# N716CA: 1998 Bombardier CL-600-2B19, registration cancelled 2015-08-26

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 26, 2015
- Status when cancelled: Valid registration
- Airframe: [Bombardier CL-600-2B19](https://openairdocs.org/model/bombardier-cl-600-2b19) (registry code 1390008)
- Engine: [GE CF34 series](https://openairdocs.org/engine/ge-cf34-series) (registry code 30015)
- Data sheets: [TCDS A21EA-1](https://openairdocs.org/tcds/A21EA-1) (OpenAirDocs)
- Serial number: 7250
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 29, 1998
- Certificate issued: October 31, 2007
- Last registry action: April 14, 2015
- Mode S code: A9928A
- Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N716CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=716CA
- Page: https://openairdocs.org/deregistered/N716CA-2015-08-26

From the FAA registry file of November 7, 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 Bombardier CL-600-2B19: https://openairdocs.org/model/bombardier-cl-600-2b19.md

## Service difficulty reports (69, newest 50)

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

- [SDR COMA2012061950047](https://openairdocs.org/sdr/COMA2012061950047), Jun 18, 2012: SELECTOR VALVE. FAILED. ON CLIMBOUT FROM CVG RECEIVED NOSE GEAR DISAGREE UPON GEAR RETRACTION. EMERGENCY DECLARED, A/C RETURNED TO CVG LANDED SAFELY. REMOVED AND REPLACED NLG SELECTOR 
- [SDR COMA2011121250099](https://openairdocs.org/sdr/COMA2011121250099), Dec 11, 2011: MANIFOLD. FAILED. ON APPROACH INTO CID THE LEFT O/B GROUND SPOILER DEPLOYED. INDICATION REMAINED, BUT VERIFIED THAT THE SPOILER HAD RETRACTED. EMERGENCY DECLARED, A/C LANDED SAFE
- [SDR COMA2011120750098](https://openairdocs.org/sdr/COMA2011120750098), Dec 7, 2011: ANGLE. CORRODED. CAMLOC CHANNEL FOR COCKPIT FLOORBOARD IS CORRODED AT FS 280.00. REPLACED DISCREPANT ANGLE P/N 600-34017-351 IAW BOMBARDIER SRM 51-42-21, PRIMED AND PAINTED IAW 
- [SDR COMA2011112850094](https://openairdocs.org/sdr/COMA2011112850094), Nov 27, 2011: ANGLE. CORRODED. PAX DOOR SILL HAS SURFACE CORROSION. FOUND ANGLE ASSEMBLY CORRODED BEYOND LIMITS, REMOVED AND REPLACED ANGLE IAW SRM 51-42-21, 51-42-06, 51-42-13.
- [SDR COMA2009110550205](https://openairdocs.org/sdr/COMA2009110550205), Nov 5, 2009: BULKHEAD. CRACKED. CARGO DOOR LINTEL ATTACHMENT FITTING CRACKED AT FS 621.00. REPAIRED AFT PRESSURE BULKHEAD AT FS 621.00 IAW REO 601R-53-61-1230.
- [SDR COMA2009110450203](https://openairdocs.org/sdr/COMA2009110450203), Nov 4, 2009: INTERCOSTAL. CRACKED. CARGO DOOR LOWER FRAME INTERCOSTAL CRACKED BETWEEN FASTENERS. REPLACED CARGO DOOR LOWER FRAME INTERCOSTAL P/N 601R35027-31 IN ACCORDANCE WITH CRJ SRM 51-42-00.
- [SDR COMA2009110550206](https://openairdocs.org/sdr/COMA2009110550206), Nov 1, 2009: BULKHEAD. CRACKED. FOUND CRACK ON AFT PRESSURE BULKHEAD AT FS 621.00 LBL 27.50 ABOVE THE CARGO DOOR AFT TRACK SUPPORT. REMOVED DAMAGE AND INSTALLED DOUBLER, TRIPLER IAW REO 601R-5
- [SDR COMA2009110250202](https://openairdocs.org/sdr/COMA2009110250202), Oct 31, 2009: BULKHEAD. CRACKED. FOUND 4 CRACKS ON AFT PRESSURE BULKHEAD AT FS 621.00 RBL 18.00. REMOVED DAMAGE AND REPAIRED IAW REO 601R-53-61-1285.
