 20, 2006 · N690SW · Boeing 7373G7SDR SWAA061346Wedge · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING T/E MID FLAP WEDGE PANEL DELAMINATED. REMOVED AND REPLACED RT WING T/E MID FLAP PER MM.Apr 20, 2006 · N690SW · Boeing 7373G7SDR SWAA061344Structure · crackedDURING SCHEDULED 10Y CHECK, FOUND LT WING T/E AFT FLAP INBOARD END CAP CRACKED. REPAIRED LT TRAILING EDGE AFT FLAP INBOARD END CAP PER BOEING SB AND SRM.Apr 20, 2006 · N632SW · Boeing 7373H4SDR CALA0600128Attach Bracket · crackedLT WING UPPER SURFACE T/E PANEL ATTACH BRACKET CRACKED O/B OF NR 3 FLAP FAIRING. REPLACE BRACKET PER 51-40-02.Apr 20, 2006 · N76354 · Boeing 7373T0SDR DYV2006F00001Bearing · damagedTHE ROLLER BEARINGS HAVE VERY LITTLE SIDE CLEARANCE BETWEEN THE BEARING AND THE FLAP RIBS. AS THE BEARING WEARS SIDE PLAY INCREASES TO THE POINT WHERE THE BEARING FLANGE CONTACTS THE RIB. MDG HAS NOT PROVIDED ANY CHAFE PROTECTION ON THIS SIDE OF THE BEARING,Apr 18, 2006 · N590GM · Beech C90SDR DYV2006F00000Bearing · damagedTHE ROLLER BEARINGS HAVE VERY LITTLE SIDE CLEARANCE BETWEEN THE BEARING AND THE FLAP RIBS. AS THE BEARING WEARS SIDE PLAY INCREASES TO THE POINT WHERE THE BEARING FLANGE CONTACTS THE RIB. MFG HAS NOT PROVIDED ANY CHAFE PROTECTION ON THIS SIDE OF THE BEARING,Apr 18, 2006 · N1083S · Beech C90SDR SWAA061297Failsafe · corrodedDURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD T/E MIDFLAP INBOARD FAIL-SAFE TUBE CORRODED. REMOVED AND REPLACED TUBE PER CMM.Apr 17, 2006 · N632SW · Boeing 7373H4SDR SWAA061296Rib · corrodedDURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD T/E MIDFLAP INBOARD END RIB CORRODED. REMOVED AND REPLACED RIB PER SRM.Apr 17, 2006 · N632SW · Boeing 7373H4SDR 06FDEA1486Skin · delaminatedRIGHT WING I/B FORE FLAP DELAMINATED MID SPAN ON UPPER SURFACE. *S/D* REPAIRED DELAM ON UPPER SURFACE ON RIGHT WING I/B FORE FLAP PER SRM 51-40-20.Apr 17, 2006 · N192FE · Boeing 727100SDR DU4R2006371Skin · delaminatedN/R 24751) FOUND SMALL AREA OF DELAMINATION OF UPPER IB SKIN LT IB FORE FLAP. CUT OUT DELAMINATED (DISBONDED) AREA ON UPPER SKIN LT IB FORE FLAP. FABRICATED AND BONDED DOUBLER 6.5 X 5.6250 INCH AND FILLER 3.3750 INCH X 1.2500 INCH FROM 2024-T3 .016 IAW SRM 5Apr 14, 2006 · N289MT · Boeing 727223SDR DU4R2006370Skin · delaminatedNR 24718 DENTED AND DISBONDED RT IB FORE FLAP UPPER SKIN 19 INCHES FROM IB EDGE. REPAIRED DENTED AND DISBONDED RT IB FORE FLAP UPPER SKIN 19 INCHES FROM IB EDGE BY CUTTING OUT DELAMINATED AREA, APPROX 5 INCHES IN DIAMETER. FABRICATED AND INSTALLED DOUBLER ANApr 14, 2006 · N289MT · Boeing 727223SDR CA060413009Spar · corroded(CAN) LT OB MAIN FLAP AFT SPAR UPPER CHORD 44 INCHES OB OF MAIN FLAP IB EDGE. (TC NR 20060413009)Apr 13, 2006 · Boeing 757200SDR QXEA200601628Skin · misrepairedYYC - C3 LEFT WING, OUTBOARD FLAP UNDER SIDE AT YW212.0 HAS INCORRECT RIVET NUT INSTALLED. REPAIRED IAW DHC-8-400 SRM 51-42-65.Apr 12, 2006 · N425QX · Bombdr DHC8402SDR DU4R2006361Flap · debondedS/O 304001) N/R 21640 - LT IB FT FLAP IB END HAS AREA OF DEBOND. REPAIRED BY CLEANING, PREPPED AND REPAIRED IAW SRM 51-40-21 FIG. 1.Apr 12, 2006 · N289MT · Boeing 727223SDR DU4R2006360Flap · chafedS/O 304001) N/R 21637 - LT IB FORE FLAP UNDER SIDE LEADING EDGE 8 INCHES FROM OB END HAS CHAFED AREA. BLENDED CHAFED AREA, FOUND OUT OF LIMITS, FABRICATED AND INSTALLED DOUBLER 3.750 INCHES X 6.0 INCHES FROM 2024-T3 .063 IAW SRM 57-50-04 PG. 2-3.Apr 12, 2006 · N289MT · Boeing 727223SDR DU4R2006359Flap · delaminatedS/O 304001 N/R 21634 - LT IB FORE FLAP UPPER SIDE HAS DISBOND AFT OF CENTER ACCESS PANEL. CUT OUT DISBONDED UPPER SKIN AND HONEYCOMB. FABRICATED AND BONDED DOUBLERS 13-5/8" X 11" AND 12-1/2" X 11-1/4" AND 9-1/4" X 8? X 5" X 5" X 5" FROM 2024-T3 .016 AND ANApr 12, 2006 · N289MT · Boeing 727223SDR 06FDEA1349Support Fitting · corrodedLT WING O/B FLAP I/B HINGE SUPPORT FITTING (ARC4009) O/B NR 3 BOLT HOLE FOUND CORROSION. LT WING O/B FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30- 4. OPERATIONAL CHECK AND ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATISFACTORY.Apr 10, 2006 · N595FE · Doug MD11SDR 06FDEA1348Fitting · crackedRT WING O/B FLAP SECONDARY UP STOP SUSPECT CRACK. RT WING O/B FLAP SECONDARY UP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.Apr 10, 2006 · N595FE · Doug MD11SDR UIEA200600078Support Fitting · corrodedCORROSION FOUND ON NR 4 BEARING SUPPORT FITTING, P/N 65B08410-5 BY SIAGE W/SHOP DURING LT INBD TE MID FLAP SHOP VISIT. POS 002, P/N 65B02025-35, S/N 000388. BEARING SUPPORT FITTING P/N 65B08410-5 REPAIR CARRIED OUT IAW BOEING REPAIR NR 1-168327827 BY W/SHOP. Apr 10, 2006 · N540MC · Boeing 747243BSDR UIEA200600077Bushing · corrodedCORROSION FOUND IN BUSHING BORES OF INBD FLAP TRACK ASSY NR 4 BY SIAGE WORKSHOP DURING REPAIR (SHOP VISIT) P/N 65B17064-13, S/N 0039. REPAIR CARRIED OUT IAW BOEING REPAIR NR 1-171550575 BY W/SHOP. REFER TO SWJC NR MS 130382145 AND SWJC NR E-W3LG000130382145 Apr 10, 2006 · N540MC · Boeing 747243BSDR NOCA03306Fitting · looseLEFT HAND FLAP OUTBOARD FORWARD MAINFLAP CARRIAGE FITTING LOOSE.Apr 8, 2006 · N750NA · Boeing 75728ASDR EIA2006072Flap Track · damagedDURING C CHECK, DISCREPANCIES FOUND IN THE NR 5 FLAP TRACK FWD SUPPORT FITTING. INSTALLATION OF BUSHING AND BEARING PER S/B 747-57-22262 REV 4- STEEL FITTING PER DRWG 65B16774 ALL REWORK OTHERWISE CONFORMS TO DRWG 65B16774, 65B16768, SB 747-57-2262 REV 4 AND Apr 7, 2006 · N477EV · Boeing 747SR46SDR IXXA06RNG041SSkin · misrepairedDURING ROUTINE C CHECK FOUND AN IMPROPER REPAIR ON INBOARD FLAP LOWER SKIN STATION XW 63.604 TO 50.232 RIGHT. IMPROPER REPAIR WAS REMOVED AND PERMANENT REPAIR WAS FABRICATED AND INSTALLED IAW EWO ATI 57-080. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.Apr 6, 2006 · N823BX · Doug DC871FSDR IXXA06RNG040SSkin · bulgedDURING ROUTINE C CHECK, FOUND DENTED AND BULGING SKIN ON INBOARD FLAP UPPER SKIN TRAILING EDGE SKIN BETWEEN STATIONS XW 91.6564 TO 84.534 – RIGHT. DAMAGED SECTION SKIN WAS REMOVED. REPAIR SPLICE WAS MANUFACTURED AND NEW SKIN SECTION WAS FABRICATED AND INSTALApr 6, 2006 · N823BX · Doug DC871FSDR QXEA200601059Skin · chafedYYC - C4 LEFT INBOARD FLAP UPPER SKIN HAS CHAFED MARK. REPAIRED IAW DHC-8-200 RD 8-57-1023 AND DHC-8-200 AMM 20-30-11.Apr 6, 2006 · N353PH · Dhav DHC8202SDR 06FDEA1319Repair · misinstalledPREVIOUS REPAIR INSTALLED ON LT ELEVATOR STA 604/ER26 UPPER SURFACE T/E WEDGE UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION. NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. EVALUATED AND FOUND NOT TO CONFORMApr 6, 2006 · N426FE · Airbus A310203SDR F3LA200600016Skin · damagedDURING C-3 CHECK, INSPECTION REPORTED RT WING OTBD FLAP L/E BETWEEN NR 3 AND 4 FAIRINGS DAMAGED. CUT OUT DAMAGED SKIN PER SRM 57-53-00, PAGE 213. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 57-53-00 AND EA A9-57R-11353.Apr 5, 2006 · N908FR · Airbus A319111
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