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 A6WA201040949Fitting · chafedRT OTBD FLAP INBD ROLLER GUIDE FITTING CHAFED. BLENDED OUT DAMAGE IAW SRM 51-12-00, EDDY CURRENT INSPECTION IAW NDTM 51-20-06. ROTO PEEN REWORKED AREA SRM 51-24-11.Oct 29, 2010 · N448AW · Cndair CL6002B19SDR A6WA201040951Fitting · chafedRT OTBD FLAP INBD ROLLER FITTING BENEATH ROLLER CHAFED. BLENDED OUT CHAFED AREA IAW SRM 51-12-00, EDDY CURRENT INSPECT IAW NDTM 51-20-06, ROTOPEEN IAW SRM 51-24-11.Oct 29, 2010 · N448AW · Cndair CL6002B19SDR A6WA201040944Fitting · chafedLT OTBD FLAP INBD ROLLER FITTING BENEATH ROLLER IS CHAFED. BLENDED OUT DAMAGE TO A SMOOTH CONTOUR IAW SRM 51-12-00, EDDY CURRENT INSPECTED IAW 51-20-06 SHOT PEEN IAW SRM 51-24-11. RESTORED PROCTINO FINISH IAW SRM 51-21-16.Oct 29, 2010 · N448AW · Cndair CL6002B19SDR IPXA10B63543Fairing · chafedINSPECTION TYPE:C, LT WING OTBD FORE FLAP L/E FAIRING OTBD AREA HOLE CHAFED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5D, FIG 6, REV 57 121, CELSIUS DEGREE.Oct 29, 2010 · N581UP · Boeing 7474R7FSDR A6WA201040946Skin · chafedLT INBD FLAP VANE L/E INBD CTR AND OTBD CHAFED. REPAIR LT INBD FLAP VANE SKIN AT FLAP STA 137.012 AND BETWEEN FLAP STA 98.509 AND 108.135 IAW REO 601R-57-52-004, REV C. R & R LT INBD FLAP VANE INBD L/E SIN IAW SRM 51-42-13.Oct 28, 2010 · N448AW · Cndair CL6002B19SDR A6WA201040809Skin · chafedRT INBD FLAP, FLAP VANE SKIN L/E CHAFED AT INBD CTR OTBD ENDS BLENDED CTR AND OTBD LOCATIONS ARE WITHIN LIMITS, INBD VANE L/E LOCATION REPLACED L/E SKIN COMPLETING WORK IAW REO 601R-57-52-004, REV C, SRM 51-42-13.Oct 28, 2010 · N448AW · Cndair CL6002B19SDR SWAA106736Wedge · puncturedDURING SCHEDULED 14Y CHECK, FOUND LT WING I/B MID FLAP T/E WEDGE PUNCTURED AT LOWER SURFACE I/B END. REPAIRED MID FLAP PER MM.Oct 28, 2010 · N638SW · Boeing 7373H4SDR DHLA201000145Rib · crackedLT INBD FLAP.- RIB CRACKED AND WITH IMPROPER REPAIR, STA XW 125.000. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 2, SHEET 4, ITEM "Q". REMOVED DAMAGED RIB IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA + NEW RIB IAOct 27, 2010 · N801DH · Doug DC873FSDR A6WA201040857Vane · chafedLT INBD FLAP VANE HAS CHAFING DAMAGE ON L/E IN 3 PLACES. REPAIRED CHAFE DAMAGE ON LT INBD FLAP VANE L/E IAW REO 601R-57-52-004.Oct 27, 2010 · N453AW · Cndair CL6002B19SDR WX0A070648Vane · gougedRIGHT WING OUTBOARD FLAP INBOARD VANE LEADING EDGE IS GOUGED IN 2 PLACES. REPAIRED RIGHT WING O/B FLAP I/B VANE IAW MD80 SRM 57-03 PG 27.Oct 27, 2010 · N865GA · Doug MD83SDR REXA201000224Skin · damagedLEFT OUTBOARD FLAP VANE HAD WEAR DAMAGE OUTBOARD OF THE WF = 282.5 FLAP HINGE ARM. THE DAMAGE WAS THE RESULT OF AN INCORRECT LENGTH FASTENER INSTALLED IN THE WING TRAILING EDGE STRUCTURE. THE FLAP VANE LEADING EDGE DAMAGE MEASURES 0.65 INCHES LONG BY 0.25 INOct 27, 2010 · N8416B · Cndair CL6002B19SDR FOTR2016910867Skin · corrodedLEFT WING O/B FLAP UPPER SURFACE XW 138-342 IS CORRODED. REPAIRED