# N250PS: 2004 Bombardier CL-600-2B19, registration cancelled 2025-12-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 9, 2025
- 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: 7929
- Year built: 2004
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 30, 2004
- Certificate issued: April 11, 2023
- Last registry action: May 2, 2023
- Mode S code: A258D4
- Owner when cancelled: [Frontera Flight Holdings Inc](https://openairdocs.org/faa-owner/FRONTERA%20FLIGHT%20HOLDINGS%20INC)
- Location: [Dover, DE](https://openairdocs.org/faa-place/DE/Dover)
- Owner type: Corporation
- Owner's area on the map: 39.1815° N, 75.4736° W: Placed by OpenAirDocs at the center of ZIP code 19901, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N250PS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=250PS
- Page: https://openairdocs.org/deregistered/N250PS-2025-12-09

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 Bombardier CL-600-2B19: https://openairdocs.org/model/bombardier-cl-600-2b19.md

## Service difficulty reports (89, newest 50)

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

- [SDR VNAA2020031921101](https://openairdocs.org/sdr/VNAA2020031921101), Mar 16, 2020: FLASHLIGHT. INOPERATIVE. FWD FA FLASHLIGHT INOP. MX REMOVED AND REPLACED FWD FA FLASHLIGHT. OPS CHECK GOOD.
- [SDR VNAA2020031101101](https://openairdocs.org/sdr/VNAA2020031101101), Mar 8, 2020: TUBE. CRACKED. UNCOMMANDED DECELERATION OF RH ENGINE IN FLIGHT APROX 8% N1. MAINTENANCE FOUND THE T2 ANTI ICE TUBE ASSY CRACKED, REMOVED AND AND REPLACED THE TUBE ASSY OPS CHE
- [SDR VNAA2020030511101](https://openairdocs.org/sdr/VNAA2020030511101), Mar 2, 2020: BPSU. OUT OF RIG. ON FINAL APPROACH INTO LGA, THE CREW PULLED FLAPS FROM 8-20, BUT FLAPS DID NOT MOVE, AND A FLAP FAILURE MESSAGE APPEARED. THE CREW EXECUTED A GO AROUND, AND DEC
- [SDR VNAA2020021261102](https://openairdocs.org/sdr/VNAA2020021261102), Jan 26, 2020: ENGINE. OSCILLATES. AT 27000 FEET RIGHT ENGINE N1 OSCILLATED BETWEEN 81 TO 88 SLOWED THE PLANE AND IT STEADIED OUT. CONTINUED THE FLIGHT. PERFORMED ENG. RUN & CHECK N1 SPEED-CONTRO
- [SDR VNAA2019123091101](https://openairdocs.org/sdr/VNAA2019123091101), Dec 29, 2019: WIRE. DISCONNECTED. EXIT SIGN EMERGENCY LIGHT BY PAX DOOR INOP. FOUND WIRE UNPLUGGED. CONNECTED THE WIRE IAW AMM 33-51-10-400-801. OPS CHECK GOOD.
- [SDR VNAA2019121011101](https://openairdocs.org/sdr/VNAA2019121011101), Dec 10, 2019: SENSOR. DIRTY. AT 800 FT AFTER TAKEOFF, THE CREW OBSERVED AND FELT THE RH N1 SURGE. CREW LEVELED OFF AT 5000 FT, RAN QRH, AND RETURNED TO THE FIELD. THE CREW DID NOT DECLARE A
- [SDR VNAA2019082097111](https://openairdocs.org/sdr/VNAA2019082097111), Aug 17, 2019: PUMP. FAILED. ON CLIMB OUT AT FL100 ENGINE 1 OIL TEMP READ OUT FLASHED RED INDICATING HIGH OIL TEMP. CREW REQUESTED LEVEL OFF WITH ATC, BACKED ENGINE POWER DOWN AND RAN THE Q
- [SDR VNAA2019073011101](https://openairdocs.org/sdr/VNAA2019073011101), Jul 30, 2019: POWER SUPPLY. FAILED. CENTER AISLE EMERGENCY EXIT/FWD SIGN LIGHT INOP. R&R EMERGENCY BATTERY SUPPLY. IAW CRJ200 AMM 33-51-04-000/400-801. OPS CHECK GOOD.
