# N202PS: 2003 Bombardier CL-600-2B19, registration cancelled 2023-10-27

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 27, 2023
- 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: 7858
- Year built: 2003
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 29, 2003
- Certificate issued: February 10, 2021
- Last registry action: April 21, 2023
- Mode S code: A19AC7
- Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%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/N202PS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=202PS
- Page: https://openairdocs.org/deregistered/N202PS-2023-10-27

From the FAA registry file of October 31, 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 (85, newest 50)

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

- [SDR VNAA2019100231105](https://openairdocs.org/sdr/VNAA2019100231105), Sep 30, 2019: ACM. MALFUNCTIONED. THE AIRCRAFT WAS SINGLE-PACK ONLY WHEN IT LEFT DCA. DURING CLIMB AT FL230, THE FUNCTIONING LH PACK OVER-PRESSURED AND AUTOMATICALLY SHUTOFF. THE CREW INITIATED 
- [SDR VNAA2019092711102](https://openairdocs.org/sdr/VNAA2019092711102), Sep 27, 2019: LIGHT. INOPERATIVE. SUPPLEMENTAL INFORMATION RH SIDE #4 EMERGENCY LIGHT ABOVE THE WING INOP RELAMPED RH SIDE #4 EMERGENCY LIGHT OPS CHECK GOOD.
- [SDR VNAA2019090811101](https://openairdocs.org/sdr/VNAA2019090811101), Sep 8, 2019: COMPUTER. FAILED. ON APPROACH TO DCA CREW RECEIVED FUEL IMBALANCE MESSAGES FOLLOWED QRH SAID NEEDED TO LAND WITH 20 DEGREES FLAPS, CREW DIVERTED TO IAD FOR THE LONGER RWY AND SAF
- [SDR VNAA2019070211103](https://openairdocs.org/sdr/VNAA2019070211103), Jul 2, 2019: BPSU. FAILED. FLAPS FAIL IN FLIGHT. R&R LT FLAP BPSU OPS CHECK GOOD.
- [SDR VNAA2019010611101](https://openairdocs.org/sdr/VNAA2019010611101), Jan 6, 2019: WINDSHIELD. CRACKED. ON DECENT THE CAPTAINS WINDSHIELD CRACKED IN FLIGHT. THE CREW DONNED THEIR OXYGEN MASKS AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT FURTHUR INCIDENTS
- [SDR VNAA2018121899908](https://openairdocs.org/sdr/VNAA2018121899908), Dec 18, 2018: FRAME. CORRODED. F.S. 364 FRAME CORRODED AT STINGER 23R. C/A: SPLICE REPAIRED FS 264 FRAME IAW BBD REO 601R-53-21-3055
- [SDR VNAA2018031211101](https://openairdocs.org/sdr/VNAA2018031211101), Mar 12, 2018: WARNING MESSAGE. FALSE ACTIVATION. THE AIRCRAFT RECEIVED A STALL FAIL 1 MESSAGE AT 5000 FEET. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE COMPLIED WITH A SYS RESET OF STALL COM
- [SDR VNAA2017092199911](https://openairdocs.org/sdr/VNAA2017092199911), Sep 18, 2017: STIFFENER. CRACKED. LOWER STIFFENER ON AFT SIDE OF THE BS 621 BULKHEAD, LBL 36 FOUND CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-40-11, AND 51-42-06.
- [SDR VNAA2017092199910](https://openairdocs.org/sdr/VNAA2017092199910), Sep 18, 2017: DOOR FRAME. CORRODED. PASSENGER DOOR UPPER FRAME AT BS 333 IS CRACKED AT THE STANDOFF. REMOVED & REPLACED THE UPPER DOOR FRAME,
