# N215PS: 2003 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: 7880
- Year built: 2003
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 16, 2003
- Certificate issued: June 8, 2023
- Last registry action: June 9, 2023
- Mode S code: A1CD6B
- 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/N215PS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=215PS
- Page: https://openairdocs.org/deregistered/N215PS-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 (67, newest 50)

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

- [SDR VNAA2020022311101](https://openairdocs.org/sdr/VNAA2020022311101), Feb 23, 2020: INVERTER. FAILED. R&R #2 EMERGENCY LIGHT INVERTER IAW CRJ 200 AMM 33-51-07-000/400-801 OPS CHECK GOOD AT THIS TIME.
- [SDR VNAA2020021399908](https://openairdocs.org/sdr/VNAA2020021399908), Feb 13, 2020: INTERCOSTAL. CRACKED. LH UPPER INTERCOSTAL FROM FS 621 TO FS 625, BL 45, STR 14L, WL 97.5 IS CRACKED APPROX 0.5" LONG. R.CHEUVRONT 1/12/20 (PCC) M/A: 1. REMOVED INTERCOSTAL IAW CRJ 2
- [SDR VNAA2020021399907](https://openairdocs.org/sdr/VNAA2020021399907), Feb 13, 2020: BULKHEAD WEB. CRACKED. 5 EA AREAS OF CRACK INDICATIONS NOTED ON FS 621 RPB WEB IN THE HEEL LINE AREA OF VERT POST. 1ST AREA AT RBL 9 WL 127 - 132.5 50% FSH, SECOND AREA AT RBL 9 WL 11
- [SDR VNAA2020021399906](https://openairdocs.org/sdr/VNAA2020021399906), Feb 13, 2020: POST. CRACKED. ONE CRACK ON LH WINDISHIELD SIDE POST LOWER AFT ATTACH FITTING IN RADIUS 0.150" LONG. MARKED ON A/C IN RED SHARPIE. REMOVED DAMAGED LH WINDSHIELD SIDE POST LOWE
- [SDR VNAA2020021399905](https://openairdocs.org/sdr/VNAA2020021399905), Feb 13, 2020: POST. CRACKED. ONE CRACK INDICATION NOTED ON LH WINDSHIELD SIDE POST AT LOWER C/B FASTENER APPROX 1.500" LONG BY 100% FSH. FAILED NDT INSP. MARKED ON A/C WIHT SHARPIE. B.FLEEM
- [SDR VNAA2020021399904](https://openairdocs.org/sdr/VNAA2020021399904), Feb 13, 2020: STRAP. CORRODED. FS 559 FLOOR SUPPORT STRAP CORRODED BETWEEN LBL 45 AND LBL 27. REMOVED SUPPORT STRAP BETWEEN LBL 45 AND LBL 27 IAW CRJ 200 SRM 51-42-06. LOCATED AND DRILLED NEW
- [SDR VNAA2020021399903](https://openairdocs.org/sdr/VNAA2020021399903), Feb 13, 2020: STRAP. CORRODED. FS 559 FLOOR SUPPORT STREP CORRODED BETWEEN RBL 27 AND RBL 45. REMOVED FLOOR SUPPORT STRAP BETWEEN RBL 27 AND RBL 45 IAW SRM 51-42-06. LOCATED AND DRILLED NEW S
- [SDR VNAA2020021399902](https://openairdocs.org/sdr/VNAA2020021399902), Feb 13, 2020: FRAME. CORRODED. DEEP CORROSION ON LH FS 513 FRAME AFT FREE FLANGE JUST ABOVE FLOOR IN 1" AREA AT CORNER OF PART. MARKED WITH TAPE. BLOCKED OUT CORROSION ON FRAME, BLEND OUT IS 
- [SDR VNAA2020021399901](https://openairdocs.org/sdr/VNAA2020021399901), Feb 13, 2020: ATTACH ANGLE. CRACKED. PAX DOOR MOTOR BOTTOM ATTACH ANGLE CRACKED. DISPLACED POWER ASSIST MOTOR FOR ACCESS. CANON PLUG WAS NOT DISCONNECTED. REINSTALLED PAX DOOR MOTOR ASSIST IAW CRJ2
- [SDR VNAA2019123081103](https://openairdocs.org/sdr/VNAA2019123081103), Dec 28, 2019: CONTACT. DIRTY. LOWER EMERGENCY EXIT LIGHT INOPERATIVE ON THE L/H SIDE BY THE EMERGENCY DOOR. REMOVED EMERGENCY LIGHT, CLEANED CONTACTS, AND REINSTALLED EMERGENCY LIGHT IAW AMM
- [SDR VNAA2019120541101](https://openairdocs.org/sdr/VNAA2019120541101), Dec 4, 2019: WARNING MESSAGE. FALSE ACTIVATION. FLIGHT 5663 DCA/CLE DIVERTED TO CMH DUE TO MAINTENANCE. IN FLIGHT WHILE ON DESCENT INTO CLE ANTI-ICE CAUTION MESSAGE ALERT. CREW RAN QRH AND CAUTION MESSAGE EXT
- [SDR VNAA2019042641101](https://openairdocs.org/sdr/VNAA2019042641101), Apr 24, 2019: COMPUTER. FAILED. EMERGENCY DECLARED DUE TO LT AND TOTAL FUEL READOUT DASHED OUT DURING CRUISE. CAPTAIN CONTINUED FLT AND LANDED SAFELY. READOUTS REMAINED DASHED OUT FOR THE REST
- [SDR VNAA2017121399908](https://openairdocs.org/sdr/VNAA2017121399908), Dec 13, 2017: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 27.50 WL83; BL0 WL114; RBL 18 WL 113; RBL 27.5 WL 87; RBL 27.5 WL 132; BL 0 WL 132. C/A: 
- [SDR VNAA2017121399907](https://openairdocs.org/sdr/VNAA2017121399907), Dec 13, 2017: FRAME. CORRODED. FRAME FS 605, LOWER SECTOR, 27-26L FWD FLANGE IS CORRODED. C/A: INSTALLED FRAME SECTOR @ FS 605 IAW CRJ 200 SRM 51-42-06 AND 51-42-21.