- [SDR COMA2009110250201](https://openairdocs.org/sdr/COMA2009110250201), Oct 31, 2009: BULKHEAD. CRACKED. FOUND FWD PRESSURE BULKHEAD CRACKED AT FS 202.75 AROUND PARKING BRAKE CABLE HOLE. REMOVED DAMAGE AND REPAIRED IAW REO 601R-53-11-563 AND EA 10-5311-02789.
- [SDR COMA2009110250200](https://openairdocs.org/sdr/COMA2009110250200), Oct 31, 2009: BULKHEAD. CRACKED. FOUND 5 CRACKS AT FS 621.00 BL 0.00. REMOVED DAMAGE AND INSTALLED SERVICEABLE REPAIR DOUBLERS IAW BOMBARDIER REO 601R-53-61-1285.
- [SDR COMA2009102850199](https://openairdocs.org/sdr/COMA2009102850199), Oct 28, 2009: BULKHEAD. CRACKED. FOUND 2 CRACKS ON AFT PRESSURE BULKHEAD AT FS 621.00 LBL 18.00. REMOVED DAMAGE AND REPAIRED IAW REO 601R-53-61-1285.
- [SDR COMA2009102650198](https://openairdocs.org/sdr/COMA2009102650198), Oct 24, 2009: POST. CRACKED. VERTICAL BULKHEAD POST AT FS 559.00 RBL 9 CRACKED ON O/B LOWER END. REPAIRED BULKHEAD POST IAW REO 601R-53-41-057.
- [SDR COMA0760675](https://openairdocs.org/sdr/COMA0760675), Nov 29, 2007: PDU. WORN. FLIGHT 5053 - FLAPS FAIL CAUTION MESSAGE, FLAPS FAILED AT 12 DEGREES ON DESCENT. AIRCRAFT LANDED SAFELY IN JFK. REMOVED AND REPLACED PDU.
- [SDR COMA0760651](https://openairdocs.org/sdr/COMA0760651), Nov 16, 2007: CONTROL ROD. FAULTY. FLIGHT 5109 - AFTER TAKEOFF FROM CLE AIRCRAFT WOULD NOT PRESSURIZE, FLIGHT RETURNED TO CLE. REPLACED THE CABIN DOOR VENT VALVE CONTROL ROD. 
- [SDR COMA0760557](https://openairdocs.org/sdr/COMA0760557), Sep 4, 2007: HANDLE. OUT OF POSITION. FLIGHT 5354 - PAC DOOR HANDLE CAUTION MESSAGE AT 8000 FT DURING CLIMB. QRH PROCEDURE COMPLETED. AIRCRAFT RETURNED BACK TO CHS AND LANDED SAFELY. UPON ARRIVAL FO
- [SDR COMA0660679](https://openairdocs.org/sdr/COMA0660679), Dec 3, 2006: WARNING SYSTEM. MALFUNCTIONED. FLIGHT 5145 - PAX DOOR OUTER HANDLE CAUTION MESSAGE DURING FLIGHT. DIVERTED TO BTV. LANDED WITHOUT INCIDENT. FOUND DOOR SENSORS D113 AND D117 BOTH SHOWED INCORR
- [SDR COMA0660467](https://openairdocs.org/sdr/COMA0660467), Aug 1, 2006: WARNING MESSAGE. FALSE INDICATION. FLIGHT 5093 - DURING CVG APPROACH RECEIVED A CABIN DOOR OUTER HANDLE MESSAGE, CREW DECLARED AN EMERGENCY AND PERFORMED QRH, ABORTED APPROACH THEN LANDED WITHOUT
- [SDR COMA0660437](https://openairdocs.org/sdr/COMA0660437), Jul 13, 2006: WARNING SYSTEM. FALSE ACTIVATION. FLIGHT 5036 - PAX DOOR CAUTION MESSAGE. ONCE LEVEL AT 3000 FT OVBD AND INBD COOL FAIL CAME ON. RETURNED TO BOS AND FLIGHT LANDED WITHOUT INCIDENT. INSPECTED PAX
- [SDR COMA0560449](https://openairdocs.org/sdr/COMA0560449), Aug 16, 2005: WARNING LIGHT. FALSE ACTIVATION. FLIGHT 5298 - CABIN DOOR OUTER HANDLE CAUTION. CND, FOUND NO DEFECTS WITH DOOR.
- [SDR COMA0560426](https://openairdocs.org/sdr/COMA0560426), Aug 4, 2005: HANDLE. WORN. FLIGHT 5486 - DURING CLIMBOUT OF HSV RECEIVED A CABIN DOOR WARNING CAUTION MESSAGE. FLIGHT RETURNED TO THE FIELD. REPLACED THE OUTER CABIN DOOR HANDLE LATCH BAS
- [SDR COMA0560412](https://openairdocs.org/sdr/COMA0560412), Jul 27, 2005: WARNING LIGHT. ILLUMINATED. FLIGHT 5429 - CABIN DOOR OUTER HANDLE CAUTION MESSAGE. DEFERRED MAINTENANCE ON DOOR WARNING PER MEL.
