# N244PS: 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: 7912
- Year built: 2004
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 16, 2004
- Certificate issued: April 11, 2023
- Last registry action: May 1, 2023
- Mode S code: A24031
- 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/N244PS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=244PS
- Page: https://openairdocs.org/deregistered/N244PS-2025-12-09

From the FAA registry file of November 4, 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 (90, newest 50)

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

- [SDR VNAA2022012011101](https://openairdocs.org/sdr/VNAA2022012011101), Dec 30, 2019: FAIRING. BENT. UPPER FWD CORE COWL HINGE NOT PINNED CORRECTLY. NO. 2 ENGINE EXHAUST NOZZLE FAIRINGÏ¿½S ACCESS PANEL WAS FOUND TO BE BENT AND TWISTED. PLACED ON TEMP REPAIR REF
- [SDR VNAA2019103011102](https://openairdocs.org/sdr/VNAA2019103011102), Oct 30, 2019: INVERTER. FAILED. R/H OVERWING EMERGENCY "EXIT: SIGN NOT WORKING. R/R INVERTER FOR RH OVERWING LOWER EMERGENCY EXIT SIGN. OPS CHECK GOOD.
- [SDR VNAA2019092711103](https://openairdocs.org/sdr/VNAA2019092711103), Sep 27, 2019: CABLE. FRAYED. DOOR SUPPORT WHEEL CABLE ON AFT SIDE OF PAX DOOR IS HEAVILY FRAYED REMOVED AND REPLACED MAIN CABIN DOOR LOWER SUPPORT WHEEL CABLE NO FURTHER DEFECTS NOTED AT TH
- [SDR VNAA2019062211102](https://openairdocs.org/sdr/VNAA2019062211102), Jun 22, 2019: RING. WORN. RIGHT ENGINE OIL PRESSURE MSG IN FLIGHT. O/S MX SERVICED RT ENGINE WITH 6.0 QTS. GOING TO PROCEED WITH OIL CONSUMPTION RUN. FAILED OIL CONSUMPTION RUN. .75QTS A
- [SDR VNAA2019100217101](https://openairdocs.org/sdr/VNAA2019100217101), Mar 17, 2019: SIGN. INOPERATIVE. RH EXTERNAL MIDDLE OVERWING EMERGENCY LIGHT INOP. PERFORMED OPS CHECK ON RH EMRGENCY EXIT LOWER SIGN. IAW CRJ200 AMM 33-51-00-710-801. OPS CHECK GOOD AT THIS TI
- [SDR VNAA2019031211101](https://openairdocs.org/sdr/VNAA2019031211101), Mar 12, 2019: WINDSHIELD. CRACKED. RIGHT AFTER DEPARTURE FROM DCA FLIGHT 5484 GOT A SHATTERED CA WINDSHIELD AT ABOUT FL098 A EMERGENCY WAS DECLARED BY THE CREW WHEN RETURNING BACK TO DCA. THEY DI
- [SDR VNAA2018110899912](https://openairdocs.org/sdr/VNAA2018110899912), Nov 8, 2018: FITTING. CRACKED. WINDSHIELD CNTR POST R/H BOTTOM FITTING CRACKED FROM LOWER FASTENER HOLE TO EDGE OF FITTING. C/A:REMOVED UNSERVICEABLE CENTER POST IAW CRJ 200 SRM 51-42-21. REC
- [SDR VNAA2018110899911](https://openairdocs.org/sdr/VNAA2018110899911), Nov 8, 2018: SUPPORT BRACKET. BROKEN. SUPPORT BRACKET AND CLIP FOR LH UPPER STANG FAIRING IS BROKEN ON PYLON TRACK. C/A: REMOVED AND REPLACED SUPPORT ASSY IAW CRJ200 SRM 51-42-06.
