# Service difficulty reports: N61CX, cancelled Jan 25, 2018 A list on [N61CX, cancelled Jan 25, 2018](https://openairdocs.org/deregistered/N61CX-2018-01-25.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR IXXA0000039](https://openairdocs.org/sdr/IXXA0000039.md): Compressor · failed · Oct 31, 2000 · N61CX · Doug DC862 · Cabin Compressor System > EN ROUTE FROM NBW TO NGU, SMOKE WAS EMITTED INTO THE COCKPIT WHEN THE NUMBER THREE TURBO COMPRESSOR WAS OPERATED. THE FLIGHT CREW SECURED THE COMPRESSOR, SMOKE SUBSIDED. THE FLIGHT CONTINUED TO NGU FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE TURBO - [SDR IXXA0000022](https://openairdocs.org/sdr/IXXA0000022.md): Fan · defective · Jun 23, 2000 · N61CX · Doug DC862 · Air Distribution Fan > EN ROUTE FROM EDI TO TOL, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT WHEN THE LEFT RECIRULATION FAN WAS TURNED ON. THE FLIGHT CREW SECURED THE FAN, THE ODOR SUBSIDED AND THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE THE - [SDR IXXA0000010](https://openairdocs.org/sdr/IXXA0000010.md): Wire · broken · Feb 25, 2000 · N61CX · Doug DC862 · Landing Gear System Wiring > TOL - FLT 1837 - EN ROUTE FROM AUS TO TOL, AFTER LANDING GEAR RETRACTION, THE GEAR UNSAFE WARNING LIGHT ILLUMINATED. THE CREW CYCLED THE LANDING GEAR TO EXTINGUISH THE WARNING LIGHT. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECT - [SDR IXXA9900026](https://openairdocs.org/sdr/IXXA9900026.md): Unknown · odor · Oct 21, 1999 · N61CX · Doug DC862 · Air Distribution System > EN ROUTE FROM AVB TO RMS, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT WHEN THE OVER HEAD FLORESENT LIGHTING SYSTEM WAS ILLUMINATED. THE CREW TURNED THE LIGHTS OFF AND THE ODOR SUBSIDED, THE FLIGHT CONTINUED TO RMS FOR AN UNEVENTFUL LANDING. MAINTENANCE INS - [SDR IXXA9900009](https://openairdocs.org/sdr/IXXA9900009.md): Uplatch · lack of lube · May 4, 1999 · N61CX · Doug DC862 · Landing Gear Retraction/Extension System > AFTER TAKEOFF FROM AVB EN ROUTE TO FRA, WHEN THE LANDING GEAR WAS RETRACTED THE MAIN GEAR DOOR NOT LATCHED LIGHT REMAINED ILLUMINATED. THE FLIGHT CREW CYCLED THE LANDING GEAR WITH THE WARNING INDICATION REMAINING THE SAME. THE FLIGHT CONTINUED TO FRA FOR AN - [SDR IXXA9800061](https://openairdocs.org/sdr/IXXA9800061.md): Retract Mech · malfunctioned · Jul 9, 1998 · N61CX · Doug DC862 · Landing Gear Door Retract Section > AFTER TAKEOFF FROM MSP, EN ROUTE TO TOL, WHEN THE GEAR WAS RETRACTED, THE FLIGHT CREW NOTICED A LOUD NOISE AND SLIGHT VIBRATION COMING FROM THE NOSE WHEEL WELL AREA. THE CREW PERFORMED A GEAR UPLATCH CHECK WHICH PASSED, THEN CYCLED THE GEAR. THE VIBRATION CO - [SDR IXXA9800055](https://openairdocs.org/sdr/IXXA9800055.md): Retract Mech · lack of lube · Jun 9, 1998 · N61CX · Doug DC862 · Landing Gear Door Retract Section > AFTER TAKEOFF WHEN THE GEAR WAS RETRACTED, THE FORWARD NOSE GEAR DOORS REMAINED OPEN. THE CREW CYCLED THE GEAR WITH NO HELP. THE FLIGHT CONTINUED TO TOL, MAKING AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE NOSE GEAR DOOR LATCH MECHANISMS, WITH NO DISCRE - [SDR IXXA9800029](https://openairdocs.org/sdr/IXXA9800029.md): Regulator Valve · defective · Mar 18, 1998 · N61CX · Doug DC862 · Pneumatic Distribution System > DURING CLIMBOUT, THE NUMBER ONE AND TWO ENGINE PNEUMATIC MANIFOLD OVER TEMPERATURE INDICATING LIGHTS ILLUMINATED, VERIFIED BY TEMPERATURE INDICATOR. THE FLIGHT ENGINEER SECURED THE NUMBER ONE AND TWO ENGINE BLEED SYSTEMS FOLLOWING COMPANY EMERGENCY PROCEDURES - [SDR IXXA9700168](https://openairdocs.org/sdr/IXXA9700168.md): Smoke Detector · dirty · Dec 10, 1997 · N61CX · Doug DC862 · Smoke Detection > EN ROUTE FROM EDDF TO OKBK, THE MAIN CARGO COMPART SMOKE DETECTION LIGHT ILLUMINATED ACCOMPANIED BY THE WARNING HORN. THE CREW SILENCED THE HORN AND THE A/C DIVERTED TO IST FOR AN UNEVENTFUL LANDING. THE CARGO WAS OFF LOADED AND INSPECTED WITH NO EVIDENCE O - [SDR IXXA9700166](https://openairdocs.org/sdr/IXXA9700166.md): Wire · chafed · Nov 16, 1997 · N61CX · Doug DC862 · Fire Detection > ON SHORT FINAL INBOUND EDDF FROM KWI, THE NUMBER 4 ENGINE FIRE BELL SOUNDED AND THE FIRE WARNING LIGHT ILLUMINATED. CAPTAIN RESET MASTER FIRE WARNING SWITCH WHICH SILENCED THE BELL. THE LIGHT REMAINED ILLUMINATED FOR 3 TO 4 SECONDS AND EXTINGUSHED. AN UNEVE - [SDR IXXA9700163](https://openairdocs.org/sdr/IXXA9700163.md): Control Cable · out of adj · Nov 11, 1997 · N61CX · Doug DC862 · Landing Gear Door Retract Section > AFTER TAKEOFF WHEN THE GEAR WAS RETRACTED, THE LANDING GEAR AND DOOR UNSAFE LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO KWI, MAKING AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE MAIN GEAR DOOR FOLLOW-UP CONTROL MECHANISM O - [SDR IXXA9700161](https://openairdocs.org/sdr/IXXA9700161.md): Control Cable · misrigged · Nov 9, 1997 · N61CX · Doug DC862 · Landing Gear Door Retract Section > AFTER TAKEOFF WHEN THE LANDING GEAR WAS RETRACTED, THE DOOR UNSAFE LIGHT REMAINED ILLUMINATED. THE CREW RECYCLED THE LANDING GEAR AND THE INDICATION REMAINED THE SAME. THE AIRCRAFT RETURNED TO FRA, MAKING AN UNEVENFUL LANDING. MAINTENANCE INSPECTED THE AIRC - [SDR IXXA9700083](https://openairdocs.org/sdr/IXXA9700083.md): Container · leaking · Jun 19, 1997 · N61CX · Doug DC862 · Cargo Compartments > SHORTLY AFTER TAKEOFF, CREW NOTICED FUMES ENTERING THE COCKPIT. FLIGHT ENGINEER WAS DISPATCHED TO INVESTIGATE MAIN CARGO DECK TO DETERMINE ORIGIN OF FUMES. THE FLIGHT ENGINEER CONFIRMED FUMES EMANATING FROM THE CARGO PALLET LOCATED IN THE NR 1 POSITION. CRE - [SDR IXXA9700014](https://openairdocs.org/sdr/IXXA9700014.md): Track Bearings · failed · Jan 30, 1997 · N61CX · Doug DC862 · Trailing Edge Flaps > ON LANDING ROLLOUT BGTL, WITH ALL ENGINES IN REVERSE, NR 2 ENGINE EPR DROPPED AND THE REVERSER LEVER MOVED FORWARD OUT OF REVERSE. ON INSPECTION, THE TRANSLATING RING OF THE REVERSER WAS FOUND TO BE MISSING AND TWO AREAS OF DAMAGE WERE NOTED AT THE INBOARD SE - [SDR IXXA96137](https://openairdocs.org/sdr/IXXA96137.md): Skin · corroded · Aug 6, 1996 · N61CX · Doug DC862 · Fuselage Main, Plate/Skin > DURING ROUTINE C-CHECK INSPECTION, THE EXTERNAL PLATING WAS FOUND TO BE CORRODED AT FUSELAGE STATION 1495 AND LONGERON 32 RIGHT. REPAIR OF THE PLATING WAS ACCOMPLISHED BY CUTTING OUT THE DAMAGED AREA, FABRICATING AND INSTALLING REPAIR FILLERS AND DOUBLERS IAW - [SDR IXXA96136](https://openairdocs.org/sdr/IXXA96136.md): Skin · corroded · Aug 6, 1996 · N61CX · Doug DC862 · Ailerons > DURING ROUTINE C-CHECK INSPECTION, THE LEFT OUTBOARD AILERON LOWER PLATING SURFACE WAS FOUND TO BE CORRODED BETWEEN STATIONS XW500 AND 577. THE PLATING WAS REPLACED IAW THE STRUCTURAL REPAIR MANUAL 51-1-21 AND FAA DER APPROVED SKETCH A89-R05. (M) - [SDR IXXA96135](https://openairdocs.org/sdr/IXXA96135.md): Spar · cracked · Aug 6, 1996 · N61CX · Doug DC862 · Wing Spar > WHILE ACCOMPLISHING THE REPLACEMENT OF THE RIGHT MAIN LANDING GEAR FITTING, THE RIGHT LOWER REAR SPAR WAS FOUND TO BE CRACKED BETWEEN WING STATION S XRS 13 AND XRS 20. THE REPAIR OF THE SPAR WAS ACCOMPLISHED IAW DOUGLAS DRAWINGS 5613917, 5613918, 5613919, 561 - [SDR IXXA96145](https://openairdocs.org/sdr/IXXA96145.md): Skin · cracked · Jul 23, 1996 · N61CX · Doug DC862 · Fuselage Main, Plate/Skin > DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE EXTERNAL FUSELAGE PLATING AT THE FORWARD UPPER CORNER OF THE FORWARD LOWER CARGO DOOR OPENING. THE CRACK WAS REMOVED BY CUTOUT, AND FABRICATION AND INSTALLATION OF A FILLER AND REPAIR DOUBLERS IAW TH - [SDR IXXA96144](https://openairdocs.org/sdr/IXXA96144.md): Plating · corroded · Jul 23, 1996 · N61CX · Doug DC862 · Ailerons > DURING ROUTINE C-CHECK INSPECTION, THE RIGHT OUTBOARD AILERON LOWER PLATING ON THE INBOARD SIDE WAS FOUND TO BE CORRODED. REPAIR TO THE AREA WAS ACCOMPLISHED IAW THE STRUCTURAL REPAIR MANUAL 57-10-0. (M) - [SDR IXXA96138](https://openairdocs.org/sdr/IXXA96138.md): Bus Links · cracked · Jul 23, 1996 · N61CX · Doug DC862 · Aileron Control System > DURING ROUTINE C-CHECK INSPECTION, THE RIGHT INBOARD AILERON, INBOARD BUS LINKS WERE FOUND TO BE CRACKED. THE BUS LINKS WERE REPLACED IAW THE DOUGLAS SRM AND MM. (M) - [SDR IXXA96146](https://openairdocs.org/sdr/IXXA96146.md): Plating · cracked · Jul 22, 1996 · N61CX · Doug DC862 · Fuselage Main, Plate/Skin > DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE EXTERNAL PLATING A FUSELAGE STATION 225 BETWEEN LONGERONS 29 AND 30 LEFT. THE CRACK WAS REPAIRED IAW THE STRUCTURAL REPAIR MANUAL. (M) - [SDR IXXA96143](https://openairdocs.org/sdr/IXXA96143.md): Plating · cracked · Jul 22, 1996 · N61CX · Doug DC862 · Wing, Plate/Skin > DURING ROUTINE C-CHECK INSPECTION, THE RIGHT WING LEADING EDGE PLATING WAS FOUND CRACKED AT THE INBOARD STUB WING, INBOARD END. THE CRACK WAS REPAIRED IAW THE DOUGLAS SRM 57-2-1. (M) - [SDR IXXA96142](https://openairdocs.org/sdr/IXXA96142.md): Fitting · cracked · Jul 22, 1996 · N61CX · Doug DC862 · Wing, Landing Gear Attach Fittings > DURING ROUTINE C-CHECK INSPECTION, THE RIGHT MAIN LANDING