- [SDR COMA0560390](https://openairdocs.org/sdr/COMA0560390), Jul 10, 2005: WIRE HARNESS. UNRELIABLE. FLIGHT 5823 - CABIN DOOR OUTER HANDLE CAUTION. REPLACED THE DOOR WIRE HARNESS.
- [SDR COMA0560379](https://openairdocs.org/sdr/COMA0560379), Jul 4, 2005: FLT CONTROLS. VIBRATION. MODERATE VIBRATION IN CONTROLS AT SPEED GREATER THAN 260. INSPECTED FUSELAGE, VERTICAL STAB FAIRINGS AND FLIGHT CONTROLS. NO DEFECTS NOTED.
- [SDR COMA0560155](https://openairdocs.org/sdr/COMA0560155), Mar 2, 2005: CONNECTOR. CONTAMINATED. FLIGHT 5747 NO STARTER CUTOUT MESSAGE. CLEANED OIL FROM STARTER WIRING CONNECTOR.
- [SDR COMA0560114](https://openairdocs.org/sdr/COMA0560114), Feb 6, 2005: WARNING LIGHT. ILLUMINATED. FLIGHT 5089 FLAPS FAIL CAUTION. RESET FLAP SYSTEM PER AD 98-20-01 AND DEFERRED MAINT PER MEL.
- [SDR COMA0560018](https://openairdocs.org/sdr/COMA0560018), Dec 31, 2004: WARNING SYSTEM. MALFUNCTIONED. FLIGHT 5715 DISPLAY COOL MESSAGE. COULD NOT DUPLICATE. INSPECTED SYSTEM, FOUND NO DEFECTS.
- [SDR COMA0460525](https://openairdocs.org/sdr/COMA0460525), Sep 15, 2004: PUMP. MALFUNCTIONED. FLIGHT 5260 LT ENGINE OIL PRESSURE WARNING. REPLACED THE LT ENGINE LUBE PUMP.
- [SDR COMA0460444](https://openairdocs.org/sdr/COMA0460444), Aug 2, 2004: FRAME. CORRODED. DURING A 72/48 MO INSP, TASK CRJ-2-142005, FOUND FUSELAGE FRAME CORRODED ON TOP EDGE. PERFORMED PERMANENT REPAIR IAW COMAIR EA 10-5310-00389 AND REO 601R-53-11-
- [SDR COMA0460381](https://openairdocs.org/sdr/COMA0460381), Jun 14, 2004: SEAL. LEAKING. FLIGHT 5835 RT ENGINE LOW OIL PRESSURE WARNING. REPLACED ACCESSORY GEARBOX DRIVE OIL SEALS.
- [SDR COMA0460359](https://openairdocs.org/sdr/COMA0460359), Jun 8, 2004: WARNING LIGHT. ILLUMINATED. FLIGHT 5143 FLAPS FAIL CAUTION MESSAGE. RESET FLAPS AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0460196](https://openairdocs.org/sdr/COMA0460196), Mar 12, 2004: WARNING LIGHT. ILLUMINATED. FLGIHT 5710 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0460182](https://openairdocs.org/sdr/COMA0460182), Mar 4, 2004: WARNING LIGHT. ILLUMINATED. FLIGHT 5088 FLAPS FAIL WARNING MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0460069](https://openairdocs.org/sdr/COMA0460069), Jan 20, 2004: FLAP. FAILED. FLIGHT 5211 FLAPS FAILED AT 26 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0360580](https://openairdocs.org/sdr/COMA0360580), Dec 28, 2003: OIL SYSTEM. OVERSERVICED. FLIGHT 5904 RIGHT ENGINE OIL PRESSURE DROPPING AND TEMP INCREASING IFSD. ENGINE WAS OVERSERVICED 6 QTS OF OIL. DRAINED EXCESS OIL.
- [SDR COMA0360487](https://openairdocs.org/sdr/COMA0360487), Nov 5, 2003: POWER SUPPLY. DISCHARGED. FLIGHT 5238 SECTION OF FLOOR EMERGENCY LIGHTING AFT OF ROW 8 IS INOPERATIVE. REPLACED FAILED FLOOR EMERGENCY POWER STRIP.
- [SDR COMA0360458](https://openairdocs.org/sdr/COMA0360458), Oct 13, 2003: CONTROLLER. MALFUNCTIONED. RT WINDSHIELD HEAT CAUTION MESSAGE. REPLACED THE HEAT CONTROLLER.
- [SDR COMA0360443](https://openairdocs.org/sdr/COMA0360443), Oct 3, 2003: ELEMENT. FALSE INDICATION. FLIGHT 5703 LT 14TH STAGE BLEED LEAK WARNING. REPLACED THE PYLON BLEED LEAK SENSE ELEMENT.
