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 2005UALA00219Panel · damagedLEFT WING OUTBOARD T/E AFT FLAP PANEL 588JT HAS ELONGATED HOLE. DAMAGE OCCURED DURING MAINTENANCE. REPAIRED PER EA 747-5753-13-A1252.Mar 7, 2005 · N117UA · Boeing 747422SDR SWAA050694Flap · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.Mar 7, 2005 · N317WN · Boeing 7373Q8SDR SWAA050693Flap · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.Mar 7, 2005 · N317WN · Boeing 7373Q8SDR IXXA0500138SPanel · dentedDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP AFT PANEL DENT DAMAGE BETWEEN STA XF 304.000-XF 333.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED PLATING. FABRICATED NEW PLATING, CLEANED, TREATED AND PRIMED AREA + INNER FACE ON NEW PLATINMar 4, 2005 · N821BX · Doug DC871FSDR DL76K050150Hinge · fracturedON WALKAROUND FOUND LEFT INBOARD FLAP NOT FAIRED WITH WING. FOUND LEFT INBOARD FLAP HINGE ASSEMBLY BROKEN. REPLACED HINGE ASSEMBLY AND CARRIAGE RODS PER MM.Mar 4, 2005 · N176DZ · Boeing 767332SDR QXEA200500521Skin · chafedYYC - RIGHT HAND FLAP LOWER SURFACE INBOARD HINGE AREA HAS CHAFED MARKS FROM FAIRING. REPAIRED IAW CRJ700 SRM 57-52-01-101-001-A01, SRM 51-25-01-001-001-A01.Mar 3, 2005 · N605QX · Cndair CL6002C10SDR QXEA200500520Skin · damagedYYC - RIGHT HAND INBOARD FLAP LOWER SURFACE HAS GRAVEL DAMAGED. REPAIRED IAW CRJ700 SRM 57-52-01-101-001-A01, SRM 51-12-00-001-001-A01, AND SRM 51-25-16-001-001-A01.Mar 3, 2005 · N605QX · Cndair CL6002C10SDR SWAA050655Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING, T/E OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT FLAP PER MM.Mar 3, 2005 · N683SW · Boeing 7373G7SDR 05FDEA00352Skin · chafedLT INBOARD FLAP LOWER SKIN, INBOARD END AFT SECTION IS CHAFED. COMPLIED WITH EA 8-5710-83979 WINGS - LT INBOARD FLAP, LOWER SKIN REPLACEMENT- REPAIR.Mar 3, 2005 · N361FE · Doug MD1010FSDR 05FDEA00347Panel · delaminatedRIGHT OUTBOARD FLAP PANEL 635 HL HAS LARGE AREA OF DELAMINATION. REPAIRED IAW EA 8-5710-83085, COVER ASSY ACCESS, LOWER INBOARD FLAP, REPAIR. REFERENCE NON-ROUTINE N01042.Mar 3, 2005 · N361FE · Doug MD1010FSDR QXEA200500522Vane · chafedYYC - RIGHT HAND INBOARD FLAP VANE INBOARD LEADING EDGE PANEL 684ET HAS CHAFED MARK. REPAIRED IAW CRJ700 SRM 57-52-02-101-001-A01 AND SRM 51-12-00-001-001-A01.Mar 2, 2005 · N605QX · Cndair CL6002C10SDR QXEA200500474Vane · chafedYYC - LEFT HAND WING INBOARD FLAP VANE HAS CHAFFED MARK AT LEADING EDGE MID SECTION. REPAIRED IAW CRJ700 SRM 57-52-02-101-001-A01 AND SRM 51-25-01-001-001-A01.Mar 2, 2005 · N605QX · Cndair CL6002C10SDR QXEA200500471Skin · damagedYYC - LEFT HAND INBOARD FLAP LOWER SURFACE HAS GRAVEL DAMAGE. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, SRM 51-25-01-001-001-A01, AND SRM 57-52-01-101-001-A01.Mar 2, 2005 · N605QX · Cndair CL6002C10SDR QXEA200500473Vane · chafedYYC - LEFT HAND WING INBOARD FLAP VANE, INBOARD LEADING EDGE PANEL 584ET HAS CHAFED MARK. REPAIRED IAW CRJ700 SRM 57-52-02-101-001-A01 AND SRM 51-25-01-001-001-A01.Mar 2, 2005 · N605QX · Cndair CL6002C10SDR QXEA200500461Vane · chafedYYC - RIGHT HAND INBOARD FLAP VANE LEADING EDGE HAS CHAFE MARK AT WS 88. REPAIRED IAW CRJ700 SRM 57-53-02-101-001-A01 AND SRM 51-25-01-001-001-A01.Mar 2, 2005 · N605QX · Cndair CL6002C10SDR 05FDEA00335Skin · gougedLT IB MID FLAP UPPER SURFACE IS GOUGED AT OB END 13 INCHES FROM LE. BLENDED GOUGE ON LT IB MIDFLAP OB END PER FEDEX EA 7-5710-86252Mar 2, 2005 · N481FE · Boeing 727227SDR ASAA0580160Skin · dentedHV - CHECK - RT IB FLAP BOTTOM SKIN DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (K)Mar 1, 2005 · N965AS · Doug DC983SDR ASAA0580158Vane · chafedHV-CHECK - LT OB FLAP NR 1 VANE IB END L/E SKIN IS CHAFED. INSTALLED REPAIR DOUBLER. (K)Mar 1, 2005 · N965AS · Doug DC983SDR SWAA050635Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND DELAMINATION ON RT WING T/E OUTBOARD AFT FLAP. REMOVED AND REPLACED RT WING T/E OUTBOARD AFT FLAP PER MM.Mar 1, 2005 · N386SW · Boeing 7373H4SDR 05FDEA00322Skin · damagedRIGHT OUTBOARD FLAP WEDGE TOP SKIN STATION XFO 560 TO 575 HAS 3 EACH PREVIOUS REPAIRS WITH TEMPORARY FASTENERS. REMOVED DAMAGED SKIN IAW DC10 SRM 51-35-01 VOL II, FABRICATED NEW SKIN IAW DAC DWG NR ARC1953. INSTALLED SKIN IAW DC 10 SRM 51-35-01 VIL II AND FEMar 1, 2005 · N361FE · Doug MD1010FSDR ASAA0580155Vane · chafedC-CHECK, RT WING OB FLAP VANE CHAFED BEHIND IB HINGE FAIRING. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)Feb 28, 2005 · N975AS · Doug DC983SDR ASAA0580173Vane · damagedHV - CHECK - FRAME HAS RIVET SET MARKS. REMOVED DAMAGED SECTION. INSTALED REPAIR FILLER, ANGLE, AND PLATE. (K)Feb 28, 2005 · N965AS · Doug DC983SDR ASAA0580156Vane · dentedC-CHECK - RT WING IB FLAP VANE DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)Feb 28, 2005 · N975AS · Doug DC983SDR QXEA200500481Access Panel · chafedYYC - RIGHT HAND INBOARD FLAP LOWER ACCESS PANEL 684BB HAS CHAFFED MARK FROM HINGE FAIRING. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01 AND SRM 57-52-01-101-001-A01.Feb 28, 2005 · N605QX · Cndair CL6002C10SDR GTIA050055Skin · dentedLT WING FLAP VANE NR 4 HAS DENT TOP SIDE. REMOVED DAMAGED SKIN AND CORE. FABRICATED NEW CORE AND DOUBLER, TREATED DOUBLER AND BONDED CORE IAW 57-50. (K)Feb 27, 2005 · N804NK · Doug DC982SDR DL76L050131Support Beam · corrodedCOMPLIED WITH REPAIR NR 1 OF ERA 089397-14MA REV C ON LEFT INBOARD FLAP DUE TO CORROSION IN ATTACH FASTENER HOLES.Feb 24, 2005 · N179DN · Boeing 767332SDR DL76L050128Support Beam · corrodedCORROSION FOUND IN ATTACH POINTS FOR INBOARD FLAP (NR 3), C/W ERA 089397-14MA SUBMITTED MRR PER REQUIREMENTS OF THIS ERA.Feb 24, 2005 · N179DN · Boeing 767332SDR SWAA050555Skin · delaminatedDURING SHOP VISIT, FOUND LT T/E AFT INBD FLAP UPPER SKIN DELAMINATED. REPAIRED SPARE FLAP PER SWA EA.Feb 23, 2005 · Boeing 737SDR MALA050228Panel · chafedDURING 4Y/2Y CHECK IN BNA FOUND I/B UPPER SURFACE OF LT FLAP ON ACCESS PANEL S41AT IS CHAFED OUT OF LIMITS. DAMAGE IS