ON NR 10867 FASI W/O 20169.Oct 27, 2010 · N831US · Doug MD83SDR FOTR2016910869Skin · corrodedLEFT WING OUTBOARD FORE FLAP LOWER SURFACE HAS SURFACE CORROSION IN SEVERAL SPOTS XW 138-342.Oct 27, 2010 · N831US · Doug MD83SDR DHLA201000146Vane · delaminatedNR 2 RT FLAP VANE DELAMINATED. R & R NEW FLAP VANE NR2 RT IAW MM 27-51-14, PG 201-203. REFER TO NR 239348 FOR OPS CHECK.Oct 26, 2010 · N801DH · Doug DC873FSDR CA101118006Bracket · broken(CAN) WHILE THE A/C WAS DOWN FOR SCHEDULED MAINTENANCE, THE GUYS FOUND A BROKEN LOWER FLAP MOTOR BRACKET SUPPORT DURING PHASE 5 INSPECTION, THIS WAS FOUND VISUALLY. THE SUPPORT P/N IS 2611144-5. THERE WERE NO ISSUES WITH THE OPERATION OF THE FLAPS, NO BINDINOct 25, 2010 · Cessna 208BSDR A6WA201040950Plate · chafedRT INBD FLAP INBD OF LUG PLATE HAS CHAFE DAMAGE WS 80.50. REPAIRED IAW REO 601R-57-52-1536, TYPE I.Oct 25, 2010 · N448AW · Cndair CL6002B19SDR A6WA201040945Plate · chafedLT INBD FLAP INBD AFT LUG PLATE HAS CHAFE DAMAGE WS 80.50. REPAIRED IAW REO 601R-57-52-1536, TYPE I.Oct 25, 2010 · N448AW · Cndair CL6002B19SDR SWAA106693Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Oct 25, 2010 · N698SW · Boeing 737317SDR FDEA201010244160Structure · crackedLEFT WING, I/B FLAP, MID FLAP T/E LWR CHORD HAS A CRACK , O/B OF NO. 4 FLAP TRACK. REMOVED CRACKED T/E LOWER CHORD SECTION DIM 69 1/2" IN LENGTH IAW SRM 51-30-2 LOCATED AND DRILLED NEW CHORD SECTION FROM BAC1503-100046 7075 T6 DIM 69 1/2" IN LENGTH IAW SROct 24, 2010 · N467FE · Boeing 727225SDR A6WA201040862Fitting · chafedLT OTBD FLAP ALIGNMENT GUIDE ROLLER FITTING HAS CHAFING DAMAGE BLENDED OUT CHAFED DAMAGE IAW B/A REO 601R-57-53-835 AND SRM 51-12-00.Oct 23, 2010 · N453AW · Cndair CL6002B19SDR AALA20101023TUL03Skin · corrodedCORROSION ON OUTBOARD FLAP LOWER LEADING EDGE INBOARD OF NUMBER 8 FLAP TRACK. INSTALLED FLUSH DOUBLER AND FILLER PER SRM 57-53-01 2R3.Oct 23, 2010 · N645AA · Boeing 757223SDR DALA1124893356Flap Track · corrodedDURING HCK INSPECTIONS PER AA 2754-01029, CORROSION WAS FOUND COMMON TO THE R/W NR 4 FLAP TRACK AFT LINK. BUSHING FABRICATED AND INSTALLED AS PER PRI 484977-14 REV 1. ACCOMPLISH ER/A 484977-14 REV 0 SECTION II AT EVERY KCK INTERVAL TO ACCOMPLISH ER/A 484977-Oct 22, 2010 · N856NW · Airbus A330223SDR DALA1124733356Flap Track · corrodedDURING HCK AND INSPECTIONS PER AA 2754-01029, CORROSION WAS FOUND COMMON TO THE R/W NR 4 FLAP TRACK AFT LINK. THE CORROSION WAS REWORKED PER SECTION I OF ER/A 484977-14. BUSHING FABRICATED AND INSTALLED AS PER PRI 484977-14 REV 1 ACCOMPLISH ER/A 484977-14 REOct 22, 2010 · N856NW · Airbus A330223SDR SPAA1000009Structure · crackedRT OTBD MIDFLAP INBD THRUST BEARING BORE HAS CRACK AT 3 O'CLOCK POSITION. REPLACED FLAP WITH O/H SERVICEABLE UNIT IAW AMM.Oct 22, 2010 · N712S · Boeing 7372Y5SDR UIEA201000236Skin · damagedDURING WALK-AROUND , MX FOUND DAMAGE TO THE RT WING OTBD FORE AND AFT FLAPS (REF FIG 1-3).DIMENSIONS AND DETAILS: RT OTBD FORE