- [SDR VNAA2017092199909](https://openairdocs.org/sdr/VNAA2017092199909), Sep 18, 2017: FRAME. CORRODED. FUSELAGE FRAME AT BS 605 IS CORRODED FROM STRINGERS 24L TO 24R. INSTALLED A NEW FRAME.
- [SDR VNAA2017092199908](https://openairdocs.org/sdr/VNAA2017092199908), Sep 18, 2017: FLOOR SUPPORT. CORRODED. LEFT FLOOR SUPPORT IS CORRODED FROM BS 574 TO 621. REPAIRED IAW REO 601R-53-00-526.
- [SDR VNAA2017092199907](https://openairdocs.org/sdr/VNAA2017092199907), Sep 18, 2017: FLOOR SUPPORT. CORRODED. RIGHT FLOOR SUPPORT CORRODED FROM BS 559+96 TO 595. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-00-526.
- [SDR VNAA2017092199906](https://openairdocs.org/sdr/VNAA2017092199906), Sep 18, 2017: FLOOR SUPPORT. CORRODED. LEFT FLOOR SUPPORT IS CORRODED AT BS 473.15 AND 559. COMPLIED WITH REO 601R-53-41-666.
- [SDR VNAA2017092199905](https://openairdocs.org/sdr/VNAA2017092199905), Sep 18, 2017: FLOOR SUPPORT. CORRODED. RIGHT SIDE FLOOR SUPPORT CORRODED AT BS 499 AND 513 . COMPLIED WITH REO 601R-53-41-666.
- [SDR VNAA2017092199904](https://openairdocs.org/sdr/VNAA2017092199904), Sep 18, 2017: FLOORBEAM. CRACKED. FS 280.00 FLOORBEAM CRACKED AT RBL 9. REPAIRED IAW REO 601R-53-11-171 REV D.
- [SDR VNAA2017092199903](https://openairdocs.org/sdr/VNAA2017092199903), Sep 18, 2017: DOOR SILL. CORRODED. RT FLOOR SILL DOUBLER AT FS 319.70 IS CORRODED ON I/B CORNER RBL 36. REMOVED AND REPLACED W/NEW SERVICEABLE P/N 601R38669-49 IAW SRM 51-42-06, 51-40-11 AND 51-4
- [SDR VNAA2017092199902](https://openairdocs.org/sdr/VNAA2017092199902), Sep 18, 2017: BULKHEAD. CRACKED. FS 621 REAR PRESSURE BULKHEAD WEB CRACKED AT LBL 18.0 / WL 132, LBL 27.50 / WL 112, BL 0.0 / WL 112, BL 0.0 / WL 134, RBL 9.50 / WL103, RBL 9.50 / WL110, RBL 9.
- [SDR VNAA2017010900006](https://openairdocs.org/sdr/VNAA2017010900006), Jan 9, 2017: BEAM. LEAKING. LOUD HIGH PRESSURE HISS EMINATING FROM FRONT LEFT SIDE OF COCKPIT. RESEALED LEFT WINDSHIELD I-BEAM.
- [SDR VNAA2016092400027](https://openairdocs.org/sdr/VNAA2016092400027), Sep 24, 2016: LIGHT. PEELING. EMERGENCY LIGHT STRIP AT ROW 1D PEELING UP. MAINTENANCE INSPECTED, R & R THE LIGHT STRIP COVER AT ROW 1D AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED
- [SDR VNAA2016061200018](https://openairdocs.org/sdr/VNAA2016061200018), Jun 12, 2016: SHUTOFF VALVE. MALFUNCTIONED. RIGHT BLEED AIR SHUTOFF VALVE FAILED TO OPEN. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, AND PERFORMED OPS CHECKS IAW THE AM
- [SDR VNAA2015102100014](https://openairdocs.org/sdr/VNAA2015102100014), Oct 21, 2015: CONTROL PANEL. FAILED. CREW REPORTED AIR DRIVEN GENERATOR INADVERTENTLY DEPLOYED DURING TAKEOFF ROTATION. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, 