- [SDR VNAA2019020199913](https://openairdocs.org/sdr/VNAA2019020199913), Feb 1, 2019: FLOORBEAM. CRACKED. R/H FS484.00 ANGLES @ RBL27 & RBL36 ARE CRACKED. C/A: REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-40-11, & 51-42-21
- [SDR VNAA2019020199912](https://openairdocs.org/sdr/VNAA2019020199912), Feb 1, 2019: FLOORBEAM. CRACKED. L/H FS484.00 ANGLES @ LBL27 & LBL36 ARE CRACKED. C/A: REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-40-11, & 51-42-21
- [SDR VNAA2019020199911](https://openairdocs.org/sdr/VNAA2019020199911), Feb 1, 2019: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT ANGLES AND CUPS AT PAX DOOR SILL ARE CORRODED FROM F.S. 310 TO F.S. 349. C/A: REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT ANGLES AND CUPS REF CRJ 
- [SDR VNAA2019020199910](https://openairdocs.org/sdr/VNAA2019020199910), Feb 1, 2019: SEAT TRACK. CORRODED. LBL9 AND RBL9 FS364-399 FLOOR SEAT TRACK SEGMENTS HAVE CORROSION. C/A: REMOVED AND REPLACED TRACK SEGMENT IAW BOMBARDIER REO 601R-53-00-485.
- [SDR VNAA2019020199909](https://openairdocs.org/sdr/VNAA2019020199909), Feb 1, 2019: SEAT TRACK. CRACKED. LBL9 AND RBL9 FS399-409+120 FLOOR SEAT TRACK SEGMENTS HAVE CORROSION. C/A: REMOVED AND REPLACED TRACK SEGMENT IAW BOMBARDIER REO 601R-53-00-485.
- [SDR VNAA2019020199908](https://openairdocs.org/sdr/VNAA2019020199908), Feb 1, 2019: STIFFENER. CRACKED. PAX DOOR ASSIST MOTOR CRACKED AT WEB SIDE ATTACH POINT. C/A: REMOVED AND REPLACED PAX DOOR SIDE PANEL STIFFENER REF CRJ 200 SRM 51-42-15.
- [SDR VNAA2019020199907](https://openairdocs.org/sdr/VNAA2019020199907), Feb 1, 2019: FRAME. CRACKED. FS 333.0 FRAME IS CRACKED BETWEEN STRINGER 0 AND STRINGER 1L. C/A: REMOVED AND REPLACED FRAME IAW CRJ 200SRM 51-40-11,51-42-21 AND 51-42-06.
- [SDR VNAA2019020199906](https://openairdocs.org/sdr/VNAA2019020199906), Feb 1, 2019: TRUNNION. CRACKED. L/H LOWER WING PLANK MLG TRUNNION FASTENER HOLE (FWD LOOKING AFT) HAS AN INDICATION AT 5TH FASTENER HOLE FROM THE FWD EDGE OF STEEL STRAP AT 55% FSH, FAILED NDT
- [SDR VNAA2019020199905](https://openairdocs.org/sdr/VNAA2019020199905), Feb 1, 2019: TRUNNION. CRACKED. L/H LOWER WING PLANK MLG TRUNNIION FASTENER HOLE (FWD LOOKING AFT) HAS AN INDICATION AT 2ND FASTENER HOLE FROM THE FWD EDGE OF STEEL STRAP AT 60% FSH FAILED NDT
