# N86: 1994 Canadair CL-600-2B16, registration cancelled 2025-12-24 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 24, 2025 - Status when cancelled: Valid registration - Airframe: [Canadair CL-600-2B16](https://openairdocs.org/model/canadair-cl-600-2b16) (registry code 1900305) - Engine: [GE CF34-3B](https://openairdocs.org/engine/ge-cf34-3b) (registry code 30069) - Data sheets: [TCDS A21EA](https://openairdocs.org/tcds/A21EA), [TCDS E15NE](https://openairdocs.org/tcds/E15NE) (OpenAirDocs) - Serial number: 5167 - Year built: 1994 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 27, 2009 - Certificate issued: December 1, 1998 - Last registry action: July 22, 2023 - Mode S code: ABCC7D - Owner when cancelled: [Federal Aviation Administration](https://openairdocs.org/faa-owner/FEDERAL%20AVIATION%20ADMINISTRATION) - Location: [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City) - Owner type: Government - Owner's area on the map: 35.3806° N, 97.6484° W: Placed by OpenAirDocs at the center of ZIP code 73169, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N86 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=86 - Page: https://openairdocs.org/deregistered/N86-2025-12-24 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Canadair CL-600-2B16: https://openairdocs.org/model/canadair-cl-600-2b16.md ## Service difficulty reports (22) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2022FA0000640](https://openairdocs.org/sdr/2022FA0000640), Oct 21, 2022: HOSE. RUPTURED. LOSS OF THE # 3 HYDRAULIC SYSTEM IN FLIGHT. EMERGENCY DECLARED AND LANDING GEAR WAS MANUALLY DEPLOYED. UPON INSPECTION, THE NLG DOOR ACTUATOR HOSE WAS FOUND TO - [SDR RU3A2021100100013](https://openairdocs.org/sdr/RU3A2021100100013), Jul 29, 2021: NONE. NONE. “FUSELAGE SKIN BUCKLED AFT OF NOSE LANDING FOLLOW UP DOOR” ON LOGBOOK PAGE 270398 DATED JULY 29, 2021 HOURS 14193.3 LANDINGS 5792 THE AIRCRAFT WAS FERRIED UP TO - [SDR RU3A2021030300004](https://openairdocs.org/sdr/RU3A2021030300004), Mar 3, 2021: WARNING LIGHT. ILLUMINATED. FLAPS FAIL LIGHT ILLUMINATED ON APPROUCH - [SDR RU3A201912065069](https://openairdocs.org/sdr/RU3A201912065069), Nov 22, 2019: SWITCH. OUT OF ADJUST. NOSE GEAR DID NOT RETRACT ON TAKEOFF. NOSE DOOR OPEN LIGHT REMAINED ILLUMINATED. ACCOMPLISHED GEAR DISAGREE CHECKLIST. MA ADJUSTED LH LANDING GEAR DOOR (NOSE) O - [SDR RU3A201912062068](https://openairdocs.org/sdr/RU3A201912062068), Nov 21, 2019: CONNECTOR. LOOSE. NOSE GEAR DID NOT RETRACT. DOOR LIGHT REMAINED ON. COMPLETED GEAR DISAGREE CHECKLIST. FOUND LOOSE BACKSHELL AND CANNON PLUG CONNECTION GOING TO NOSE LANDING GEA - [SDR RU3A2018092524045](https://openairdocs.org/sdr/RU3A2018092524045), Sep 24, 2018: SENSOR. FAILED. INBOARD ANTI-SKID FAIL ANNUNCIATOR ON. LT WHEEL SPEED SENSOR WAS