FLAP WBL793 - L/E PUNCTURE - 2.250 IN. X 2.0 IN. (REF FIG 1). RT OTBD FORE FLAP WBL810 - L/E PUNCTURE - 5.0 IN. X 2.5 IN. (REF FIG 2)Oct 22, 2010 · N499MC · Boeing 74747UFSDR FDEA201010214133Skin · dentedPREVIOUS REPAIRED DENTS NOT LISTED IN THE MCMRT AT RT FLAP INBD LOWER SKIN. DENT 1 - BTW RIB 5 & RIB 6 AND BTW FRONT SPAR & STRINGER 9. DENT 2 AND DENT 3 - BTW RIB 10 & RIB 11 AND STRINGER 11 & REAR SPAR. REPAIR OF THE DENTS IAW EA 6-5710-50143.Oct 21, 2010 · N456FE · Airbus A310SDR SWAA106559Sleeve · crackedDURING SCHEDULED MV2 CHECK, FOUND RT WING O/B MID FLAP NR 8 SPINDLE BEARING SLEEVE CRACKED. REMOVED AND REPLACED MIDFLAP PER MM.Oct 21, 2010 · N609SW · Boeing 7373H4SDR SWAA106543Flap · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING O/B FORE FLAP O/B LEADING EDGE DELAMINATED. REPAIRED FORE FLAP PER SRM.Oct 21, 2010 · N352SW · Boeing 7373H4SDR DALA1033829853Support Angle · crackedDURING M-CHECK FOUND RIGHT WING FLAP IN SIDE ACCESS HOLE I/B SIDE OF NR 4 FLAP HINGE SUPPORT ANGLE IS CRACKED 2 EA PLACES AT UPPER ATTACH BOLTS. REMOVED AND INSTALLED NEW FORMER IAW DC-9 SRM 51-30-02.Oct 20, 2010 · N762NC · Doug DC951SDR AALA20101020TUL03Skin · damagedLEFT INBOARD FLAP UPPER SKIN HAS HOLE WORN THROUGH BONDED REPAIR DOUBLER APPROXIMATELY 18 INCHES FROM OUTBOARD END OF FLAP. LEFT INBOARD FLAP REMOVED DAMAGED SKIN AND INSTALLED BONDED DOUBLER REPAIR PER SRM 51-70-10-2R.Oct 20, 2010 · N904AN · Boeing 737823SDR SPAA1000008Structure · corrodedLT OTBD MIDFLAP THRUST BEARING BORES (2 EA) CORRODED. REPLACED MIDFLAP WITH O/H UNIT IAW AMM.Oct 19, 2010 · N703S · Boeing 7372T4SDR SPAA1000007Structure · corrodedRT WING MIDFLAP HAS CORRODED THRUST BEARING BORES, 2 EA REPLACED MIDFLAP WITH SERVICEABLE UNIT IAW AMM.Oct 19, 2010 · N703S · Boeing 7372T4SDR FDEA201010194110Skin · crackedPOSSIBLE CRACK OR DEBONDED L/E INBD FOREFLAP LT WING AT NR4 FLAP ASSY ATTACHMENT. CUTOUT DAMAGE DIM: 1" X 1" AND FABRICATED DOUBLER DIM: 5" X 5 1/4" AND INSTALLED DOUBLER IAW SRM 57-50-4 FIG 1, SRM 51-10-2, SRM 51-30-2, AND NDTM 51-00-00.Oct 19, 2010 · N490FE · Boeing 727227SDR SWAA106471Skin · delaminatedDURING SCHEDULED MV2 CHECK, FOUND RT WING O/B AFT FLAP LOWER SURFACE DELAMINATED. REPAIRED AFT FLAP PER SRM.Oct 19, 2010 · N643SW · Boeing 7373H4SDR SWAA106453Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING I/B AFT FLAP LOWER SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Oct 19, 2010 · N396SW · Boeing 7373H4SDR IPXA0163584Skin · damagedINSPECTION TYPE:10YR, REPAIR SURVEY SEQUENCE NR137-W3-05 DOES NOT CORRELATE TO SRM AT LT INBD FLAP LWR SKIN, RIB 22A TO 20D STR 2.6 TO STR 2.7. ACCOMPLISHED REPAIR ON LT INBD FLAP LWR SKIN IAW EO A300-5750-40510-A AND STA EA 300-5750-01-A2792 IR.Oct 18, 2010 · N137UP · Airbus A300F4622RSDR IPXA10B63270Fairing · delaminatedINSPECTION TYPE:C2, LT WING OTBD FORE FLAP OTBD L/E FAIRING DELAMINATION COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5.A, FIG 5, REV 57.Oct 