- [SDR VNAA2019020199904](https://openairdocs.org/sdr/VNAA2019020199904), Feb 1, 2019: TRUNNION. CRACKED. FOUND INDICATION ON R/H TRUNNION 7TH HOLE FROM AFT TO STRAP 90% FSH APPROX. 0.5 UP THE TRUNNION FAILS NDT. C/A: REPAIRED R/H TRUNNION DAMAGED FASTENER HOLE IAW 
- [SDR VNAA2019020199903](https://openairdocs.org/sdr/VNAA2019020199903), Feb 1, 2019: TRUNNION. CRACKED. FOUND INDICATION ON R/H TRUNNION 4TH HOLE FROM AFT OF STRAP 60% FSH APPROX. 0.75 UP THE TRUNNION FAILS NDT. C/A: REPAIRED R/H TRUNNION DAMAGED FASTENER HOLE IAW
- [SDR VNAA2019020199902](https://openairdocs.org/sdr/VNAA2019020199902), Feb 1, 2019: ANGLE. CRACKED. FS409+128 BLO RH VERTICAL POST ANGLE HAS AN INDICATION .15" LONG BY 80% FSH IN THE UPPER AFT RADIUS WL69. C/A: REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-40-
- [SDR VNAA2019020199901](https://openairdocs.org/sdr/VNAA2019020199901), Feb 1, 2019: SEAL DEPRESSOR. CORRODED. PAX DOOR LOWER SEAL SURROUND CORRODED. C/A: REMOVED AND REPLACED PAX DOOR LOWER SEAL SURROUND IAW CRJ 200 SRM 51-40-11 AND 51-42-06.
- [SDR VNAA2018091711101](https://openairdocs.org/sdr/VNAA2018091711101), Sep 10, 2018: LOOP. CONTAMINATED. CREW RECEIVED A L 10TH DUCT RED MSG. RAN THE QRH AND CAUTION DID NOT CLEAR. DECLARED AN EMERGENCY AND LANDED IN GSO. CLT MX GOING TO GSO WITH PARTS. CLT MX FOUN
- [SDR VNAA2018021611102](https://openairdocs.org/sdr/VNAA2018021611102), Feb 16, 2018: WARNING MESSAGE. ACTIVATED. THE CREW RECEIVED AN ANTI-ICE DUCT SYSTEM MESSAGE. THE CREW RAN THE QRH AND DECLARED AN EMERGENCY TO CLIMB OUT OF ICING CONDITIONS. THE CREW CONTINUED TO THEIR 
- [SDR VNAA2017082911102](https://openairdocs.org/sdr/VNAA2017082911102), Aug 29, 2017: CONTROLLER. MALFUNCTIONED. AFTER DEPARTURE, THE CREW RECEIVED A LEFT WINDSHIELD HEAT CAUTION MESSAGE AND NOTICED A SLIGHT ODOR. THE QUICK REFERENCE HANDBOOK WAS FOLLOWED AND CYCLED SYSTEM
- [SDR VNAA2017082811102](https://openairdocs.org/sdr/VNAA2017082811102), Aug 28, 2017: UNKNOWN. ODOR. BURNING ODOR FROM LEFT PACK ON GROUND. PERFORMED AN OPS CHECK OF THE LT PACK, OPS CHECKED GOOD.
- [SDR VNAA2017012300030](https://openairdocs.org/sdr/VNAA2017012300030), Jan 23, 2017: SKIN. DAMAGED. EXTERNAL FUSELAGE SKIN AT BS 235 BETWEEN STRINGERS 26L AND 26R DAMAGED. PERFORMED A MAJOR REPAIR.
