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 IXXA20150115007Channel · corrodedLOWER PANEL DIAGONAL ATTACH CHANNEL INBD OF H BLOCK AT WS 289 SPLIT ON EDGE. R & R IAW SRM 51-40-02.Sep 30, 2014 · N761CX · Boeing 767223 · Wing Miscellaneous StructureSDR IXXA20150115010Structure · corrodedPANEL 661AB REAR SPAR TO TE ATTACH RIB LOWER CHORD SPLIT ON EDGE WS 435. LOWER CHORD R & R IAW SRM 51-40-02.Sep 24, 2014 · N761CX · Boeing 767223 · Wing Miscellaneous StructureSDR IXXA201405140080Cable · defectiveNUMBER 2 DESCENT DEVICE CABLE IS EXTENDED, NEEDS REPLACED. IAW MM 25-61-03 R & R NR 2 EMERGENCY DESCENT DEVICE, NO DEFECTS NOTED.May 10, 2014 · N761CX · Boeing 767223 · Emergency EquipmentSDR IXXA2014041100060Battery Pack · dischargedAT SERVICE CHECK RT SIDE EMERGENCY EXIT LIGHT INOPERABLE. R & R EMERGENCY BATTERY PACK AT M736. OPERATIONAL CHECK SATISFACTORY IAW MM SUPP 33-51-00.Apr 9, 2014 · N761CX · Boeing 767223 · Emergency LightingSDR IXXA201401300040Power Supply · inoperativeLEFT FWD CABIN ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. EMERGENCY LIGHT POWER SUPPLY M735 AT FAULT, ACFT WAS GNDED.Jan 27, 2014 · N761CX · Boeing 767223 · Emergency LightingSDR IXXA20130901031ODuct · damagedDURING CLIMB RECEIVED EICAS MESSAGE RT BLEED DUCT LEAK AND APPROXIMATELY ONE MINUTE LATER RT AC BUSS POWER FAILURE. BUSS OFF LIGHT ILLUMINATED. RETURNED TO ORIGINATING STATION. INSPECTION FOUND RIGHT BLEED CROSSOVER DUCT RUPTURED. RIGHT HAND ISOLATION VALVESep 1, 2013 · N761CX · Boeing 767223 · Pneumatic Distribution SystemSDR IXXA2013041500005Tee Fitting · corrodedLEFT T-FITTING IS CORRODED AT LOWER FASTENER HOLE COMMON TO FAILSAFE STRAP. INSTALLED NEW T-FITTING IAW SRM 51-40-05.Feb 28, 2013 · N761CX · Boeing 767223 · Fuselage Main, Attach FittingsSDR IXXA2013041500004Skin · corrodedAFTER THE FAIL SAFE TRIM OUT PROCEDURE, THE INTERNAL SURFACE OF THE RT SIDE FUSELAGE SKIN WAS FOUND TO BE CORRODED AT FAILSAFE TRIM OUT AREA. THE CORROSION WAS REMOVED, AREAS SPOT FACED AND FILLERS INSTALLED IAW ENGINEERING DOCUMENT 47008ORD10. REF SB767-53AFeb 28, 2013 · N761CX · Boeing 767223 · Fuselage Main, Plate/SkinSDR IXXA2013041500002Failsafe · crackedRIGHT FAILSAFE STRAP HAS A 0.450" CRACKED AT THE LOWER HOLE IN INSPECTION AREA. THE CRACK WAS REMOVED DURING THE FAILSAFE TRIM OUT PROCEDURE THAT WAS PERFORMED IAW AMES ENGINEERING DOCUMENT 47008ORD04. REF SB 767-53A0100, REV 3, DATED FEB 06, 2012 AND SB 76Feb 28, 2013 · N761CX · Boeing 767223 · Fuselage Main, StructureSDR IXXA2013041200007Pressure Deck · corrodedRIGHT PRESSURE DECK WEB IS CORRODED AND HAS PREVIOUS DRILL STARTS. FABRICATED REPAIR WEB IAW DWG 145T8752 AND INSTALLED WEB IAW ENGINEERING DOCUMENT 47008ORD04.Feb 28, 2013 · N761CX · Boeing 767223 · Fuselage Main, BulkheadSDR IXXA2013041200006Tee Fitting · corrodedRT