18, 2010 · N572UP · Boeing 74744AFSDR SWAA106436Skin · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.Oct 18, 2010 · N639SW · Boeing 7373H4SDR UIEA201000234Skin · damagedDURING A3 CHECK INSP OF ACFT, MX FOUND 4 EA CHAFE MARKS ON THE RT INBD AFT FLAP UPPER EXTERNAL SKIN CAUSED BY BOTTOM OF SCREWS THAT SECURE AFT SECTION OF COVE PANEL. AFTER BLENDOUT AREAS 1-4 FOUND BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 57-53-01, FIG 101, DETAIOct 18, 2010 · N498MC · Boeing 74747UFSDR IPXA10663210Skin · damagedRT OTBD FLAP T/E WEDGE SKIN DAMAGED. REPAIRED IAW EO B767-5750-39284-B.Oct 18, 2010 · N313UP · Boeing 76734AFSDR SWAA106394Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND RT WING AFT FLAP T/E DELAMINATED. REPAIRED AFT FLAP PER SRM.Oct 16, 2010 · N345SA · Boeing 7373K2SDR FDEA201010154096Rib · crackedRIB CRACKED LT WING IB FOREFLAP REMOVED LH IB FORE FLAP OB END RIB IAW SRM 51-30-2 AND FABRICATED NEW RIB FROM 2024O .040 HEAT TREATED TO T4 CONDITION DIM: 7" X 5 1/2" IAW ER 2-37153-801 REV A AND SRM 51-20-1 AND SRM 57-50-2 FIG 5. INSTALLED NEW RIB LT IB Oct 15, 2010 · N490FE · Boeing 727227SDR AALA20101015TUL02Skin · damagedRIGHT WING INBOARD TRAILING EDGE FLAP LOWER SURFACE HAS SMALL DENT AND GOUGE LOCATED 3 FEET OUTBOARD OF WING ROOT IN CENTER OF FLAP, ALSO .75 INCH GOUGE AND SCRATCH WITHIN SRM LIMITS LOCATED 3 FEET OUTBOARD OF WING ROOT. RIGHT WING INBOARD TRAILING EDGE FLAP Oct 15, 2010 · N595AA · Doug DC983SDR SWAA106341Flap · delaminatedDURING SCHEDULED 14Y CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.Oct 14, 2010 · N639SW · Boeing 7373H4SDR SWAA106330Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING FORE FLAP LOWER SKIN I/B DELAMINATED. REPAIRED FORE FLAP PER SRM.Oct 14, 2010 · N602SW · Boeing 7373H4SDR SWAA106316Flap · puncturedDURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP PUNCTURED. REPAIRED FORE FLAP PER SRM.Oct 14, 2010 · N338SW · Boeing 7373H4SDR IPXA0M63592Vane · damagedINSPECTION TYPE:4C, RT OTBD FLAP OTBD VANE HAS DAMAGE AT OTBD END. REPAIRED VANE IAW STA-SA EA 011-5750-01-A2757 I/R AND EO MD11-5750-40466-A.Oct 13, 2010 · N284UP · Doug MD11FSDR IPXA0M63587Skin · dentedINSPECTION TYPE:4C, DENT ON LOWER SURFACE OF RT INBD FLAP LOWER SURFACE, 13.25" FROM DENT TO OTBD FLAP HINGE FAIRING AND 41.5" FROM DENT TO T/E. CUT OUT DAMAGED AREA ON RT INBD FLAP LOWER SKIN BETWEEN STA XIFH 249-2 55. FABRICATED 1EA EXTERNAL DOUBLER AND INSOct 13, 2010 · N284UP · Doug MD11FSDR SWAA106262Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Oct 13, 2010 · N328SW · Boeing 7373H4SDR IPXA10163563Skin · damagedINSPECTION TYPE:10YR, LT CTR FLAP L/E BETWEEN FLAP TRACKS 3 AND 4 RIB 12 AND 16 HAS A EXTERNAL REPAIR DOUBLER THAT DOES NOT CORRELATE TO THE SRM REPAIR SURVEY ACCOMPLISHED REPAIR ON LT CTR FLAP L/E RIB 12 AND RIB 16 IAW SRM 57-50-00 PARA 4H FIG 208.Oct 12, 2010 · N137UP · Airbus A300F4622R
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