- [SDR VNAA2015081800030](https://openairdocs.org/sdr/VNAA2015081800030), Aug 18, 2015: BATTERY PACK. FAILED. PRIOR TO FIRST FLIGHT OF THE DAY, CREW REPORTED THE FOLLOWING EMERGENCY LIGHTS INOPERATIVE: FLOOR LEVEL AFT OF ROW 5, LT OVERWING EXIT, TOP, RT OVERWING EXIT, L
- [SDR VNAA2015081800029](https://openairdocs.org/sdr/VNAA2015081800029), Aug 18, 2015: BATTERY PACK. FAILED. PRIOR TO FIRST FLIGHT OF THE DAY, CREW REPORTED THE FOLLOWING EMERGENCY LIGHTS INOPERATIVE: FLOOR LEVEL AFT OF ROW FIVE, LEFT OVERWING EXIT - TOP, RT OVERWING E
- [SDR VNAA2015051000013](https://openairdocs.org/sdr/VNAA2015051000013), May 10, 2015: ENGINE. FLUCTUATES. CREW REPORTED RT ENGINE N1 FLUCTUATING FROM 80.8 TO 93.0 IN CLIMB AT FL190. CREW LANDED AT DESTINATION AIRPORT WITHOUT INCIDENT. MAINTENANCE INSPECTED AND DEFER
- [SDR VNAA2014070500004](https://openairdocs.org/sdr/VNAA2014070500004), Jul 5, 2014: CONTROL UNIT. FAILED. CREW REPORTED FLAPS FAIL AMBER MESSAGE AT FLAPS 8 DEGREES AFTER TAKEOFF. FLAPS WOULD NOT RETRACT TO ZERO DEGREES. CREW DECLARED EMERGENCY, RETURNED TO FIELD AND
- [SDR VNAA2014062000019](https://openairdocs.org/sdr/VNAA2014062000019), Jun 20, 2014: FEEDER CABLE. DAMAGED. CREW REPORTED LT ENGINE SURGING AT MAXIMUM CLIMB THRUST (MCT) 86.0 TO 91.0 PERCENT N1 AND LT ENGINE FUEL FLOW SURGE 2,300-2,500 AT MCT. NO SURGE BELOW 76 PERCEN
- [SDR VNAA2014050200004](https://openairdocs.org/sdr/VNAA2014050200004), May 2, 2014: SENSOR. FAILED. CREW REPORTED LT N1 PLUS OR MINUS 5 PERCENT UNCOMMANDED POWER ADJUSTMENTS DURING FLIGHT, N1, ITT, N2 AND FUEL FLOW ALL UNCOMMANDED MOVEMENT. UNABLE TO SET AND M
- [SDR VNAA2014030800008](https://openairdocs.org/sdr/VNAA2014030800008), Mar 8, 2014: CONNECTOR. DIRTY. CREW REPORTED LIGHTS ON WITH EMERGENCY LIGHT SWITCH IN ARM POSITION. MAINTENANCE INSPECTED, CLEANED CONNECTOR AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FO
- [SDR VNAA2014030200003](https://openairdocs.org/sdr/VNAA2014030200003), Mar 2, 2014: SKIN. CRACKED. DURING SCHEDULED MAINTENANCE, THE INTERIOR SKIN OF THE CARGO DOOR WAS FOUND CRACKED FORWARD SIDE OF HANDLE CUTOUT. THE AREA WAS INSPECTED AND REPAIRED USING AMM
- [SDR VNAA2014030200002](https://openairdocs.org/sdr/VNAA2014030200002), Mar 2, 2014: STRINGER. CRACKED. DURING SCHEDULED MAINTENANCE, BS 379.0 AT STRINGER 3L WAS FOUND CRACKED WHERE IT CONNECTS TO THE PASSENGER DOOR UPPER SILL. THE AREA WAS INSPECTED AND REPAIRED 
- [SDR VNAA2014030200001](https://openairdocs.org/sdr/VNAA2014030200001), Mar 2, 2014: BULKHEAD. CHAFED. DURING SCHEDULED MAINTENANCE, THE BS 621 PRESSURE BULKHEAD WAS FOUND CHAFED AT BL 0.0 AFT FACE ZEE MEMBER. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRA
- [SDR VNAA2013092200009](https://openairdocs.org/sdr/VNAA2013092200009), Sep 22, 2013: BATTERY PACK. FAILED. CREW REPORTED EMERGENCY LIGHT STRIP ON RT SIDE, FROM SEAT 2D TO 5D, WILL NOT LIGHT UP. MX INSPECTED, R & R NR 2 EMERGENCY LIGHT BATTERY AND INVERTER AND PERFORM