REPLACED. OPERATIONAL CHECK SATISFACTORY. - [SDR RU3A2018092523044](https://openairdocs.org/sdr/RU3A2018092523044), Sep 23, 2018: MODULE. INTERMITTENT. OUTBOARD ANTI-SKID LIGHT ILLUMINATED WHEN GEAR EXTENDED WOULD NOT RESET. FOUND ANTI-SKID CONTROL PANEL LT LIGHT MODULE INTERMITTENT. THE ISSUE WAS RESOLVED BY R - [SDR RU3A20180529022](https://openairdocs.org/sdr/RU3A20180529022), May 22, 2018: ACCELEROMETER. FAULTY. RIGHT ENGINE VIBRATION LIGHT ILLUMINATED AT 75% N1 AT 16000 FEET. REMOVED AND REPLACED ENGINE VIBRATION ACCELEROMETER. - [SDR RU3A20180523019](https://openairdocs.org/sdr/RU3A20180523019), May 22, 2018: SIGNAL COND UNIT. MALFUNCTIONED. RT ENGINE VIBRATION LIGHT ILLUMINATED AT 75% N1 AT 16,000 FEET. REMOVED AND REPLACED ENGINE VIBRATION SIGNAL CONDITIONER. - [SDR RU3A20180312013](https://openairdocs.org/sdr/RU3A20180312013), Mar 12, 2018: CRANK ASSY. CRACKED. PASSENGER DOOR LATCH MECHANISM CRANK CRACKED. - [SDR RU3A2018031200001](https://openairdocs.org/sdr/RU3A2018031200001), Mar 12, 2018: CRANK ASSY. CRACKED. PASSENGER DOOR LATCH MECHANISM CRANK CRACKED. - [SDR RU3A20170810023](https://openairdocs.org/sdr/RU3A20170810023), Aug 10, 2017: LANDING GEAR. MALFUNCTIONED. LEFT MAIN LANDING GEAR UNSAFE AFTER LOWERING GEAR. PULLED MANUAL RELEASE WITH NO CHANGE IAW CHECKLIST. RESET MANUAL RELEASE PER SERVICE CENTER MX DIRECTION. GEA - [SDR RU3A20160513009](https://openairdocs.org/sdr/RU3A20160513009), May 13, 2016: SHUTOFF VALVE. MALFUNCTIONED. BLEED AIR FAIL LIGHT ILLUMINATED WHEN BLEED AIR IN CLOSED POSITION. REPLACEMENT OF THE PNEUMATIC SOV SOLVED THE ISSUE. NO FURTHER ACTION REQUIRED. - [SDR RU3A20150618014](https://openairdocs.org/sdr/RU3A20150618014), Jun 18, 2015: FLAP. LACK OF LUBE. FLAPS FAIL ON INITIAL TAKE OFF. FAILED AT 18^. AIRSPEED REACHED 240 KIAS WITH NO OVER SPEED WARNING. COMPLIED WITH OVER SPEED INSPECTION. LUBED FLAPS. - [SDR RU3A20131126014](https://openairdocs.org/sdr/RU3A20131126014), Nov 24, 2013: UNKNOWN. MALFUNCTIONED. AFTER TAKEOFF COULDN’T RAISE GEAR, THEN WOW INPUT LIGHT CAME ON. LIGHT WENT OUT AFTER 2 MIN. GEAR HANDLE REMAINED LOCKED DUE TO MOMENTARY WOW INPUT FAILURE, TRO - [SDR RU3A20130509008](https://openairdocs.org/sdr/RU3A20130509008), May 9, 2013: UNKNOWN. MALFUNCTIONED. UPON COMPLETION OF A LOW APPROACH, GEAR HANDLE SELECTED UP FOR CLIMBOUT. AFTER MAINS RETRACTED, NOSE GEAR REMAINED EXTENDED AND RED LIGHT IN HANDLE CONTINUED FL - [SDR RU3A20121211002](https://openairdocs.org/sdr/RU3A20121211002), Dec 11, 2012: WINDSHIELD. CRACKED. RIGHT SIDE WINDSHIELD ANTI-ICE FAILURE IN CRUISE FLIGHT. PERFORMED WINDSHIELD ANTI-ICE FAILURE AS DIRECTED IN ABNORMAL PROCEDURE. CONTINUED ON ORIGINAL ROUTE TO - [SDR RU3A1117](https://openairdocs.org/sdr/RU3A1117), Jul 21, 2011: HINGE FITTING. CRACKED. REMOVED RUDDER TO NDI ATTACH FITTINGS. DURING