# N87: 1995 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 series](https://openairdocs.org/engine/ge-cf34-series) (registry code 30015)
- Data sheets: [TCDS A21EA](https://openairdocs.org/tcds/A21EA) (OpenAirDocs)
- Serial number: 5190
- Year built: 1995
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 15, 1996
- Certificate issued: March 2, 1999
- Last registry action: September 9, 2023
- Mode S code: ABF3FC
- 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/N87
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=87
- Page: https://openairdocs.org/deregistered/N87-2025-12-24

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 (32)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR RU3A2021052101111](https://openairdocs.org/sdr/RU3A2021052101111), May 21, 2021: SELECTOR VALVE. FAULTED. GEAR FAILED TO RETRACT AFTER TAKEOFF. 'I/P WOW' LIGHT ILLUMINATED. REPLACED DOOR SELECTOR VALVE AND WEIGHT ON WHEELS HARNESS ON NOSE LANDING GEAR
- [SDR RU3A20200108001](https://openairdocs.org/sdr/RU3A20200108001), Jan 7, 2020: WARNING LIGHT. ACTIVATED. STALL PROTECTION SYSTEM FAIL LIGHTS FLASHING IN FLIGHT.
- [SDR RU3A201912065072](https://openairdocs.org/sdr/RU3A201912065072), Dec 4, 2019: WIRE HARNESS. DAMAGED. R/ OUTBOARD ANTI-SKID FAIL ILLUMINATED AFTER TEST. (AIRBORNE)...TEMP REPAIR #2 MLG HARNESS FOR SFP TO REPAIR STATION. WILL MONITOR
- [SDR RU3A20191030060](https://openairdocs.org/sdr/RU3A20191030060), Oct 30, 2019: MOTOR. FAILED. FLAP MOTOR 2 CIRCUIT BREAKER POPPED IN FLIGHT. REPLACING FLAP MOTOR CORRECTED THE DISCREPANCY.
- [SDR RU3A20191030058](https://openairdocs.org/sdr/RU3A20191030058), Oct 30, 2019: CHARGER. FAILED. BATTERY CHARGER CIRCUIT BREAKER TRIPPED IN FLIGHT. CORRECTION: REMOVED AND REPLACED AIRCRAFT BATTERY CHARGER.
- [SDR RU3A20190628026](https://openairdocs.org/sdr/RU3A20190628026), Jun 19, 2019: SKIN. CRACKED. CRACKS THE WING SKIN
- [SDR RU3A20181210050](https://openairdocs.org/sdr/RU3A20181210050), Dec 10, 2018: CONTROL HEAD. BURNED. DESCENDING THROUGH 5000'MSL CREW NOTICED ACRID SMELL. DONNED OXYGEN MASK AND TURNED AFIS OFF. SMELL SLOWLY DISSIPATED. NO SMOKE WAS VISIBLE. CAUSE WAS FOUND TO 
- [SDR RU3A2018031200002](https://openairdocs.org/sdr/RU3A2018031200002), Mar 5, 2018: CRANK ASSY. CRACKED. PASSENGER DOOR LATCH MECHANISM CRANK CRACKED PART 600-31890-21.
- [SDR RU3A20171205043](https://openairdocs.org/sdr/RU3A20171205043), Dec 5, 2017: DISPLAY. INOPERATIVE. AFIS FAILED IN FLIGHT. DISPLAY WENT DEAD, AND ELECTRICAL FUMES WERE PRESENT. MILTOPE(EIFW IN-FLT WKSTATION)
- [SDR RU3A20171012034](https://openairdocs.org/sdr/RU3A20171012034), Oct 12, 2017: WINDSHIELD. CRACKED. PILOT SIDE FRONT WINDOW OUTER GLASS HAD A MAJOR CRACK. REMOVED AND REPLACED PILOT'S WINDSHIELD.
- [SDR RU3A20170210003](https://openairdocs.org/sdr/RU3A20170210003), Feb 10, 2017: CONNECTOR. DIRTY. RIGHT ENGINE COWL ANTI-ICE FAIL LIGHT ILLUMINATED DURING FLIGHT, PROBLEM WAS CORRECTED AFTER CLEANING OF ELECTRICAL CONNECTORS.