- [SDR VNAA2016071800018](https://openairdocs.org/sdr/VNAA2016071800018), Jul 18, 2016: CONTROL UNIT. MALFUNCTIONED. LEFT JET OVERHEAT FAIL MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R FIRE AND OVERHEAT CONTROL UNIT AND 
- [SDR VNAA2016071800017](https://openairdocs.org/sdr/VNAA2016071800017), Jul 18, 2016: OVERHEAT SENSOR. OUT OF POSITION. LEFT JET OVERHEAT FAIL MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED JETPIPE SENSING ELEMENTS AND FOUND LOOP-A SENSING ELE
- [SDR VNAA2016070400005](https://openairdocs.org/sdr/VNAA2016070400005), Jul 4, 2016: AIR FILTER. FAULTY. LEFT HIGH PRESSURE CAUTION MESSAGE AT 8000 FEET. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE LT 10TH STAGE PRESSU
- [SDR VNAA2016062300025](https://openairdocs.org/sdr/VNAA2016062300025), Jun 23, 2016: STRIP. MISSING. ROW EMERGENCY LIGHTS COLOR STRIPPING MISSING. MAINTENANCE INSPECTED, REINSTALLED PHOTOLUMINESCENT FLOOR MARKING AND COVER, AND PERFORMED CHECKS IAW THE AMM. THE
- [SDR VNAA2015091000014](https://openairdocs.org/sdr/VNAA2015091000014), Sep 10, 2015: WINDSHIELD. DELAMINATED. CREW REPORTED SEVERE DELAMINATION ON LT FORWARD WINDSHIELD AND WINDSHIELD ARCING. MAINTENANCE INSPECTED, R & R CAPTAIN’S WINDSHIELD AND PERFORMED CHECKS IAW AMM
- [SDR VNAA2015091000015](https://openairdocs.org/sdr/VNAA2015091000015), Sep 10, 2015: CONTROLLER. FAILED. CREW REPORTED SEVERE DELAMINATION ON LT FORWARD WINDSHIELD AND WINDSHIELD ARCING. MAINTENANCE INSPECTED, R & R CAPTAIN’S WINDSHIELD TEMPERATURE CONTROLLER AND P
- [SDR VNAA2015062800041](https://openairdocs.org/sdr/VNAA2015062800041), Jun 28, 2015: HOSE. LEAKING. ON APPROACH, CREW REPORTED HYD SYS NR 3 LOW PRESSURE MESSAGE CAME ON WHEN LANDING GEAR SELECTED DOWN. CREW LANDED AND USING DIFFERENTIAL BRAKING, TAXIED TO GATE
- [SDR VNAA2015062800040](https://openairdocs.org/sdr/VNAA2015062800040), Jun 28, 2015: HOSE. LEAKING. ON APPROACH, CREW REPORTED HYDRAULIC SYSTEM NR 3 LOW PRESSURE MESSAGE CAME ON WHEN LANDING GEAR SELECTED DOWN. CREW LANDED AND USING DIFFERENTIAL BRAKING, TAXIE
- [SDR VNAA2015032600026](https://openairdocs.org/sdr/VNAA2015032600026), Mar 26, 2015: STRUCTURE. CORRODED. IN PASSENGER COMPARTMENT AT PASSENGER DOOR CUTOUT ON FS 310.00 AND FS 349.00, THE PASSENGER DOOR COUNTER BALANCE ANCHOR FITTING SERATED PLATES HAVE EXFOLIATION 
- [SDR VNAA2014071200006](https://openairdocs.org/sdr/VNAA2014071200006), Jul 12, 2014: SENSOR. MALFUNCTIONED. CREW REPORTED LT 14TH DUCT RED WARNING MESSAGE WHILE DESCENDING THROUGH 14,000 FT. CREW COMPLIED WITH QRH. MESSAGE DID NOT EXTINGUISH IMMEDIATELY, BUT DID EXTIN
- [SDR VNAA2013062800018](https://openairdocs.org/sdr/VNAA2013062800018), Jun 28, 2013: DOWNLOCK SENSOR. FAULTY. CREW REPORTED TRIPLE CHIME AND GEAR DISAGREE AMBER NOSEWHEEL INDICATION ON DESCENT. CREW PERFORMED MANUAL GEAR EXTENSION AND LANDED WITHOUT INCIDENT. MAINTENANC
- [SDR VNAA2013052700016](https://openairdocs.org/sdr/VNAA2013052700016), May 27, 2013: BULKHEAD. CRACKED. DURING SCHEDULED MAINTENANCE FS 621 PRESSURE BULKHEAD HAD INDICATION OF CRACK. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT 
