N761CX

Service difficulty reports · 209

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N761CX' AND registry_match = 'registration'
  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 IXXA10WSAP056SSkin · gougedDURING ROUTINE C CHECK INSP FOUND GOUGE ON LWR FUSELAGE LT OF CTR LINE AT STATION 1619. BLENDED OUT GOUGE. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01, 53-00-01 FDec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, Plate/SkinSDR IXXA10WSAP055SSkin · dentedDURING ROUTINE C-CHECK INSP, FOUND DENTS ON L/E RT SIDE OF VERTICAL STABILIZER. BLENDED OUT DENTS. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01, 55-30-01 FIGURE 10Dec 31, 2009 · N761CX · Boeing 767223 · Vertical Stabilizer, Plate/SkinSDR IXXA10WSAP054SSkin · scratchedDURING ROUTINE C CHECK INSP FOUND SCRATCHES ON LT FUSELAGE AFT BODY FAIRING BY T/E. BLENDED OUT SCRATCHES. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01, 53-00-01 FIGURE101 REV 101, NDT D634T3Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, Plate/SkinSDR IXXA10WSAP053SSkin · gougedDURING ROUTINE C CHECK INSP, FOUND L/E SURFACE LT HORIZONTAL STABILIZER GOUGED 1’ FROM ROOT. BLENDED OUT GOUGE. PERFORMED NDT INSP, NO CRACK OR CORROSION NOTED. CLEANED, TREATED AND PRIMED IAW SRM 51-10-01, 51-20-01, 55-10-01 FIGURE 101 REV101 AND NDT 634T30Dec 31, 2009 · N761CX · Boeing 767223 · Horizontal Stabilizer, Plate/SkinSDR IXXA10WSAP052SPanel · scratchedDURING ROUTINE C CHECK INSP, FOUND SCRATCHES ON L/E OF LT STABILIZER. BLENDED OUT SCRATCHES. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01 REV 101, 55-10-01 FIGURE 1Dec 31, 2009 · N761CX · Boeing 767223 · Horizontal Stabilizer, Plate/SkinSDR IXXA10WSAP051SSkin · dentedDURING ROUTINE C CHECK INSP, FOUND A DENT 15 FWD OF AFT ACCESSORY DOOR AT STA 1788. BLENDED OUT DENT. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01 REV101, 5300-01 Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, Plate/SkinSDR IXXA10WSAP050SSkin · scratchedDURING ROUTINE C-CHECK INSP FOUND SCRATCHES ON FUSELAGE FWD AND BELOW FWD CARGO DOOR CONTROL. BLENDED OUT SCRATCHES. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, Plate/SkinSDR IXXA10WSAP049SSkin · scratchedDURING ROUTINE C-CHECK INSP, FOUND SCRATCHES BELOW FORWARD CARGO DOOR CONTROL PANEL. BLENDED OUT SCRATCHES. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 55-00-01 FIGURE 101 REV 101, Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, Plate/SkinSDR IXXA10WSAP048SDoor · dentedDURING ROUTINE C CHECK INSP, FOUND DENTS IN TAIL CONE ACCESS DOOR RT SIDE. REMOVED DENTS. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP. NO CRACK OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01 REV101, 52-40-01 FIGURE 101 REDec 31, 2009 · N761CX · Boeing 767223 · Tail Cone DoorsSDR IXXA10WSAP047SSkin · dentedDURING ROUTINE C-CHECK INSP FOUND DENTS IN UPPER AREA OF BULK CARGO DOOR. REMOVED DENTS. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP. NO CRACK OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01 REV101, 53-00-01 FIGURE 101 REDec 31, 2009 · N761CX · Boeing 767223 · Cargo/Baggage DoorsSDR IXXA10WSAP046SSkin · dentedDURING ROUTINE C-CHECK INSP, FOUND DENTS IN VERTICAL STABILIZER AT STA FSS118. REMOVED DENTS. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP. NO CRACK OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01REV 101, SRM 51-20-01 REV 101, 55-Dec 31, 2009 · N761CX · Boeing 767223 · Vertical Stabilizer, Plate/SkinSDR IXXA10WSAP045SKeelbeam · corrodedDURING ROUTINE C-CHECK INSP FOUND CORROSION ON LOWER KEELBEAM LT INBD FLANGE BETWEEN STA 801-803. REMOVED CORROSION. FOUND WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12 FIGURE 101 REV 101, 20-10-03 REV 036, AND 51-20-01 REV 101.Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, KeelSDR IXXA10WSAP044SKeelbeam · corrodedDURING ROUTINE C-CHECK INSP FOUND CORROSION ON LOWER KEELBEAM RT INBD FLANGE BETWEEN STA 905-925. REMOVED CORROSION. FOUND WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12, FIGURE 101, REV 101, 20-10-03 REV 036, AND 51-20-01 REV 101.Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, KeelSDR IXXA10WSAP043SKeelbeam · corrodedDURING ROUTINE C CHECK INSP FOUND CORROSION ON LOWER KEELBEAM RT INBD FLANGE BETWEEN STA 876-901. REMOVED CORROSION. FOUND WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12 FIGURE 101 REV 101, 20-10-03 REV 036, AND 51-20-01 REV 101.Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, KeelSDR IXXA10WSAP042SKeelbeam · corrodedDURING ROUTINE C CHECK INSP FOUND CORROSION ON LOWER KEELBEAM RT INBD FLANGE BETWEEN STA 843-854. REMOVED CORROSION. FOUND WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12 FIGURE 101 REV 101, 20-10-03 REV 036, AND 51-20-01 REV 101.Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, KeelSDR IXXA10WSAP041SKeelbeam · corrodedDURING ROUTINE C CHECK INSP FOUND CORROSION ON LOWER KEELBEAM RT INBD FLANGE BETWEEN STA 825-839. REMOVED CORROSION. FOUND WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW IAW SRM 53-50-12, FIGURE 101, REV 101, 20-10-03 REV 036, AND 51-20-01 REV 101.Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, KeelSDR IXXA10WSAP040SKeelbeam · corrodedDURING ROUTINE C CHECK INSP FOUND CORROSION ON LOWER KEELBEAM RT INBD FLANGE AT STA 808. REMOVED CORROSION. FOUND WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12 FIGURE 101 REV 101, 20-10-03 REV 036, AND 51-20-01 REV 101.Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, KeelSDR IXXA10WSAP038SKeelbeam · corrodedDURING ROUTINE C-CHECK INSP FOUND CORROSION ON LOWER KEELBEAM RT AT STA 975.5. REMOVED CORROSION. FOUND WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12 FIGURE 101, REV 101, 20-10-03 REV 036, AND 51-20-01 REV 101.Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, KeelSDR IXXA10WSAP037SKeelbeam · corrodedDURING ROUTINE C CHECK INSP FOUND CORROSION ON LOWER KEELBEAM RT AT STA 1003. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED KEELBEAM. PERFORMED NDT INSP. NO CRACK OR CORROSION. FABRICATED NEW KEELBEAM. ACCOMPLISHED HEAT TREATMENT TO REPAIR PART.Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, KeelSDR IXXA10WSAP036SPanel · damagedDURING ROUTINE C-CHECK INSP FOUND LT FUSELAGE BODY FAIRING PANEL NR 193PL EDGE DAMAGED. APPLIED GLASS CLOTH AND RESIN. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-70-06 REV 101 AND MM 51-21-10 REV 97.Dec 30, 2009 · N761CX · Boeing 767223 · Aerodynamic FairingsSDR IXXA10WSAP035SFloorboard · puncturedDURING ROUTINE C CHECK INSP FOUND FWD CARGO COMPARTMENT FLOORBOARD PUNCTURED AT STA 455 BOTTOM LINE 0. APPLIED GLASS CLOTH AND RESIN TO FILL PUNCTURE FLOOR. CLEANED, TREATED, PAINTED AREA IAW SRM 53-00-50 REV 101 AND 51-21-10 REV 97.Dec 30, 2009 · N761CX · Boeing 767223 · Fuselage Floor PanelSDR IXXA10WSAP034SPanel · erodedDURING ROUTINE C CHECK INSP FOUND LT HORIZ STABILIZER EXTERIOR UPPER SURFACE AFT STRIP PANEL NR 335UT ERODED. APPLIED RESIN FOR PROTECTION. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-70-06 REV 101 AND MM 51-21-10 REV 97.Dec 29, 2009 · N761CX · Boeing 767223 · Horizontal Stabilizer, Plate/SkinSDR IXXA10WSAP033SPanel · nickedDURING ROUTINE C-CHECK INSP FOUND NICKS ON LT HORIZONTAL STABILIZER REMOVABLE L/E NR 332DL. BLENDED OUT NICKS. PERFORMED NDT INSP. NO CRACKS INDICATED. CLEANED, TREATED, PRIMED PART IAW SRM 55-10-01 FIGURE 101 REV 101 AND NDT D634T301, REV 93, PART 6 51-00-19Dec 29, 2009 · N761CX · Boeing 767223 · Horizontal Stabilizer, Plate/SkinSDR IXXA10WSAP032SPanel · nickedDURING ROUTINE C CHECK INSPECTION FOUND NICKS ON LEFT HAND HORIZONTAL STABILIZER REMOVABLE LEADING EDGE NUMBER 332CL. BLENDED OUT NICKS. PERFORMED NDT INSPECTION. NO CRACKS INDICATED. CLEANED, TREATED, PRIMED PART IAW SRM 55-10-01 FIGURE 101, REV 101 AND NDT DDec 29, 2009 · N761CX · Boeing 767223 · Horizontal Stabilizer, Plate/SkinSDR IXXA10WSAP031SPanel · nickedDURING ROUTINE C-CHECK INSP FOUND NICKS ON LT HORIZONTAL STABILIZER REMOVABLE L/E NR 332BL. BLENDED OUT NICKS. PERFORMED NDT INSP. NO CRACKS INDICATED. CLEANED, TREATED, PRIMED PART IAW SRM 55-10-01 FIGURE 101, REV 101 AND NDT D634T301 REV 93, PART 6 51-00-1Dec 29, 2009 · N761CX · Boeing 767223 · Horizontal Stabilizer, Plate/SkinSDR IXXA10WSAP030SPanel · crackedDURING ROUTINE C-CHECK INSP, FOUND LT HORIZ STAB REMOVABLE L/E NR 332BL CRACKED. REMOVED CRACKED L/E PANEL. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK NOTED. FABRICATED REPAIR DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. INSTALLED REPAIR PADec 29, 2009 · N761CX · Boeing 767223 · Horizontal Stabilizer, Plate/SkinSDR IXXA10WSAP029SSkin · delaminatedDURING ROUTINE C-CHECK INSP, FOUND LT OTBD ELEVATOR UPPER SKIN AFT INBD SIDE HAS DELAMINATED. REMOVED DELAMINATED PART. APPLIED GRAPHITE FABRIC AND RESIN TO PART. CLEANED, TREATED, PRIMED AND PAINTED. ACCOMPLISHED WEIGHT AND BALANCE PROCEDURES IAW SRM 51-70-03Dec 29, 2009 · N761CX · Boeing 767223 · Elevator, Plate/SkinSDR IXXA10WSAP028SSkin · misrepairedDURING ROUTINE C-CHECK INSP FOUND IMPROPER REPAIR ON RT OTBD ELEVATOR UPPER SURFACE. REMOVED DAMAGED AREA. APPLIED RESIN. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-70-06 REV 101 AND 51-21-10 REV 97.Dec 29, 2009 · N761CX · Boeing 767223 · Elevator, Plate/SkinSDR IXXA10WSAP027SSkin · delaminatedDURING ROUTINE C CHECK INSP FOUND DELAMINATING ON VERTICAL STABILIZER RT SIDE SKIN. ACCOMPLISHED REPAIR IAW SRM 51-70-03 REV 101, SRM 51-21-10 REV 97.Dec 29, 2009 · N761CX · Boeing 767223 · Vertical Stabilizer, Plate/SkinSDR IXXA10WSAP026SPanel · erodedDURING ROUTINE C-CHECK INSP, FOUND VERTICAL STABILIZER L/E PANEL NR 321E ERODED. ACCOMPLISHED REPAIR IAW SRM 51-70-06 REV101 AND 51-20-10 REV 97.Dec 29, 2009 · N761CX · Boeing 767223 · Vertical Stabilizer, Plate/SkinSDR IXXA10WSAP025SKeelbeam · corrodedDURING ROUTINE C-CHECK INSP, FOUND CORROSION ON LOWER KEEL BEAM LT BETWEEN STA 982-993, STR 38. REMOVED CORROSION. FOUND TO BE WITHIN LIMIT’S. CLEAN, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12 FIGURE 101 REV 101, 20-10-03 REV 36, AND 51-20-01 REV101.Dec 29, 2009 · N761CX · Boeing 767223 · Fuselage Main, KeelSDR IXXA10WSAP024SKeelbeam · corrodedDURING ROUTINE C CHECK INSP FOUND CORROSION ON LOWER KEELBEAM RIGHT BETWEEN STA 925-936, STR 38. REMOVED CORROSION. FOUND TO BE WITHIN LIMIT’S. CLEAN, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12 FIGURE 101, REV 101, 20-10-03 REV 36, AND 51-20-01 REV101.Dec 29, 2009 · N761CX · Boeing 767223 · Fuselage Main, KeelSDR IXXA10WSAP023SKeelbeam · corrodedDURING ROUTINE C-CHECK INSP, FOUND CORROSION ON LOWER KEEL BEAM LT BETWEEN STATION 839-854 STR 38. REMOVED CORROSION. FOUND TO BE WITHIN LIMIT’S. CLEAN, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12 FIGURE 101 REV 101, 20-10-03 REV 36, AND 51-20-01 REV101.Dec 29, 2009 · N761CX · Boeing 767223 · Fuselage Main, KeelSDR IXXA10WSAP022SKeelbeam · corrodedDURING ROUTINE C CHECK INSP, FOUND CORROSION ON LWR KEELBEAM BETWEEN STATION 786 - 815 LT STRINGER 38. REMOVED CORROSION. FOUND TO BE WITHIN LIMIT’S. CLEAN, TREATED, PRIMED AND PAINTED IAW SRM 53-50-12 FIGURE 101 REV 101, 20-10-03 REV 36, AND 51-20-01 REV 101.Dec 29, 2009 · N761CX · Boeing 767223 · Fuselage Main, KeelSDR IXXA10WSAP021SFrame · crackedDURING ROUTINE C-CHECK INSP FOUND NR 2 PYLON V-FAIRING 447DB FWD EDGE INBD ATTACH SUPPORT FRAME CRACKED. REMOVED FASTENER’S AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED FRAME. INSTALLED EXISTING FASTENER’S AND NEW FRAME IAW AMM 20-11-00 REV97, SRM 51-40-02 Dec 28, 2009 · N761CX · Boeing 767223 · Nacelle/Pylon, Frame/Spar/RibSDR IXXA10WSAP020SChannel · crackedDURING ROUTINE C-CHECK INSP FOUND NR 2 PYLON V-FAIRING 447DB FWD EDGE OTBD ATTACH SUPPORT CHANNEL CRACKED. REMOVED FASTENER’S AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED CHANNEL. INSTALLED NEW FASTENER’S AND CHANNEL IAW SRM 51-40-02 REV101 AND SRM 54-40-05Dec 28, 2009 · N761CX · Boeing 767223 · Nacelle/Pylon Miscellaneous StructureSDR IXXA10WSAP019SChannel · crackedDURING ROUTINE C-CHECK INSP FOUND NR 2 PYLON V-FAIRING 447DB FWD EDGE INBD ATTACH SUPPORT CHANNEL CRACKED. REMOVED FASTENER’S AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED CHANNEL. INSTALLED NEW FASTENER’S AND CHANNEL IAW SRM 51-40-02 REV101 AND SRM 54-40-05Dec 28, 2009 · N761CX · Boeing 767223 · Nacelle/Pylon Miscellaneous StructureSDR IXXA10WSAP018SFairing · delaminatedDURING ROUTINE C-CHECK INSP FOUND NR 2 PYLON V-FAIRING 447DB FWD AREA DELAMINATED. ACCOMPLISHED REPAIR IAW SRM 51-70-17, REV 101 AND SRM 51-21-10, REV 101.Dec 28, 2009 · N761CX · Boeing 767223 · Nacelle/Pylon, Main FrameSDR IXXA10WSAP017SPanel · corrodedDURING ROUTINE C-CHECK INSP FOUND CORROSION ON NR 2 PYLON PANEL 447CR. REMOVED CORROSION. FOUND TO BE WITHIN LIMIT’S. CLEANED, TREATED, PRIMED AND PAINTED AREA IAW SRM 51-10-02 REV 101, SRM 54-51-70 FIGURE 101 REV 101, AND SRM 51-20-01 REV 101.Dec 28, 2009 · N761CX · Boeing 767223 · Nacelle/Pylon, Plate/SkinSDR IXXA10WSAP016SFrame · corrodedDURING ROUTINE C-CHECK INSP FOUND CORROSION ON RT WING LOWER SURFACE L/E PANEL 621AFB