- [SDR VNAA2018110899910](https://openairdocs.org/sdr/VNAA2018110899910), Nov 8, 2018: CASCADE. CRACKED. UPPER CENTER CASCADE CRACKED ON LH THRUST REVERSER ASSY MARKED WITH TAPE. C/A: REMOVED L/H TR UPPER CENTER CASCADE IAR CRJ200 AMM 78-33-01-000-801. INSTALLED L/
- [SDR VNAA2018110899909](https://openairdocs.org/sdr/VNAA2018110899909), Nov 8, 2018: ANGLE. CRACKED. FS.280 CROSSBEAM IS CORRODED BETWEEN LBL9 AND RBL9. FOUND 4EA FS280 CLIPS TO BE CRACKED BETWEEN LBL9 AND RBL9. C/A: FABRICATED 4 EA F.S. 280 CLIPS REFERENCING R
- [SDR VNAA2018110899908](https://openairdocs.org/sdr/VNAA2018110899908), Nov 8, 2018: CARGO TRACK. CORRODED. AFT CARGO COMPARTMENT, SEAT TRACK @ RBL9, APPROX. F.S. 559.00+80 CORRODED. C/A: REMOVED AN REPLACED DAMAGED SEAT TRACK AT @FS559.00+80 LBL 9 NEW SEAT TRACK IAW 
- [SDR VNAA2018110899907](https://openairdocs.org/sdr/VNAA2018110899907), Nov 8, 2018: CARGO TRACK. CORRODED. AFT CARGO COMPARTMENT, SEAT TRACK @ LBL9, APPROX. F.S. 559.00+80 CORRODED. C/A: REMOVED AN REPLACED DAMAGED SEAT TRACK AT @FS559.00+80 LBL 9 NEW SEAT TRACK IAW 
- [SDR VNAA2018110899906](https://openairdocs.org/sdr/VNAA2018110899906), Nov 8, 2018: SEAT TRACK. CORRODED. SEAT RAIL AT LBL27, APPROX F.S. 559.00+80 CORRODED. C/A: REMOVED AND REPLACED DAMAGED SEAT TRACK AT F 559.00+80 LBL 27. INSTALLED NEW SEAT TRACK IAW CRJ 200 AMM
- [SDR VNAA2018110899905](https://openairdocs.org/sdr/VNAA2018110899905), Nov 8, 2018: CARGO TRACK. BROKEN. AFT CARGO COMPARTMENT TWO SEAT TRACK FILLERS BROKEN. K.LONG 10/22/18. C/A: INSTALLED 3 EACH NEW SERVICEABLE SEAT TRACK FILLERS P/N:601R38731-7, 601R38731-17 AND
- [SDR VNAA2018110899904](https://openairdocs.org/sdr/VNAA2018110899904), Nov 8, 2018: CARGO TRACK. CORRODED. AFT CARGO COMPARTMENT, SEAT TRACK @ RBL9, APPROX. F.S.559.00+112 CORRODED. C/A: REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK P/N: 601R38779-49 IAW CRJ200 AMM
- [SDR VNAA2018110899903](https://openairdocs.org/sdr/VNAA2018110899903), Nov 8, 2018: CARGO TRACK. CORRODED. AFT CARGO COMPARTMENT SEAT TRACK @ LBL9, APPROX. F.S. 559.00+112 CORRODED. C/A: REMOVED SEAT TRACK AND REPLACED SEAT TRACK, P/N 601R38779-S, IAW CRJ200 AMM 53-0
- [SDR VNAA2018110899902](https://openairdocs.org/sdr/VNAA2018110899902), Nov 8, 2018: SEAT TRACK. CORRODED. SEAT TRACK ON RBL9 BETWEEN FS.559+16 TO FS.559+80 IS CORRODED. C/A: NSTALLED NEW SERVICEABLE SEAT TRACK ON RBL9 BETWEEN FS559.00+16 - FS559.00+80 IAW CRJ200 AMM
- [SDR VNAA2018110899901](https://openairdocs.org/sdr/VNAA2018110899901), Nov 8, 2018: DOOR FRAME. CRACKED. R/H OVERWING DOOR CUTOUT HAS CRACKED/ MISSING STRUCTUAL FILLER FOR DOOR SEAL LANDING. C/A: REPAIRED RH OVERWING DOOR CUTOUT MISSING STRUCTURAL FILLER IAW SRM 51
- [SDR VNAA2018111199901](https://openairdocs.org/sdr/VNAA2018111199901), Oct 11, 2018: FRAME. CRACKED. FS718 FRAME IS CRACKED AT STGR 11R. C/A: REMOVED FRAME AT R/H FS718 AND COMPLETED INSTALLATION OF FRAME AT FS718 IAW CRJ 200 SRM 51-42-06 AND 51-42-21.