- [SDR RU3A20151021022](https://openairdocs.org/sdr/RU3A20151021022), Sep 29, 2015: ANTI-ICE SYSTEM. DEFECTIVE. PILOT LT SIDE WINDSHIELD HEAT FAIL. REPEAT FAILURE.
- [SDR RU3A20150811017](https://openairdocs.org/sdr/RU3A20150811017), Aug 11, 2015: FMS. MALFUNCTIONED. WAAS 1 & WAAS 2 FAILED IN CRUISE FLIGHT. MULTIPLE NAV SYS FAILURES, FD, CDU, FMS 1 & 2 FLAGS ON MFD BOTH SIDE NAV INDICATIONS FAILED. RE-SEATING & RE-LOADING TH
- [SDR RU3A20140519019](https://openairdocs.org/sdr/RU3A20140519019), May 19, 2014: HYDRAULIC LINE. LOOSE. SUPPLEMENTAL INFORMATION: CORRECT ATA CODE(C) TO 2910, CORRECT HOW DISCOVERED (E) TO V-VISUAL. CORRECTIVE ACTION: FOUND LOOSE B NUT ON HYDRAULIC TUBE ASSY P/N: 
- [SDR RU3A20130502006](https://openairdocs.org/sdr/RU3A20130502006), May 1, 2013: WINDOW. CRACKED. DURING FLIGHT, CREW HEARD LOUD POP. INITIAL INSPECTION DISCOVERED LEFT PILOT SIDE WINDOW WITH LARGE CRACK AND SIGNIFICANT GAP IN OUTER PANE WITH ASSOCIATED "FAI
- [SDR RU3A1203](https://openairdocs.org/sdr/RU3A1203), Feb 15, 2012: THRUST REVERSER. MALFUNCTIONED. AT FL150, GOT RIGHT T/R UNLOCK LIGHT. CREW PRESSED T/R EMERGENCY STOW AND COMPLIED WITH CHECKLISTS. DECLARED EMERGENCY AND DIVERTED TO NEAREST AIRPORT WITH ADEQ
- [SDR RU3A1119](https://openairdocs.org/sdr/RU3A1119), Sep 16, 2011: BULKHEAD. BUCKLED. BULKHEAD AND AIRCRAFT SKIN AT FORWARD FUSELAGE STATION 235 IS CRACKED AND BUCKLED.
- [SDR RU3A1109](https://openairdocs.org/sdr/RU3A1109), Feb 15, 2011: PROXIMITY SWITCH. FAULTY. AFTER TAKEOFF THE LANDING GEAR HANDLE WAS MOVED TO THE UP POSITION. BOTH MAIN GEAR RETRACTED BUT THE NOSE GEAR DID NOT RETRACT. THE ONLY INDICATION IN THE COCKP
- [SDR RU3A1018](https://openairdocs.org/sdr/RU3A1018), Jul 23, 2010: UNKNOWN. MALFUNCTIONED. TWO UNCOMMANDED ABRUPT RIGHT RUDDER INPUTS. AUTOPILOT ON. YAW DAMP ON. AIRCRAFT CLIMBING THROUGH 8000 FEET AT 250 KNOTS. SECOND EVENT 11000 FEET AT 250 KNOTS. N
- [SDR RU3A1007](https://openairdocs.org/sdr/RU3A1007), Mar 1, 2010: WINDSHIELD. SPLIT. AFTER APPROXIMATELY 1.0 HOUR OF FLYING IN THE CLIMBOUT TO NEXT WORK, NOTICED WINDSHIELD SPLITTING FROM A SMALL SCRATCH. LEVELED OFF TO 17,000 FEET, RAN CHECKLIS
- [SDR RU3A004](https://openairdocs.org/sdr/RU3A004), Oct 20, 2008: HYDRAULIC LINE. CHAFED. NUMBER 2 HYDRAULIC SYSTEM LOST PRESSURE ON APPROACH. FOUND PRESSURE HOSE ASSY IN PYLON CHAFED BY HOSE CLAMP WHERE RUBBER LINER WAS ERODED AND THE CLAMP AND HOSE
- [SDR RU3A0710](https://openairdocs.org/sdr/RU3A0710), Dec 3, 2007: WINDSHIELD. CRACKED. FLYING AT FL340 1.5 HOURS INTO FLIGHT THE CO-PILOTS WINDSHIELD OUTER PLY CRACKED. COMING INTO THE TERMINAL AREA WITH -3 DEGREE C AND MOISTURE IN THE AIR, RAIN S
- [SDR RU32006F00001](https://openairdocs.org/sdr/RU32006F00001), Apr 17, 2006: WING. SCRATCHED. UPON POST FLT, DISCOVERED STRATCHES ON RT WINGLET. APPARENTLY WHILE POSITIONING OVER GCP AT RKTP, SCRAPED GCP SIGN. NO INDICATION OF CONTACT WHILE AT RTKP. RETU