- [SDR VNAA2013072000018](https://openairdocs.org/sdr/VNAA2013072000018), Jul 20, 2013: FUEL CONTROL. FAILED. CREW REPORTED RT ENGINE WOULD NOT PRODUCE TAKEOFF THRUST AT TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. MX TROUBLESHOT, R & R RT ENGINE FUEL CONTROL AND
- [SDR VNAA2013060300001](https://openairdocs.org/sdr/VNAA2013060300001), Jun 3, 2013: POSITION SENSOR. FAILED. CREW REPORTED FLAPS DEGRADED MESSAGE IN FLIGHT AND THAT LEFT FLAP INDICATES ZERO TO 20 DEGREES WITH CONTROLLABILITY ISSUE. AIRCRAFT PITCH REFLECTED MOVEMENT. CR
- [SDR VNAA2013020800006](https://openairdocs.org/sdr/VNAA2013020800006), Feb 8, 2013: PRESSURE SWITCH. DEFECTIVE. CREW REPORTED LEFT COWL ANTI-ICE CAS MESSAGE AFTER TAKEOFF WITH ANTI-ICE SELECTED OFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESH
- [SDR VNAA2012103100016](https://openairdocs.org/sdr/VNAA2012103100016), Oct 31, 2012: BULKHEAD. CRACKED. DURING SCHEDULED MAINTENANCE FOUND FS 202.75 PRESSURE BULKHEAD WEB CRACKED AROUND THE PARKING BRAKE CUTOUT. FS 202.75 PRESSURE BULKHEAD WEB AT THE PARKING BRAKE
- [SDR VNAA2012103100015](https://openairdocs.org/sdr/VNAA2012103100015), Oct 31, 2012: BULKHEAD. CRACKED. DURING SCHEDULED MAINTENANCE THE REAR PRESSURE BULKHEAD WEB INDICATED CRACKED. THE REAR PRESSURE BULKHEAD WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE 
- [SDR VNAA2012090500003](https://openairdocs.org/sdr/VNAA2012090500003), Sep 5, 2012: TRIM SYSTEM. DISCONNECTED. DURING INITIAL CLIMB, CREW REPORTED STAB TRIM DISCONNECTED TWICE AND WAS RESET. AUTOPILOT SELF-CANCELLED AFTER 30 SECONDS OPERATION AND WOULD NOT STAY ON. WHILE
- [SDR VNAA2012082600015](https://openairdocs.org/sdr/VNAA2012082600015), Aug 21, 2012: WIRE HARNESS. DEFECTIVE. CREW REPORTED THE LANDING GEAR WAS SLOW TO RETRACT. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, AND REPLACED THE N
- [SDR VNAA2012070800008](https://openairdocs.org/sdr/VNAA2012070800008), Jul 8, 2012: CONTROL LEVER. FAILED. CREW REPORTED FLAPS FAIL AT 30 DEGREES WHILE COMING IN TO LAND. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED 
- [SDR VNAA2012051400013](https://openairdocs.org/sdr/VNAA2012051400013), May 14, 2012: COMPUTER. MALFUNCTIONED. CREW REPORTED FUEL CHANNEL 1/2 FAIL CAUTION MESSAGE IN FLIGHT FOR A FEW MINUTES, THEN MESSAGE DISAPPEARED. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. M
- [SDR VNAA2012050400005](https://openairdocs.org/sdr/VNAA2012050400005), May 4, 2012: LIGHT. INOPERATIVE. CREW REPORTED EMERGENCY LIGHT STRIP ON FLOOR AT ROW 5D INOPERATIVE. MAINTENANCE INSPECTED, RE-INSTALLED ROW 5D EMERGENCY FLOOR LIGHT STRIP AND PERFORMED CHECKS 
- [SDR VNAA2012041200006](https://openairdocs.org/sdr/VNAA2012041200006), Apr 12, 2012: CIRCUIT BREAKER. TRIPPED. CREW REPORTED PASSENGER DOOR CAS MESSAGE, SERVICE DOOR MESSAGE AND CARGO DOOR MESSAGE ALL CAME ON AT 15,000 FEET ON CLIMBOUT. CREW RETURNED TO FIELD AND LANDED 