TEE FITTING IS CORRODED AT LOWER FASTENER HOLE COMMON TO FAILSAFE STRAP. R & R WITH NEW TEE FITTING IAW SRM 51-40-05.Feb 28, 2013 · N761CX · Boeing 767223 · Fuselage Main, Attach FittingsSDR IXXA130311ILN012SFloorbeam · corrodedAFT LOWER CARGO FLOOR FRAME IS CORRODED AT STATION 1197, RBL 20. R & R CORRODED SECTION OF FLOORBEAM INNER CHORD IAW SRM 51-40-02.Feb 28, 2013 · N761CX · Boeing 767223 · Fuselage Main, Floor BeamSDR IXXA201304120001Floorbeam · corrodedAFT LOWER CARGO FLOORBEAM IS CORRODED AT BS 1153, LBL 6 TO LBL 44. R & R CORRODED SECTION OF FLOORBEAM INNER CHORD IAW SRM 51-40-02.Feb 28, 2013 · N761CX · Boeing 767223 · Fuselage Main, Floor BeamSDR IXXA2013041200003Floorbeam · crackedFLOORBEAM WEB IS DENTED WITH A 1.1250" CRACK AT RBL 30 STA 303. REMOVED DAMAGED SECTION OF FLOORBEAM AND REPAIRED IAW SRM 51-70-11, FIG 1.Feb 28, 2013 · N761CX · Boeing 767223 · Fuselage Main, Floor BeamSDR IXXA201304120002Channel · crackedNR 1 PYLON INBD CHANNEL ABOVE ARROWHEAD PANEL HAS A 2.00" CRACK. REPLACED INBD CHANNEL ON NR 1 PYLON IAW SRM 57-40-02.Feb 28, 2013 · N761CX · Boeing 767223 · Nacelle/Pylon Miscellaneous StructureSDR IXXA2013041200001Support Angle · crackedFUSELAGE TO VERTICLE WEB SUPPORT ANGLE HAS A 1.00" CRACK AT STATION 1746 ON THE LT AND RT ENDS OF THE ANGLE. COMMON TO PANELS 324AR AND 324AL. REPLACED FUSELAGE TO VERTICLE WEB SUPPORT ANGLE IAW SRM 51-40-02, 51-21-04, AND 51-21-10.Feb 28, 2013 · N761CX · Boeing 767223 · Fuselage Miscellaneous StructureSDR IXXA130311ILN007SSkin · corrodedUPPER SKIN OF RT HORIZONTAL STAB IS CORRODED IN 3 PLACES FWD OF OTBD ELEVATOR. REPAIRED RT HORIZONTAL STAB AT STA 258-270, STA 288-300, STA 311-326 IAW SRM 55-10-01, FIG 201 REPAIR 7.Feb 28, 2013 · N761CX · Boeing 767223 · Horizontal Stabilizer, Plate/SkinSDR IXXA130311ILN004SSupport · corrodedLEFT WING T/E PANEL SUPPORT IS CORRODED BETWEEN WS 330 AND 355. REPAIRED PANEL SUPPORT BEAM IAW SRM 51-70-12.Feb 28, 2013 · N761CX · Boeing 767223 · Wing Miscellaneous StructureSDR IXXA2013041200002Support · corrodedLEFT WING T/E PANEL SUPPORT IS CORRODED AT WS 355. REPAIRED PANEL SUPPORT BEAM IAW SRM 51-70-12.Feb 28, 2013 · N761CX · Boeing 767223 · Wing Miscellaneous StructureSDR IXXA130311ILN002SStructure · corrodedAFT LOWER CARGO DOOR LINER HOLES CORRODED BELOW AFT CONTROL ARM ATTACHMENT POINT ON DOOR. REPLACED INNER TEE CHORD IAW SRM 51-40-02.Feb 28, 2013 · N761CX · Boeing 767223 · Cargo/Baggage DoorsSDR IXXA2013041200005Skin · corrodedRT WING INBD MAIN FLAP T/E UPPER SURFACE CORRODED. REPLACED INBD MAIN FLAP IAW AMM 27-51-03.Feb 26, 2013 · N761CX · Boeing 767223 · Trailing Edge FlapsSDR IXXA2013041200004Skin · corrodedRT WING INBD MAIN FLAP UPPER SKIN CORRODED AT WS 205. REPLACED INBD MAIN FLAP IAW AMM 27-51-03.Feb 26, 2013 · N761CX · Boeing 767223 · Trailing Edge FlapsSDR