# N601VH: 1989 Canadair CL-600-2B16, registration cancelled 2020-12-01 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 1, 2020 - 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: 5043 - Year built: 1989 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 31, 1992 - Certificate issued: October 17, 2017 - Last registry action: May 14, 2020 - Mode S code: A7CCD9 - Owner when cancelled: [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE) - Location: [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake) - Owner type: Corporation - Owner's area on the map: 40.8386° N, 111.9179° W: Placed by OpenAirDocs at the center of ZIP code 84054, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N601VH - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=601VH - Page: https://openairdocs.org/deregistered/N601VH-2020-12-01 From the FAA registry file of November 5, 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 (13) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR O2GA201401290066](https://openairdocs.org/sdr/O2GA201401290066), Jan 25, 2014: PROXIMITY SWITCH. FAILED. WOW INPUT - OUTPUT FAIL MESSAGE AFTER TAKEOFF. ACFT LANDED, EWR AS PRECAUTIONARY MEASURE. DECLARED EMERGENCY WITH NO FURTHER PROBLEMS ON LANDING. - [SDR 2011FA0000384](https://openairdocs.org/sdr/2011FA0000384), Jun 17, 2011: SELECTOR. FAILED. LANDING GEAR DID NOT EXTEND NORMALLY. ALTERNATE EXTENSION USED SUCCESSFULLY FOR DOWN AND LOCKED. - [SDR O2G2005F00010](https://openairdocs.org/sdr/O2G2005F00010), Jul 5, 2005: DRAIN. LIGHTNING STRIKE. C/W LIGHTNING STRIKE INSPECTION. REPLACED FUEL DRAIN MASK. (NE03200509277) - [SDR O2G2005F00011](https://openairdocs.org/sdr/O2G2005F00011), Jun 28, 2005: SUPPRESSOR. LIGHTNING STRIKE. C/W LIGHTNING STRIKE INSPECTION. REPAIRED PITCH TRIM SUPPRESSOR. (K) - [SDR O2G2005F00004](https://openairdocs.org/sdr/O2G2005F00004), Mar 14, 2005: CONTACTOR. FAILED. NR1 THRU FAILED INFLIGHT CAUSING LOSS OF NR 1 DC BUSS AND UTILITY BUSS. REPLACED THE NR 1 LINE CONTACTOR AND NR1 TRU. - [SDR O2G2005F00005](https://openairdocs.org/sdr/O2G2005F00005), Mar 10, 2005: PROXIMITY SWITCH. FAILED. WOW INPUT FAIL ANNUNCIATOR CAME ON AFTER TAKEOFF. REPLACED LT NOSE AND LT MAIN LANDING GEAR OB PROXIMITY SWITCH. (NE03200506802) (K) - [SDR O2G2004F00004](https://openairdocs.org/sdr/O2G2004F00004), Oct 8, 2004: PROXIMITY SWITCH. FAILED. ON GEAR RETRACTION AFTER TO THE RT GEAR DOWN LIGHT REMAINED ON IN THE DOWN AND LOCK INDICATION. GEAR RETRACTED AND EXTENDED AS REPORTED BY TOWER. AIRCRAFT LANDE - [SDR 2004F00282](https://openairdocs.org/sdr/2004F00282), Aug 4, 2004: DRIVE ASSY. FAILED. NR 2 GENERATOR CAME OFF LINE ON TO ROLL OUT OF SBM. TAKEOFF WAS ABORTED BETWEEN 65-75 KTS. GENERATOR RESET WAS SUCCESSFUL ON TAXI BACK. PROCEEDED TO TAKEOFF AND - [SDR O2G2004F00003](https://openairdocs.org/sdr/O2G2004F00003), Feb 8, 2004: PROXIMITY SWITCH. FAILED. AFTER TAKEOFF, GEAR WAS RETRACTED. WOW INPUT FAIL LIGHT ILLUMINATED AND THE NOSE GEAR FAILED TO RETRACT. (MAINS RETRACTED NORMALLY). EXTENDED LANDING GEAR AND R - [SDR 2003F00532](https://openairdocs.org/sdr/2003F00532), Aug 5, 2003: SKIN. LIGHTNING STRIKE. DURING A POST FLIGHT INSPECTION, FOUND EVIDENCE OF AN APPARENT LIGHTNING STRIKE ON THE TRAILING EDGE OF RIGHT WING TIP, BELOW THE WINGLET. AS PER REO 601-57-20- - [SDR 2003F00167](https://openairdocs.org/sdr/2003F00167), Feb 13, 2003: CONTROL UNIT. INTERMITTENT. FLAPS STOPPED AT 2 DEGREES POSITION WHEN FLAPS SELECTED TO 20 DEGREES. RESET CONVETERS AT FLAP CONTROL UNIT. FLAPS OPERATED NORMALLY FOR REMAINDER OF FLIGHT. CH - [SDR 2003F00288](https://openairdocs.org/sdr/2003F00288), Dec 17, 2002: WIRE HARNESS. INTERMITTENT. NOSE GEAR FAILED TO PROPERLY RETRACT AFTER NORMAL TAKEOFF. GEAR HANDLE FLASHING LIGHT REMAINED ILLUMINATED AND NOSE GEAR DOOR REMAINED OPEN. GEAR SELECTED DOWN, - [SDR 99ZZZX4199](https://openairdocs.org/sdr/99ZZZX4199), May 17, 1999: PIN. FAILED. UPON PRE-FLIGHT, NOTICED NR 9 BLOCKER DOOR STANDING STRAIGHT UP IN THE BYPASS SECTION. (THE DOOR SHOULD BE FLUSH WITH THE T/R STOWED). THE BLOCKER DOOR ACTUATIN ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB CEN19WA137](https://openairdocs.org/ntsb/CEN19WA137), May 5, 2019: Canadair CL 600 2B16 (N601VH), Coahuila, Mexico, substantial damage, 14 fatal --- 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.