- [SDR COMA0360396](https://openairdocs.org/sdr/COMA0360396), Aug 30, 2003: BLOCKER DOOR. BROKEN. FLIGHT 5675 RT THRUST REVERSER BLOCKER DOOR AT 4 O'CLOCK POSITON FOUND BROKEN IN HALF. REMOVED BROKEN BLOCKER DOOR AND INSTALLED A SERVICEABLE ONE.
- [SDR COMA0360395](https://openairdocs.org/sdr/COMA0360395), Aug 30, 2003: THRUST PLATE. BROKEN. RIGHT THRUST REVERSER SPRING BOX ASSEMBLY AT 4 O'CLOCK POSITION WAS FOUND BROKEN. REMOVED BROKEN SPRING BOX ASSEMBLY AND INSTALLED A SERVICEABLE ONE.
- [SDR COMA0360235](https://openairdocs.org/sdr/COMA0360235), May 9, 2003: PRIORITY VALVE. UNRELIABLE. FLIGHT 5259 LANDING GEAR DISAGREE WARNING, NLG INDICATED UNSAFE. REPLACED THE NLG PRIORITY VALVE.
- [SDR COMA0360097](https://openairdocs.org/sdr/COMA0360097), Feb 10, 2003: ACTUATOR. UNRELIABLE. FLIGHT 5438 STAB CHANNEL 1 IS INOP.REPLACED THE HSTA.
- [SDR COMA0260671](https://openairdocs.org/sdr/COMA0260671), Nov 28, 2002: SPOILER. FLIGHT 5867 CONFIG SPOILERS CAUTION DURING T/O.COULD NOT DUPLICATE - NO FAULT CODES IN COMPUTER.
- [SDR COMA0260541](https://openairdocs.org/sdr/COMA0260541), Sep 19, 2002: LANDING GEAR. FLIGHT 5283 GEAR DISAGREE WARNING, NLG SLOW TO EXTEND.COULD NOT DUPLICATE. RETRACT AND EXTENSION CHECKS WERE NORMAL.
- [SDR COMA0260529](https://openairdocs.org/sdr/COMA0260529), Sep 16, 2002: CLIP. FAILED. DURING FLIGHT NUMBER ONE THROTTLE LEVER JAMMED WITH 90 PERCENT THRUST. UNABLE TO REDUCE. SHUT DOWN ENGINE WITH FIRE PUSH SW LIGHT AND LANDED SINGLE ENGINE. FOUN
- [SDR COMA0260288](https://openairdocs.org/sdr/COMA0260288), Apr 28, 2002: LIGHT. INOPERATIVE. EMERGENCY FLOOR PATH LIGHTS ROW 1 TO 5 ARE INOP. REPLACED THE NR 2 FLOOR LIGHT STRIP.
- [SDR COMA0260196](https://openairdocs.org/sdr/COMA0260196), Mar 15, 2002: SWITCH. MALFUNCTIONED. FLIGHT 5620 UNABLE TO PRESSURIZE CABIN AFTER T/O.REPLACED CABIN DOOR PROX SWITCH PS2M13.
- [SDR COMA0260107](https://openairdocs.org/sdr/COMA0260107), Feb 16, 2002: PRIORITY VALVE. MALFUNCTIONED. FLIGHT 5324 GEAR DISAGREE AND NOSE DOOR WARNINGS WHEN LANDING GEA SELECTED DOWN.REPLACED THE NLG PRIORITY VALVE.
- [SDR COMA0260032](https://openairdocs.org/sdr/COMA0260032), Jan 2, 2002: BEAM. CRACKED. THE ENGINE SUPPORT BEAM LOWER WEB WAS CRACKED AT THE L/H AND R/H SIDES.REPAIRED THE CRACKED LOWER WEB I/A/W REO 601R-53-61-366 REV. C.
- [SDR COMA0260009](https://openairdocs.org/sdr/COMA0260009), Dec 31, 2001: DOUBLER. CRACKED. F.S. 718.00 STRINGER 11 R/H AND L/H AFT DOUBLERS ARE CRACKED.REMOVED AND REPLACED R/H AND L/H AFT DOUBLERS F.S. 718.00 STRINGER 11. I/A/W CANADAIR R.E.O. 601R-5
- [SDR COMA0160038](https://openairdocs.org/sdr/COMA0160038), Dec 31, 2000: HEATER. FAILED. LT WINDOW HEAT CAUTION MESSAGE. REPLACED WINDOW.

All 69: https://openairdocs.org/deregistered/N716CA-2015-08-26/reports.md

## Other aircraft with N716CA

- [Cancelled 2024-06-13](https://openairdocs.org/deregistered/N716CA-2024-06-13): Textron 208B, S/N 208B5793, built 2024. Exported to Thailand. Owner: [Textron Financial Corp](https://openairdocs.org/faa-owner/TEXTRON%20FINANCIAL%20CORP), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)
- [Cancelled 1988-12-15](https://openairdocs.org/deregistered/N716CA-1988-12-15): Cessna 310J, S/N 310J0121. N-number assigned, not yet registered

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