IXXA20121216036OComputer · failedFAULT CODE 34-45-XA-01/02, NAV DISPLAY "TCAS FAIL" WAS DISPLAYED ON BOTH CAPTAIN'S AND F/O DISPLAY. ACFT RETURNED TO STATION. R & R TCAS SYS COMPUTER IAW AMM 34-45-01. OPS CHECK GOOD ON GROUND.Dec 16, 2012 · N761CX · Boeing 767223 · Air Collision Avoidance SystemSDR IXXA20120816022OMec · inoperativeFAULT CODE 71-05-XG-01, LT ENGINE WOULD NOT SPOOL TO N1 COMMAND AT 70 PERCENT, AFTER ENGAGING N1, LARGE THROTTLE SPLIT. REJECTED TAKEOFF AT LOW SPEED, LESS THAN 40 KNOTS. NO BRAKING REQUIRED. COMPLIED WITH BORESCOPE INSPECTION IAW AMM 72-00-00/601 AND JOB Aug 16, 2012 · N761CX · Boeing 767223 · Fuel Controlling SystemSDR IXXA110075OGround Wire · damagedDURING CRUISE THE LT ENGINE OIL TEMP STEADILY CLIMB OUT OF LIMITS, OIL TEMP 190, AND OIL PRESSURE 58. THE CREW SHUTDOWN THE LT ENGINE AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX TROUBLESHOT THE OIL TEMP WIRING CIRCUIT AND FOUND PROTECTIVE COATING Nov 4, 2011 · N761CX · Boeing 767223 · Engine Oil System WiringSDR IXXA1100730Sensor · malfunctionedLT ENGINE SHUTDOWN IN-FLIGHT DUE TO HIGH OIL TEMP - ENGINE OIL TEMP INDICATED 175 DEGREES CELSIUS, OIL PRESSURE WAS 58 PSI. MX R & R NR 1 ENGINE OIL TEMP BULB IAW MM 79-34-00, BLOCK 1 AND 79-34-99, FIG 101, PG 101 & 102, STEPS 1 THRU 10. VERIFED, ACFT RELEANov 2, 2011 · N761CX · Boeing 767223 · Engine Oil TemperatureSDR IXXA11IAI001SStringer · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND STRINGER 1 LT CRACKED AT STA 676 - 698. REMOVED CRACKED STRINGER. INSTALLED NEW STRINGER SEGMENT IAW SRM 53-00-03, FIGURE 201.Jul 24, 2011 · N761CX · Boeing 767223 · Fuselage Main, Longeron/StringerSDR IXXA110047OCabin Pressure · inoperativeAFTER TAKEOFF, THE CREW PERFORMED A PACKS OFF TAKEOFF, THE AIR CONDITIONING PACKS WOULD NOT TURN ON AND THE ACFT WOULD NOT PRESSURIZE. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX ACCOMPLISHED FIM PROCEDURES 21-31-00, FIG 104 AND BIT STEPS 1, Jun 7, 2011 · N761CX · Boeing 767223 · Cabin Pressure Control SystemSDR IXXA110017SStructure · dentedDURING TOW INTO HANGER ACFT STRUCK WORK STAND AND DENTED L/E OF LT SIDE HORIZ STABILIZER. REPAIRED IAW SRM 51-70-10, FIG 209, REV ATI 03 AND MM 55-15-01.Jan 27, 2011 · N761CX · Boeing 767223 · Horizontal Stabilizer StructureSDR IXXA110016SStructure · dentedDURING TOW INTO HANGER ACFT STRUCK WORK STAND AND DENTED L/E OF RT SIDE HORIZ STABILIZER. REPAIRED IAW SRM 51-70-10, FIG 209, REV ATI 03 AND MM 55-15-01.Jan 27, 2011 · N761CX · Boeing 767223 · Horizontal Stabilizer StructureSDR IXXA110015SPan · corrodedDURING VISUAL INSP FOUND CORROSION IN AFT WASTE SERVICE PAN AREA AT STA 1582 STRINGER 39 LT AND 39 RT. REPAIR WAS ACCOMPLISHED IAW SRM 51-30-01, DWG 146T3248, SRM 51-40-02, SRM 53-00-03, MM 38-32-03-01 AND MM 05-51-24/201.Jan 26, 2011 · N761CX · Boeing 767223 · Fuselage Miscellaneous StructureSDR IXXA100050SIntercostal · brokenAFTER UNLOADING ACFT, FOUND PANEL BELOW LOCK/GUIDE TORN AND THE PANEL SUPPORT INTERCOSTAL BROKEN. REPLACED DAMAGED INTERCOSTAL AND WEB SECTION IAW SRM 767-200 51-10-02, 51-30-01, 51-70-13 AND 51-40-02 REV 2. AIRCRAFT WAS RETURNED TO SERVICE.Sep 25, 2010 · N761CX · Boeing 767223 · Fuselage Miscellaneous StructureSDR IXXA100007OSwitch · out of adjustDURING TAKEOFF FROM ELECTRONICS BAY ACCESS DOOR WARNING ILLUMINATED. THE CREW ABORTED TAKEOFF AND RETURNED TO BLOCKS. MX CLEANED AND ADJUSTED PROXIMITY SWITCH. OPS CHECK GOOD IAW BAMM 52-71-00/501. ACFT WAS RETURNED TO SERVICE.Jan 20, 2010 · N761CX · Boeing 767223 · Door Warning SystemSDR IXXA10WSAP072SKeelbeam · corrodedDURING ROUTINE C CHECK INSP FOUND LWR KEELBEAM CORRODED AT STA 1010. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-02 REV 101, 53-50-12 FIGURE 101 REV101, AND SOPM 20-10-03 REV 36.Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, KeelSDR IXXA10WSAP071SKeelbeam · corrodedDURING ROUTINE C-CHECK INSP FOUND LWR KEELBEAM CORRODED AT STA 990. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-02 REV 101, 53-50-12 FIGURE 101 REV101, AND SOPM 20-10-03 REV36.Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, KeelSDR IXXA10WSAP070SKeelbeam · corrodedDURING ROUTINE C CHECK INSP FOUND LWR KEELBEAM LT INBD FLANGE CORRODED AT STA 914. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-02 REV 101, 53-50-12 FIGURE 101 REV 101, AND SOPM 20-10-03 REV 36.Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, KeelSDR IXXA10WSAP080SKeelbeam · corrodedDURING ROUTINE C CHECK INSP FOUND LWR KEELBEAM LT INBD FLANGE CORRODED AT STA 889. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-02 REV 101, 53-50-12 FIGURE 101 REV101, AND SOPM 20-10-03 REV36.Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, KeelSDR IXXA10WSAP069SKeelbeam · corrodedDURING ROUTINE C CHECK INSP FOUND LWR KEELBEAM LT INBD FLANGE CORRODED AT STA 856. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-02 REV 101, 53-50-12 FIGURE 101 REV101, AND SOPM 20-10-03 REV36.Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, KeelSDR IXXA10WSAP068SSkin · dentedDURING ROUTINE C CHECK INSP FOUND DENTS IN RT VERTICAL STABILIZER BETWEEN STA FSS 245 AND FSS 92. 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 REDec 31, 2009 · N761CX · Boeing 767223 · Vertical Stabilizer, Plate/SkinSDR IXXA10WSAP067SKeelbeam · corrodedDURING ROUTINE C CHECK INSP FOUND LT LWR KEELBEAM INBD FLANGE CORRODED AT STA 844. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 767 51-10-01 REV101, 53-50-12-FIGURE 101 REV 101, AND SOPM 20-10-03 REV36.Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, KeelSDR IXXA10WSAP066SKeelbeam · corrodedDURING ROUTINE C CHECK INSP FOUND KEEL BEAM LT INBD FLANGE CORRODED BETWEEN STA 815-839. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. CLEANED, TREATED PRIMED IAW SRM 51-10-02 REV 101 , 53-50-12 FIGURE 101, REV 101, AND 20-10-13 REV36.Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, KeelSDR IXXA10WSAP065SSkin · gougedDURING ROUTINE C CHECK INSP FOUND GOUGES AT AFT END OF CARGO DOOR AT 28R. BLENDED OUT GOUGES. FOUND TO BE WITHIN LIMITS. PERFORMED NDT, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01, 53-00-01 FIGURE 101 REV 101, Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, Plate/SkinSDR IXXA10WSAP064SSkin · gougedDURING ROUTINE C CHECK INSP FOUND GOUGES AT LWR FWD CORNER IN FRONT OF AFT CARGO DOOR. BLENDED OUT GOUGES. FOUND TO BE WITHIN LIMITS. PERFORMED NDT, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01, 53-00-01 FIGURE Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, Plate/SkinSDR IXXA10WSAP063SSkin · dentedDURING ROUTINE C CHECK INSP, FOUND DENTS IN SKIN AT STA 1372 30R. 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 REV 101, 53-00-01 FIGURE 101 REVDec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, Plate/SkinSDR IXXA10WSAP062SSkin · gougedDURING ROUTINE C CHECK INSP FOUND GOUGES IN SKIN AT AFT CARGO DOOR AT 27R E58 3417771. BLENDED OUT GOUGES. 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, 52-3Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, Plate/SkinSDR IXXA10WSAP061SSkin · scratchedDURING ROUTINE C CHECK INSP FOUND SCRATCHES AT AFT CARGO DOOR AREA UPPER FWD CORNER AND UPPER AFT CORNER ON RT AFT FUSELAGE. BLENDED OUT SCRATCHES. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAIDec 31, 2009 · N761CX · Boeing 767223 · Cargo/Baggage DoorsSDR IXXA10WSAP060SSkin · dentedDURING ROUTINE C CHECK INSP FOUND NR 1 ENGINE OTBD PYLON DENTED JUST AFT OF HYD ACCESS DOOR. 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 REV101,Dec 31, 2009 · N761CX · Boeing 767223 · Nacelle/Pylon, Plate/SkinSDR IXXA10WSAP059SSill · dentedDURING ROUTINE C CHECK INSP FOUND BULK CARGO DOOR FWD SILL DENTED. REMOVED DAMAGED AREA. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01 REV101, 53-00-01 FIGURE Dec 31, 2009 · N761CX · Boeing 767223 · Cargo/Baggage DoorsSDR IXXA10WSAP058SSkin · scratchedDURING ROUTINE C-CHECK INSP, FOUND SCRATCHES ON AFT OF BULK CARGO DOOR AT STA 1461 BETWEEN STR 33 LT AND 39 LT. BLENDED SCRATCHES OUT. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-Dec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, Plate/SkinSDR IXXA10WSAP057SSkin · dentedDURING ROUTINE C-CHECK INSP FOUND DENT AFT EDGE OF BULK CARGO DOOR OPENING. 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, 53-00-01 FIGURDec 31, 2009 · N761CX · Boeing 767223 · Fuselage Main, Plate/Skin
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