- [SDR VNAA2012040800005](https://openairdocs.org/sdr/VNAA2012040800005), Apr 8, 2012: LIGHT. INOPERATIVE. CREW REPORTED FLOOR LEVEL EMERGENCY LIGHTING INOPERATIVE AT SEAT 3D. REMOVED AND REPLACED ROW THREE (3) RIGHT ELECTROLUMINESCENT FLOOR LIGHTING, PERFORMED CHECK
- [SDR VNAA2012011800006](https://openairdocs.org/sdr/VNAA2012011800006), Jan 14, 2012: B-NUT. LOOSE. CREW REPORTED HYD 1 LOW PRESSURE CAS MESSAGE IN FLIGHT EN ROUTE FROM CAK TO PHL. CREW DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND TIG
- [SDR VNAA2011123000016](https://openairdocs.org/sdr/VNAA2011123000016), Dec 26, 2011: COMPUTER. INTERMITTENT. CREW REPORTED FUEL CHANNEL 1/2 FAIL CAUTION MESSAGE WITH YELLOW DASHED LINES IN ALL FUEL QUANTITY READINGS AFTER DEPARTURE FROM CLT. CREW RETURNED TO CLT AND LA
- [SDR VNAA2011120700002](https://openairdocs.org/sdr/VNAA2011120700002), Dec 3, 2011: CONNECTOR. LOOSE. AT CLT, CREW REPORTED FLOOR EMERGENCY PATH LIGHTING AT SEAT 5D HAD A LOOSE CONNECTION. MAINTENANCE INSPECTED, SECURED LOOSE CONNECTION AND PERFORMED CHECKS ON E
- [SDR VNAA2011112200013](https://openairdocs.org/sdr/VNAA2011112200013), Nov 16, 2011: LIGHT. DISCONNECTED. AT CLT, EMERGENCY FLOOR LIGHT AT ROW 4 NOT ILLUMINATING. MAINTENANCE INSPECTED FLOOR EMERGENCY LIGHTING, FOUND ROW 4 UNPLUGGED AND TRACK COVER LOOSE, REINSTALLE
- [SDR VNAA2011090800002](https://openairdocs.org/sdr/VNAA2011090800002), Sep 1, 2011: RADOME. DAMAGED. CREW REPORTED A LIGHTNING STRIKE IN FLIGHT EN ROUTE FROM CAK TO PHL. AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REP
- [SDR VNAA2011031600010](https://openairdocs.org/sdr/VNAA2011031600010), Mar 16, 2011: BULKHEAD. CHAFED. DURING SCHEDULED MAINTENANCE CHAFE DAMAGE WAS FOUND ON THE REAR PRESSURE BULKHEAD. THIS WAS FROM THE ISOLATION VALVE. REPAIRS WERE MADE USING AIRCRAFT MAINTENAN

All 85: https://openairdocs.org/deregistered/N202PS-2023-10-27/reports.md

## 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 DCA19CA035](https://openairdocs.org/ntsb/DCA19CA035), Dec 1, 2018: Bombardier CL 600 2B19 (N202PS), New York, NY, substantial damage. Probable cause: the captain initiating a cross bleed start while under tow.

## Other aircraft with N202PS

- [Cancelled 1980-01-09](https://openairdocs.org/deregistered/N202PS-1980-01-09): Dehavilland BEAVER U-6A, S/N 53-7911, built 1953. Exported to Canada. Owner: [Natrona County Disaster & Civil Def Agcy](https://openairdocs.org/faa-owner/NATRONA%20COUNTY%20DISASTER%20%26%20CIVIL%20DEF%20AGCY), [Casper, WY](https://openairdocs.org/faa-place/WY/Casper)
- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N202PS-undated): Cessna 182Q, S/N 18267558. Triennial form not returned

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