SUPPORT FRAME AT STATION LES1076. REMOVED FASTENER’S AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND TO BE WITHIN LIMIT’S. CLEANED, TREATED, PRIMED AND PAINTED AREA. Dec 28, 2009 · N761CX · Boeing 767223 · Wing SparSDR IXXA10WSAP015SFrame · corrodedDURING ROUTINE C-CHECK INSP FOUND CORROSION ON RT WING LOWER SURFACE L/E PANEL 621AFB SUPPORT FRAME AT STATION LES1070. REMOVED FASTENER’S AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND TO BE WITHIN LIMIT’S. CLEANED, TREATED, PRIMED AND PAINTED AREA.Dec 28, 2009 · N761CX · Boeing 767223 · Wing SparSDR IXXA10WSAP014SFairing · delaminatedDURING ROUTINE C-CHECK INSP FOUND LT WING INBD T/E FLAP OTBD FLAP SUPPORT FAIRING FWD FAIRING ERODED. ACCOMPLISHED REPAIR IAW SRM 51-70-06 REV 101 AND MM 51-20-10 REV 97.Dec 28, 2009 · N761CX · Boeing 767223 · Trailing Edge FlapsSDR IXXA10WSAP013SFairing · delaminatedDURING ROUTINE C-CHECK INSP FOUND RT WING INBD FLAP OTBD AFT FLAP SUPPORT FAIRING DELAMINATED. ACCOMPLISHED REPAIR IAW SRM 51-70-17 REV 101 AND MM 51-20-10 REV 97.Dec 28, 2009 · N761CX · Boeing 767223 · Trailing Edge FlapsSDR IXXA10WSAP012SPanel · crackedDURING ROUTINE C-CHECK INSP FOUND RT WING T/E PANEL NR 651WB CRACKED. ACCOMPLISHED REPAIR IAW MM 20-11-00 REV 79, AND SRM 51-70-06 REV 101, 51-21-10 REV 97, 51-40-05 REV 101.Dec 28, 2009 · N761CX · Boeing 767223 · Wing, Plate/SkinSDR IXXA10WSAP011SSkin · scratchedDURING ROUTINE C-CHECK INSP FOUND SCRATCH MARKS ON FUSELAGE SKIN BETWEEN STATIONS 1241, 1263 AND STRINGER 25-26. REMOVED SCRATCH MARK’S. FOUND TO BE WITHIN LIMIT’S. PERFORMED NDT INSP. NO CRACK’S OR CORROSION. CLEANED, TREATED, PRIMED AND PAINTED AREA IAW SRDec 28, 2009 · N761CX · Boeing 767223 · Fuselage Main, Plate/SkinSDR IXXA10WSAP010SStructure · corrodedDURING ROUTINE C-CHECK INSP FOUND CORROSION ON LOWER DRAIN VALVE SURROUNDING STRUCTURE AT STATION 1542. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED AREA IAW SRM 53-00-01 FIGURE 101 REV 101, AND SRM 51-20-01 REV 101.Dec 28, 2009 · N761CX · Boeing 767223 · Fuselage Main, StructureSDR IXXA10WSAP009SFloor Panel · puncturedDURING ROUTINE C-CHECK INSP, FOUND FLOOR PANEL PUNCTURED IN AFT CARGO COMPARTMENT AT STA 1227, RT BOTTOM LINE 12. ACCOMPLISHED REPAIR IAW SRM 53-00-50 REV 101 AND MM 51-21-10 REV 97.Dec 28, 2009 · N761CX · Boeing 767223 · Fuselage Floor PanelSDR IXXA10WSAP008SFloor Panel · puncturedDURING ROUTINE C-CHECK INSP FOUND FLOOR PANEL PUNCTURED IN AFT CARGO COMPARTMENT AT STA 1272 LT BOTTOM LINE 12. ACCOMPLISHED REPAIR IAW SRM 53-00-50 REV 101 AND MM 51-21-10 REV 97.Dec 28, 2009 · N761CX · Boeing 767223 · Fuselage Floor PanelSDR IXXA10WSAP007SFairing · corrodedDURING ROUTINE C-CHECK INSP FOUND CORROSION ON NR 1 PYLON LT AND RT UPPER HINGE FAIRING SUPPORT. REMOVED CORROSION. FOUND TO BE WITHIN LIMIT’S. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-10-02 REV 101, AND SRM 51-20-01 REV 101.Dec 27, 2009 · N761CX · Boeing 767223 · Nacelle/Pylon Miscellaneous StructureSDR IXXA10WSAP006SFairing · delaminatedDURING ROUTINE C-CHECK INSP FOUND RT WING OTBD FLAP SUPPORT FAIRING DELAMINATED. ACCOMPLISHED REPAIR IAW SRM 51-70-17 REV 101 AND 51-21-10 REV 97.Dec 27, 2009 · N761CX · Boeing 767223 · Trailing Edge Flaps
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