- [SDR VNAA2013052700015](https://openairdocs.org/sdr/VNAA2013052700015), May 27, 2013: STRUCTURE. DAMAGED. DURING SCHEDULED MAINTENANCE FS 589.0 TO FS 605.0 DAMGE WAS FOUND. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED
- [SDR VNAA2013042400017](https://openairdocs.org/sdr/VNAA2013042400017), Apr 24, 2013: LIGHT. INOPERATIVE. EMERGENCY FLOOR LIGHTING AT SEATS 4F/D REPORTED INOPERATIVE. MAINTENANCE INSPECTED, REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHTING AT SEAT 4F/D AND PERFORM
- [SDR VNAA2013042300016](https://openairdocs.org/sdr/VNAA2013042300016), Apr 23, 2013: BATTERY PACK. DISCHARGED. CREW REPORTED EMERGENCY LIGHTS ON THE FLOOR BETWEEN ROWS TWO (2) TO FIVE (5) INTERMITTENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NUMBER TWO (2) EMERGENC
- [SDR VNAA2013031800013](https://openairdocs.org/sdr/VNAA2013031800013), Mar 18, 2013: SEAL. LEAKING. CREW REPORTED RIGHT 14TH DUCT RED MESSAGE DURING FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND RIGHT ENGINE 14TH S
- [SDR VNAA2013022700017](https://openairdocs.org/sdr/VNAA2013022700017), Feb 27, 2013: ENGINE. FAILED. CREW REPORTED A HIGH ITT AND VIBRATION WITH LOSS OF POWER IN NR 2 ENGINE. CREW RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED
- [SDR VNAA2012091600018](https://openairdocs.org/sdr/VNAA2012091600018), Sep 23, 2012: BULKHEAD. CRACKED. DURING SCHEDULED MAINTENANCE FOUND FS 202.75 PRESSURE BULKHEAD WEB CRACKED. FS 202.75 PRESSURE BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANC
- [SDR VNAA2012082100016](https://openairdocs.org/sdr/VNAA2012082100016), Aug 21, 2012: WINDSHIELD. CRACKED. CREW REPORTED THE RIGHT WINDSHIELD CRACKED. AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, AND REPLACED THE RIGHT WINDSHIELD U
- [SDR VNAA2011091500013](https://openairdocs.org/sdr/VNAA2011091500013), Sep 11, 2011: FAIRING. DAMAGED. AT PHL, CREW REPORTED RIGHT WING AFT INBOARD FLAP FAIRING HAD BURN MARK / FRAYING AREA. MAINTENANCE INSPECTED AIRCRAFT AND REPAIRED LIGHTNING STRIKE DAMAGE TO R
- [SDR VNAA2011082500013](https://openairdocs.org/sdr/VNAA2011082500013), Aug 20, 2011: CONNECTOR. LOOSE. CREW REPORTED RANDOM GEAR HORN IN FLIGHT. RED GEAR DISAGREE MESSAGE AND RED NOSE DOOR OPEN MESSAGE REPORTED AFTER SELECTING GEAR DOWN ON APPROACH TO MOB. AIRCRA
- [SDR VNAA2011081000006](https://openairdocs.org/sdr/VNAA2011081000006), Aug 7, 2011: POST. CRACKED. DURING SCHEDULED MAINTENANCE THE VERTICLE POST FS718.0 WAS FOUND CRACKED. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT W
- [SDR VNAA2011081000005](https://openairdocs.org/sdr/VNAA2011081000005), Aug 7, 2011: POST. CRACKED. DURING SCHEDULED MAINTENANCE THE VERTICLE POST FS 409+128 WAS FOUND CRACKED. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAF
- [SDR VNAA2011081000004](https://openairdocs.org/sdr/VNAA2011081000004), Aug 7, 2011: ANGLE. CORRODED. DURING SCHEDULED MAINTENANCE THE FLOORBEAM CAP ANGLE BETWEEN FS 574 AND FS 608 AT LBL 27 WAS FOUND CORRODED. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCR

All 89: https://openairdocs.org/deregistered/N250PS-2025-12-09/reports.md

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