- [SDR VNAA20191108101](https://openairdocs.org/sdr/VNAA20191108101), Aug 28, 2018: WINDSHIELD. CRACKED. SUPPLEMENTAL INFORMATION: MX REPLACED FO WINDSHIELD. REMOVED & REPLACED RH WINDSHIELD HEAT CONTROLLER. OPS CHECK GOOD. P/N 1659-1 S/N 4643
- [SDR VNAA2018083081101](https://openairdocs.org/sdr/VNAA2018083081101), Aug 28, 2018: WINDSHIELD. FAILED. THE CREW REPORTED THE FIRST OFFICER'S WINDSHIELD SHATTERED IN FLIGHT, AFTER THEY RECEIVED A WINDSHIELD HEAT CUATION MESSAGE. DECLARED AN EMERGENCY AND DIVERTED.
- [SDR VNAA2018040111101](https://openairdocs.org/sdr/VNAA2018040111101), Apr 1, 2018: WARNING MESSAGE. FALSE ACTIVATION. DECLARED AN EMERGENCY ON APPROACH FOR A 14TH STAGE BLEED AIR WARNING. MAINTENANCE INSPECTED LOOPS AND NO DEFECTS WERE FOUND, OPS CHECKED GOOD. NO ABNORMAL INDIC
- [SDR VNAA20170606MOC01](https://openairdocs.org/sdr/VNAA20170606MOC01), Jun 6, 2017: OIL SYSTEM. FLUCTUATES. ON APPROACH, CREW DECLARED AN EMERGENCY DUE TO RT ENGINE OIL PRESSURE FLUCUATED AND JUST BEFORE TOUCHDOWN GOT A RT ENGINE OIL LOW PRESSURE WARNING MESSAGE.
- [SDR VNAA2017012400034](https://openairdocs.org/sdr/VNAA2017012400034), Jan 24, 2017: COVER. BROKEN. ROW 1 EMERGENCY LIGHT COVER BROKEN. REPLACED THE TRACK COVER, STRAIGHTENED PINS ON FORWARD EMERGENCY TRACK LIGHTING CONNECTOR AND CONNECTED.
- [SDR VNAA2017011600022](https://openairdocs.org/sdr/VNAA2017011600022), Jan 16, 2017: WIRE HARNESS. DEFECTIVE. PASSENGER DOOR LATCH CAUTION MESSAGE DURING FLIGHT. REMOVED AND REPLACED THE PASSENGER DOOR WIRE HARNESS, OPS CHECKED GOOD.
- [SDR VNAA2016102900036](https://openairdocs.org/sdr/VNAA2016102900036), Oct 29, 2016: BULKHEAD WEB. CRACKED. BS 621 PRESSURE BULKHEAD WEB IS CRACKED IN 4 PLACES. MAINTENANCE PERFORMED A MAJOR REPAIR.
- [SDR VNAA2016091300010](https://openairdocs.org/sdr/VNAA2016091300010), Sep 13, 2016: SENSOR. FAULTY. RIGHT ENGINE 14TH STAGE BLEED WARNING MESSAGE. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, RE
- [SDR VNAA2015090200002](https://openairdocs.org/sdr/VNAA2015090200002), Sep 2, 2015: ANTI-ICE VALVE. FAILED. CREW REPORTED RT COWL ANTI-ICE CAUTION MESSAGE. CREW RAN QRH, MESSAGE PERSISTED IN FLIGHT WITH COWL ANTI-ICE SELECTED OFF. CREW RETURNED TO FIELD AND LANDED WIT
- [SDR VNAA2015090100001](https://openairdocs.org/sdr/VNAA2015090100001), Sep 1, 2015: PRESSURE SWITCH. FAILED. CREW REPORTED RT COWL ANTI-ICE CAUTION MESSAGE IN FLIGHT WITH ANTI-ICE SELECTED OFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT
- [SDR VNAA2015083100039](https://openairdocs.org/sdr/VNAA2015083100039), Aug 31, 2015: WARNING MESSAGE. FALSE ACTIVATION. CREW REPORTED APU OIL PRESSURE CAS MESSAGE DURING CRUISE FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE VERIFIED APU OIL LEVEL AS FULL AND OIL P
- [SDR VNAA2015010100001](https://openairdocs.org/sdr/VNAA2015010100001), Jan 1, 2015: CONNECTOR. UNSECURE. CREW REPORTED ROW 6-8 EMERGENCY LIGHTS AND EMERGENCY DOOR LIGHT INOPERATIVE. MAINTENANCE INSPECTED AND SECURED CONNECTOR AND PERFORMED CHECKS IAW AMM. ACFT RELE
- [SDR VNAA2014121100003](https://openairdocs.org/sdr/VNAA2014121100003), Dec 11, 2014: STRINGER. CRACKED. STRINGER 3L FWD OF BS 379 HAS .500 INCH CRACK. REPAIRED THE STRINGER IAW SRM, 53-00-03, SPLICE REPAIR FIG 202, SHEET 1.