INSPECTION A CRACK IN UPPER FITTING WAS DETECTED. DURING STRIPPING OF PAINT, DISCOVERED PITTING AROUND BUSHING INS - [SDR RU3A1108](https://openairdocs.org/sdr/RU3A1108), Feb 11, 2011: DOWNLOCK SWITCH. FAULTY. WHILE MANEUVERING FOR APPROACH, CREW LOWERED LANDING GEAR. BOTH MAIN GEAR INDICATIONS WERE "DOWN AND LOCKED". NOSE INDICATOR DID NOT ILLUMINATE. NOSE DOOR OPEN - [SDR RU3A1021](https://openairdocs.org/sdr/RU3A1021), Nov 1, 2010: WARNING MESSAGE. FALSE ACTIVATION. ON DESCENT THRU 160 BOTH THROTTLES WERE BROUGHT TO IDLE. NR 2 LOW OIL PRESSURE LIGHT CAME ON, AND LOW OIL PRESSURE TAPE INDICATED LOW. N1 LT 65 PERCENT, RT 34 P - [SDR RU3A0923](https://openairdocs.org/sdr/RU3A0923), Dec 17, 2009: WINDSHIELD. CRACKED. IN CRUISE FLIGHT, LEFT PILOT WINDSHIELD CRACKED THE ENTIRE VERTICAL LENGTH OF THE WINDOW. PRESSURIZATION WAS CHECKED AND ABNORMAL CHECKLIST FOR WINDSHIELD OUTER - [SDR RU3A99001](https://openairdocs.org/sdr/RU3A99001), Jan 26, 1999: COVER. BROKEN. ANC - AIRPORT RAMP. AIRCRAFT OBSERVED TO BE LEAKING FUEL FROM THE LOWER TAIL SECTION WITHIN A FEW MINUTES FOLLOWING APU START. THE AIRCRAFT ENGINES WERE NOT STA ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20030710014649I](https://openairdocs.org/incident/20030710014649I), Jul 10, 2003: Cndair CL6002B16 (N86), Oklahoma City, OK. (-23) Right engine pylon over/heat light came on at ftl 290. Pilot reduced power by retarding power lever. The light went off and the pilot advanced power… - [Incident 20020424008159I](https://openairdocs.org/incident/20020424008159I), Apr 24, 2002: Cndair CL6002B16 (N86), Oklahoma City, OK. (-23) On takeoff, at gear retraction the out board anti skid light came on, and no anti skid master caution on gear extension. The anti skid out board fail… ## Other aircraft with N86 - [Cancelled 1992-09-11](https://openairdocs.org/deregistered/N86-1992-09-11): North American NA-265-40, S/N 28286. Owner: [Federal Aviation Administration](https://openairdocs.org/faa-owner/FEDERAL%20AVIATION%20ADMINISTRATION), [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City) - [Cancelled 1964-03-02](https://openairdocs.org/deregistered/N86-1964-03-02): Beech C-45F, S/N 5666, built 1944. Exported to Germany. Owner: Bremen - [Cancelled 1929-06-18](https://openairdocs.org/deregistered/N86-1929-06-18): Curtiss JN4D, S/N 4077. Owner: [Thompson Gilman](https://openairdocs.org/faa-owner/THOMPSON%20GILMAN), [Canton, SD](https://openairdocs.org/faa-place/SD/Canton) - [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N86-undated): Douglas C-48, S/N 3378. Owner: [Civil Aeronautics Administration](https://openairdocs.org/faa-owner/CIVIL%20AERONAUTICS%20ADMINISTRATION), [Anacostin, DC](https://openairdocs.org/faa-place/DC/Anacostin) --- 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.