GEAR FITTING WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW THE DOUGLAS SRM AND FITTING REPLACEMENT GUIDE. (M) - [SDR IXXA96141](https://openairdocs.org/sdr/IXXA96141.md): Fitting · cracked · Jul 22, 1996 · N61CX · Doug DC862 · Wing Miscellaneous Structure > DURING ROUTINE C-CHECK INSPECTION, THE RIGHT MAIN LANDING GEAR TORQUE TUBE SUPPORT FITTING WAS FOUND TO BE CRACKED. THE FITTING WAS REPLACED IAW THE STRUCTURAL REPAIR MANUAL. (M) - [SDR IXXA96140](https://openairdocs.org/sdr/IXXA96140.md): Bulkhead · cracked · Jul 22, 1996 · N61CX · Doug DC862 · Fuselage Main, Bulkhead > DURING ROUTINE C-CHECK INSPECTION, THE PRESSURE BULKHEAD (CABLE FEED THROUGH) AT FUSELAGE STATION 680 WAS FOUND TO BE CRACKED AT LONGERON 27 LEFT. THE BULKHEAD WAS REPLACED IAW THE AIRCRAFT SRM. (M) - [SDR IXXA96139](https://openairdocs.org/sdr/IXXA96139.md): Longeron · cracked · Jul 22, 1996 · N61CX · Doug DC862 · Fuselage Main, Longeron/Stringer > DURING ROUTINE C-CHECK INSPECTION, THE LEFT LONGERON 24 WAS FOUND CRACKED IN THE WING ATTACH BOTTLE BOLT AREA. THE LONGERON WAS REPLACED IAW THE DOUGLAS REPLACEMENT GUIDE AND THE SRM. (M) - [SDR IXXA9648](https://openairdocs.org/sdr/IXXA9648.md): Turbocompressor · malfunctioned · Apr 14, 1996 · N61CX · Doug DC862 · Cabin Compressor System > RJTY/RJOI - EN ROUTE BETWEEN RJTY AND RJOI, NR 1 CABIN TURBOCOMPRESSOR BECAME NOISY AND PRODUCED AN OILY SMELL. THE NR 12 TC WAS SHUT OFF, AND WAS DEFERRED AT RJOI. THE NR 12 TC WAS SCHEDULED FOR REPLACEMENT DUE TO POSSIBLE BEARING/OIL SEAL FAILURE. (X) - [SDR IXXA9597](https://openairdocs.org/sdr/IXXA9597.md): Eel Wire · failed · Nov 20, 1995 · N61CX · Doug DC862 · Emergency Lighting > MAINTENANCE FOUND THE FOUR FORWARD FLOOR EMERGENCY TRACK LIGHTS TO BE INOPERATIVE. THE POWER SUPPLY PROVIDING POWER TO THESE LIGHTS WAS BLOWING PICOFUSES FOR THAT SET OF LIGHTS. TROUBLESHOOTING INDENTIFIED A SHORT IN THE POWER WIRE BETWEEN THE POWER SUPPLY A - [SDR IXXA199567](https://openairdocs.org/sdr/IXXA199567.md): Wire · failed · Jul 19, 1995 · N61CX · Doug DC862 · Landing Gear System Wiring > WSAP - ON DEPARTURE DURING UPLATCH CHECK, THE GEAR LIGHT STAYED ON WITH THE MAIN GEAR DOOR LIGHT OUT. THE LANDING GEAR WAS CYCLED ONCE, AND THE UPLATCH CHECK WAS SUCCESSFUL. INSPECTION OF THE SYSTEM IN RJTY REVEALED AN INTERMITTENT GROUND WIRE ON THE RT MLG - [SDR IXXA199562](https://openairdocs.org/sdr/IXXA199562.md): Uplock Assy · lack of lube · Jun 12, 1995 · N61CX · Doug DC862 · Landing Gear Door Retract Section > ON DEPARTURE OUT OF RJTY, THE UPLATCH CHECK WAS ACCOMPLISHED AND BOTH THE GEAR DOOR AND GEAR WARNING LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO RJTY FOR MAINTENANCE. MAINTENANCE JACKED THE AIRCRAFT, CLEANED AND LUBRICATED BOTH THE LANDING GEAR AND THE GEAR ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N61CX' AND deregistration_id = 'N61CX-2018-01-25' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N61CX-2018-01-25/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.