- [SDR VNAA2014121900005](https://openairdocs.org/sdr/VNAA2014121900005), Dec 4, 2014: SKIN. DENTED. LEFT INBD GROUND SPOILER, INBD LOWER CORNER DENTED 5" LONG AND 2" WIDE. REPAIRED IAW EO CL600-2B19-57-L02986.
- [SDR VNAA2014061300011](https://openairdocs.org/sdr/VNAA2014061300011), Jun 13, 2014: PUMP. FAILED. CREW REPORTED, NR 1 HYD SYSTEM FAILED IN FLIGHT WITH NO PRESSURE AND NO FLUID LEVELS. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFO
- [SDR VNAA2014050800006](https://openairdocs.org/sdr/VNAA2014050800006), May 8, 2014: CONTROL UNIT. FAILED. CREW REPORTED STAB CHANNEL ONE INOPERATIVE MESSAGE DURING FLIGHT. ENGAGED SYSTEM AND BOTH STAB TRIM AND MACH TRIM WENT INOPERATIVE. CREW FOLLOWED QRH TO RE-ENGA
- [SDR VNAA2013092400011](https://openairdocs.org/sdr/VNAA2013092400011), Sep 24, 2013: OIL SYSTEM. LOW PRESSURE. CREW REPORTED LT ENGINE OIL PRESSURE AMBER DURING TAKEOFF ABOVE 80 KTS AND FOR FIRST 3 MINUTES AFTER TAKEOFF. MAXIMUM PSI OBSERVED WAS 150 PSI. CREW RETURNED TO
- [SDR VNAA2013082900018](https://openairdocs.org/sdr/VNAA2013082900018), Aug 29, 2013: SKIN. DAMAGED. DURING SCHEDULED MX, THE RT LOWER WING PLANK CHAFE DAMAGE WAS FOUND. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2013082900017](https://openairdocs.org/sdr/VNAA2013082900017), Aug 29, 2013: SKIN. DAMAGED. DURING SCHEDULED MX, THE LT LOWER WING PLANK CHAFE DAMAGE WAS FOUND. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2013062800019](https://openairdocs.org/sdr/VNAA2013062800019), Jun 28, 2013: CONTROL UNIT. FAILED. CREW REPORTED STAB TRIM CAUTION MESSAGE AND RUNAWAY DURING CLIMB. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLA
- [SDR VNAA2013031800017](https://openairdocs.org/sdr/VNAA2013031800017), Mar 18, 2013: RING. DAMAGED. CREW REPORTED POSSIBLE LIGHTNING STRIKE IN FLIGHT AT 17,000 FEET. AIRCRAFT IN CLEAN CONFIGURATION. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED L
- [SDR VNAA2013021000009](https://openairdocs.org/sdr/VNAA2013021000009), Feb 10, 2013: WARNING SYSTEM. FALSE ACTIVATION. CREW REPORTED GEN 2 AMBER CAS MESSAGE ON CLIMBOUT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT USING FIM (FAULT ISOLATION MANUAL
- [SDR VNAA2012050800010](https://openairdocs.org/sdr/VNAA2012050800010), May 8, 2012: DISPLAY. DIRTY. CREW REPORTED CAPTAIN’S PFD DISPLAY TEMP MESSAGE AND FIRST OFFICER’S PFD AND MFD DISPLAY TEMP MESSAGES DURING FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT.