- [SDR RU3A0419](https://openairdocs.org/sdr/RU3A0419), Nov 29, 2004: SEAL. DETERIORATED. AFTER TAKEOFF FUEL WAS SEEN STREAMING OUT OF LT OVERWING FUEL CAP DURING CLIMB. REPLACED FUEL CAP.
- [SDR 2004F00076](https://openairdocs.org/sdr/2004F00076), Jan 16, 2004: SENSOR. FAILED. ON FINAL APPROACH GEAR EXTENSION AND ANTI-SKID OUTBOARD FAIL MALFUNCTION OCCURRED. GEAR RECYCLED AND SOME TROUBLESHOOTING WAS UNSUCCESSFUL. IN FLIGHT EMERGENCY 
- [SDR RU3A03015](https://openairdocs.org/sdr/RU3A03015), Oct 10, 2003: TUBE. CRACKED. NR 1 HYDRAULIC SYSETM FAILED IN FLIGHT WITH COMPLETE LOSS OF FLUID WITHING THAT SYSTEM. FOUND HYDRAULIC LINE WITH CRACK AT BEND RADIUS. REPLACED HYDRAULIC LINE.
- [SDR R33A03015](https://openairdocs.org/sdr/R33A03015), Oct 10, 2003: LINE. BROKEN. NR 1 HYDRAULIC SYSTEM FAILED IN FILGHT WITH COMPLETE LOSS OF FLUID WITHIN THAT SYSTEM. FOUND HYDRAULIC LINE SNAPPED OFF. REPLACED HYDRAULIC LINE. ALSO, REPLACED
- [SDR RU32003F00003](https://openairdocs.org/sdr/RU32003F00003), Apr 30, 2003: HOUSING. CRACKED. APU FUEL FILTER HOUSING ATTACHMENT FLANGES CRACKED. THIS IS THE FIFTH FILTER HOUSING THAT HAS CRACKED SINCE 01/30/99, THREE ON N86 AND TWO ON N87. AFTER INVESTI
- [SDR 2003F00235](https://openairdocs.org/sdr/2003F00235), Mar 26, 2003: WINDSHIELD. CRACKED. DURING CRUISE AT FL330, PILOTS WINDSHIELD, OUTER PLY, POPPED AND THEN CRACKED IMMEDIATELY FROM TOP TO BOTTOM ORIGINATING FROM CENTER. (M)
- [SDR RU3A03003](https://openairdocs.org/sdr/RU3A03003), Feb 17, 2003: HOUSING. CRACKED. APU FUEL FILTER HOUSING ATTACHMENT FLANGES, CRACKED. THIS IS THE 5TH FILTER HOUSING THAT HAS CRACKED SINCE 01/30/99, 3 ON N86, AND 2 ON N87.
- [SDR RU32001F00000](https://openairdocs.org/sdr/RU32001F00000), Jul 3, 2001: COVER. BROKEN. APU MODEL NUMBER GTCP 36-150RJ. THE LOW PRESSURE FUEL FILTER COVER MOUNTING EAR WAS COMPLETELY BROKEN OFF THE COVER WHERE THE MOUNTING BOLT ATTACHES THE COVER T
- [SDR RU3A99007](https://openairdocs.org/sdr/RU3A99007), Jun 29, 1999: FUEL CAP. DIRTY. FUEL OBSERVED STREAMING DOWN THE RIGHT-HAND WING DURING FLIGHT. FUEL WAS LEAKING AT THE RIGHT-HAND OUTBOARD FUEL CAP. AIRCRAFT MADE UNSCHEDULED LANDING. THE LOC

## FAA accident and incident reports (1)

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 20171012016469I](https://openairdocs.org/incident/20171012016469I), Oct 12, 2017: Canadair Ltd CL-600-2B16 (N87), San Francisco, CA, No damage. The crew reported while at cruise FL340 225 NM over the pacific ocean they heard an extremely loud pop and noticed the pilot side front window pane had…

## Other aircraft with N87

- [Cancelled 1933-02-10](https://openairdocs.org/deregistered/N87-1933-02-10): Junkers MONOPLANE, S/N 663. Owner: [Metal Aircraft Express Corp](https://openairdocs.org/faa-owner/METAL%20AIRCRAFT%20EXPRESS%20CORP), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)

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