ACCEPTABLE IAW MESABA EOS57082.Feb 23, 2005 · N423XJ · Saab 340BSDR UIEA200500010Flap · damagedDURING WALK AROUND, MAINTENANCE FOUND DAMAGED TO LEFT OUTBOARD MIDFLAP T/E. REMOVED AND REPLACED LEFT OUTBOARD MIDFLAP IAW TASK CARD 27-51-04-404-025 REV 17 OCT 2003 S/N OFF, 000484. (M)Feb 22, 2005 · N493MC · Boeing 74747UFSDR IXXA0500141SRepair · unknownDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP UPPER FORWARD PLATING INTERIM REPAIR STA XF 417.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGE FROM AREA. PERFORMED A NDT INSPECTION TO AREA AND FABRICATED A REPAIR DOUBLER AND Feb 19, 2005 · N821BX · Doug DC871FSDR UPS05844017Web · crackedINSPECTION TYPE: C1, VERTICAL WEB CRACKED IN LT FLAP COVE FWD OF, AND BELOW XW3 FLAP HINGE FITTING. STOP DRILLED CRACK. NDT VERIFIED. FAB REPAIR DOUBLER FROM SHT7075T6-.071. TREAT, PRIME, INSTALL REPAIR REF DWG5643117, NDT/SPM06-10-01.001, SRM 53-2-0 FIG 1Feb 19, 2005 · N805UP · Doug DC873FSDR SWAA050492Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING FLAP PER MM.Feb 19, 2005 · N619SW · Boeing 7373H4SDR GTIA050068Wedge · damagedLT WING, IB FLAP, OB T/E WEDGE HAS TEMPORARY REPAIR LOWER SIDE IB. REMOVED TEMP REPAIR, REMOVED DAMAGED AREA (2 INCH DIA) FABRICATE DOUBLER AND FILLER, TREATED, PRIMED DOUBLER AND FILLER. INSTALLED REPAIRED DOUBLER AND FILLER IAW SRM. (K)Feb 18, 2005 · N804NK · Doug DC982SDR DHL2005764500Skin · debondedRT INBOARD MID FLAP UPPER SKIN TO T/E WBL 200 PREVIOUS FIBERGLASS REPAIR BECOME DISBONDED (PEELING OFF). REMOVED TWO EACH PREVIOUS FIBERGLASS REPAIRS & CLEANED AREA FOR NEW REPAIR IAW B727 SRM 51-40-20 FIG 30. FABRICATED TWO EACH SKIN REPLACEMENTS APPROX 4 XFeb 18, 2005 · N764AT · Boeing 727264SDR DHL2005781546Frame · crackedDURING A C-CHECK, RIGHT O/B MID FLAP LWR INTERNAL FRAME CRACKED AT WS 520. REMOVED ANGLE SUPPORT INTERNAL FRAME IAW B727 SRM 51-30-2. REMOVED RIGHT O/B MIDFLAP O/B FLAP ACTUATING MECHANISM CABLE (AFA) TO FACILITATE S/M REPAIR PSC B727 M/M 27-51-71. REMOVED Feb 16, 2005 · N781DH · Boeing 727227SDR A6WA200540070Guide · wornLEFT OUTBOARD FLAP MID BUTTE DOOR ROLLER GUIDE IS WORN, WS 235.843. S/D - REPAIRED LEFT OUTBOARD FLAP MID BUTE DOOR ROLLER GUIDE IAW BOMBARDIER INC REO 601R-57-53-019 REV NC.(M)Feb 16, 2005 · N421ZW · Cndair CL6002B19SDR GTIA050066Skin · damagedRT WING OB FLAP MID FIXED VANE DAMAGED. REMOVED DAMAGED SKIN AND CORE TO OB FLAP VANE, FABRICATED REPAIR DOUBLER AND HONEYCOMB CORE. TREATED METAL, BONDED CORE AND DOUBLER. INSTALLED REPAIRED CORE AND SKIN IAW SRM. (K)Feb 15, 2005 · N804NK · Doug DC982SDR ASAA0580109Skin · gougedOKC C-CHECK - LT WING T/E FLAP SKIN GOUGED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (K)Feb 15, 2005 · N943AS · Doug DC983SDR DHL2005781538Skin · gougedDURING A C-CHECK, LT WING I/B FORE FLAP GOUGED AT O/B LEADING EDGE. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. FAB DOUBLER FORM 2029-T3 .063 PO 9001634 BY 4.95 X 3.1 IAW B727 SRM 57-50-4 FIG 1. TREAT AND PRIME DOUBLER AREA IAW B727 SRM 51-10-2. INSTALL Feb 15, 2005 · N781DH · Boeing 727227SDR DHL2005781512Skin · gougedDURING A"C" CHECK, LEFT O/B FOREFLAP I/B UPPER L/E GOUGED. REMOVED PREV REPAIR LEFT O/B FOREFLAP I/B UPPER LT IAW B727 SRM 51-30-2. FABRICATE DOUBLER METAL IS 2024-T3 .063 5.0 BY 4.75 PO 9001634 IAW B727 SRM 57-50-2 FIG 4 57-50-4M FIG 1. TREAT PRIME AREA DOFeb 15, 2005 · N781DH · Boeing 727227SDR DHL2005781511Skin · gougedDURING A "C" CHECK, LT WING INBD FOREFLAP GOUGED ABOVE NR 3 FLAP CARRIAGE (MARKED). REMOVED PREV REPAIR ON L/WING I/B FOREFLAP IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER FROM 2024-T3 .063 IS 8.2 BY 6.4 PO 9001634 IAW B727 SRM 57-50-4 FIG 1 57-50-2 FIG 3Feb 15, 2005 · N781DH · Boeing 727227SDR SWAA050429Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP, DELAMINATED. REMOVED AND REPLACED LT WING T/E AFT FLAP PER MM.Feb 15, 2005 · N309SW · Boeing 7373H4SDR IXXA0500132SSkin · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP UPPER FORWARD PLATING INTERIM REPAIR STA XF 227.00. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED PLATING AREA. PERFORMED AN NDT INSPECTION. FABRICATED NEW PLATING SEGMENT, INTERNAL SPLICE AND Feb 14, 2005 · N821BX · Doug DC871FSDR DHL2005781544Skin · delaminatedDURING A C-CHECK, RT WING I/B MID FLAP O/B END, TRAILING EDGE IS DELAMINATED WBL 2400. REMOVED RT WING I/B MID FLAP O/B FAIRING. CUT OUT DELAM UPPER SURFACE SKIN AREA AFT APPROX 8 X 4.25 INCH. FABRICATED ONE SKIN REPLACEMENT APPROX 8 X 4.25 INCH & ONE SPLICFeb 14, 2005 · N781DH · Boeing 727227SDR AWXA200500321Skin · delaminatedMCN - MAJOR REPAIR - DURING C-14 CHECK FOUND THE UPPER RT OUTBOARD FORE FLAP DELAMINATED 92 INCHES FROM THE INBOARD END BETWEEN WBL 294.19 AND WBL 295.19. MAINTENANCE REMOVED DAMAGE ON UPPER SKIN OF RT OUTBOARD FORE FLAP FROM WBL 294.19 TO WBL 295.19; FABRICAFeb 14, 2005 · N307AW · Boeing 7373G7SDR DHL2005781509Skin · delaminatedDURING A "C" CHECK, RT WING OUTBD MID FLAP INBD END IS DELAMINATED AT TRAILING EDGE, WBL 300. REMOVED RT O/B MID FLAP I/B FAIRING TO F.D.M IAW B727 SRM 51-30-2. CUT OUT DELAM AREA UPPER SKIN AT T/E APPROX 7 INCH BY 3 1/2 INCH IAW B727 SRM 51-40-20 FIG 30. Feb 14, 2005 · N781DH · Boeing 727227SDR A6WA200540058Skin · dentedRIGHT INBOARD FLAP OUTBOARD LOWER CORNER HAS A DENT .5 INCH BY 3 INCHES BY .080 INCHES. S/D REMOVED DAMAGED SECTION OF SKIN, FABRICATED REPAIR PARTS FROM 2024.T3.050, (WVAX PO NR 40777) 2024-T3.063 (WVAC PO NR 36153) AND 2024-T3.012 (WVAC PO NR 24116). INSTAFeb 14, 2005 · N421ZW · Cndair CL6002B19SDR SWAA050424Flap · delaminatedDURING SCHEDULED 1/2D CHECK, FOUND LT WING OUTBOARD FOREFLAP DELAMINATED. REPAIRED FOREFLAP PER SRM.Feb 14, 2005 · N502SW · Boeing 7375H4SDR QXEA200500288Vane · wornRT WING FLAP VANE PANEL 684ET IS WORN. REPAIRED IAW CRJ700 SRM 57-52-02-101-001-A01, 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-01-001-001-A01.Feb 11, 2005 · N609QX · Cndair CL6002C10
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