- [SDR VNAA2012050300004](https://openairdocs.org/sdr/VNAA2012050300004), May 3, 2012: RADOME. DAMAGED. CREW REPORTED TOP STATIC WICK ON LEFT WINGLET MISSING, WITH SOME BURN DAMAGE VISIBLE. CREW ALSO REPORTED POSSIBLE LIGHTNING STRIKE DAMAGE TO TAIL CONE. MAINTENA
- [SDR VNAA2011112000001](https://openairdocs.org/sdr/VNAA2011112000001), Nov 21, 2011: BULKHEAD. CRACKED. DURING SCHEDULED MAINTENANCE THE FS 621 BULKHEAD WEB WAS FOUND CRACKED. THE FS 621.0 BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS.
- [SDR VNAA2011111500011](https://openairdocs.org/sdr/VNAA2011111500011), Nov 15, 2011: FLOORBEAM. CRACKED. DURING SCHEDULED MAINTENANCE THE FS 280.0 FLOOR TRAVERSE BEAM WAS FOUND CRACKED. THE FS 280.0 FLOOR TRAVERSE BEAM WAS INSPECTED AND REPAIRED USING AIRCRAFT MAIN
- [SDR VNAA2011102100019](https://openairdocs.org/sdr/VNAA2011102100019), Oct 17, 2011: TRANSDUCER. MALFUNCTIONED. CREW REPORTED LEFT ENGINE LOW OIL PRESSURE 40 TO 22 PSI AT ALL POWER SETTINGS AFTER DEPARTURE FROM DAY. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTE
- [SDR VNAA2011101900014](https://openairdocs.org/sdr/VNAA2011101900014), Oct 13, 2011: SCAVENGE PUMP. MALFUNCTIONED. CREW REPORTED LEFT OIL PRESSURE DROPPED FROM 70 PSI TO 48 PSI ON TAKEOFF ROLL ON DEPARTURE FROM CLT. LEFT HAND OIL PRESSURE DROPPED TO 39 PSI AT 2,000 FEET. CRE
- [SDR VNAA2011092900023](https://openairdocs.org/sdr/VNAA2011092900023), Sep 25, 2011: BPSU. FAILED. CREW REPORTED FLAPS FAIL AMBER CAS MESSAGE IN FLIGHT EN ROUTE FROM CAK TO CLT. CREW DIVERTED TO GSO AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SY
- [SDR VNAA2011092800022](https://openairdocs.org/sdr/VNAA2011092800022), Sep 23, 2011: ECU. FAILED. CREW REPORTED FLAPS FAIL CAUTION MESSAGE AT ZERO DEGREES ON DESCENT INTO SDF. AIRCRAFT LANDED IN SDF WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMO
- [SDR VNAA2011091900019](https://openairdocs.org/sdr/VNAA2011091900019), Sep 14, 2011: BPSU. FAILED. CREW REPORTED FLAPS FAIL CAUTION MESSAGE IN FLIGHT ON DESCENT INTO CLT. CREW COMPLETED QRH AND AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT 

All 90: https://openairdocs.org/deregistered/N244PS-2025-12-09/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 CHI06IA011](https://openairdocs.org/ntsb/CHI06IA011), Oct 17, 2005: Bombardier CL-600-2B19 (N244PS), West Grove, PA, incident, minor damage. Probable cause: The separation of the left engine exhaust nozzle during cruise climb due to inadequately designed attachment hardware.

## FAA accident and incident reports (2)

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 20100406055419I](https://openairdocs.org/incident/20100406055419I), Apr 6, 2010: Bombardier CL-600-2B19 (N244PS), Carlotte, NC, Minor damage. The left engine, general electric , CF34-3B1, serial number GE-E950043 suffered contained fan blade area failure after departing clt and climbing out at…
- [Incident 20051017032629I](https://openairdocs.org/incident/20051017032629I), Oct 17, 2005: Cndair CL6002B19 (N244PS), West Grove, PA, Substantial damage. (-23) A [privacy data omitted] reported to this office that he found an aircraft part in his back yard on 17 oct, 2005. A loud noise awoke him at approx 0030…

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