- [SDR VNAA2017121399906](https://openairdocs.org/sdr/VNAA2017121399906), Dec 13, 2017: STRAP. CORRODED. RIGHT FLOORBEAM STRAP AT FS 559 BETWEEN RBL 27 AND RBL 43 IS CORRODED.C/A: INSTALLED NEW SERVICEABLE STRAP IAW CRJ 200 SRM 51-42-06 & 51-42-15.
- [SDR VNAA2017121399905](https://openairdocs.org/sdr/VNAA2017121399905), Dec 13, 2017: STRAP. CORRODED. LEFT FLOORBEAM STRAP AT FS 559 BETWEEN LBL 27 AND LBL 43 IS CORRODED. C/A: LOCATED, DRILLED AND INSTALLED LEFT FLOOR SUPPORT STRAP AT FS 559 BETWEEN LBL 27 AND 
- [SDR VNAA2017121399904](https://openairdocs.org/sdr/VNAA2017121399904), Dec 13, 2017: FRAME. CRACKED. FUSELAGE FS 333.0 FRAME IS CRACKED BETWEEN STGR0 AND STGR 1L. C/A: REMOVED AND REPLACED CRACKED FRAME SECTOR BETWEEN STGR 0 AND STGR 1L @ FUSELAGE FS 333.0 IAW 
- [SDR VNAA2017121399903](https://openairdocs.org/sdr/VNAA2017121399903), Dec 13, 2017: FRAME. CRACKED. FUSELAGE FS 718 FRAME IS CRACKED AT STGR 11R. C/A: INSTALLED NEW PART F.S 718 P/N 600-36030-24 IAW CRJ200 SRM 51-42-06, 51-42-21, AND 51-41-00.
- [SDR VNAA2017121399902](https://openairdocs.org/sdr/VNAA2017121399902), Dec 13, 2017: FRAME. CORRODED. PASSENGER DOOR INTERNAL FRAME CORRODED. LOCATED AT CENTER-LINE JUST BELOW PASSENGER DOOR HANDLE HOUSING. C/A: INSTALLED NEW FRAME IAW CRJ200 SRM 51-42-06 AND 51
- [SDR VNAA2017121399901](https://openairdocs.org/sdr/VNAA2017121399901), Dec 13, 2017: VANE CAP. CHAFED. RH INBD FLAP VANE SKIN IS CHAFED AT TWO LOCATIONS (MIDDLE AND INBD). C/A: INSTALLED SERVICEABLE LEADING EDGE. P/N 601R14303-52S & -54S IAW CRJ 200 SRM 51-40-11,
- [SDR VNAA2017072611101](https://openairdocs.org/sdr/VNAA2017072611101), Jul 26, 2017: CARBON SEAL. LEAKING. ON FLIGHT LEVEL 270, THE AIRCRAFT LOST THE RIGHT ENGINE OIL PRESSURE. THEY DECENDED TO FLIGHT LEVEL 170 WHERE THEY CONTINUED TO LOSE OIL PRESSURE, AND SHUT DOWN
- [SDR VNAA2016121200023](https://openairdocs.org/sdr/VNAA2016121200023), Dec 12, 2016: WIRE HARNESS. FAULTY. EMERGENCY FLOOR LIGHTS ON ROW 1 THROUGH 5 INOPERATIVE. REMOVED AND REPLACED WIRING HARNESS.
- [SDR VNAA2016062800032](https://openairdocs.org/sdr/VNAA2016062800032), Jun 28, 2016: CONTROL UNIT. FAULTY. HORIZONTAL STABILIZER TRIM CONTOL UNIT FLAGGING MOTOR NR 1 DURING CLIMBOUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R &
- [SDR VNAA2016020700013](https://openairdocs.org/sdr/VNAA2016020700013), Feb 7, 2016: BOTTLE. LOW PRESSURE. CREW REPORTED OXYGEN LOW PRESSURE CAUTION MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, SERVICED CREW OXYGEN SYS AND PERF
- [SDR VNAA2015020500002](https://openairdocs.org/sdr/VNAA2015020500002), Feb 5, 2015: PROXIMITY SENSOR. CONTAMINATED. CREW REPORTED STEERING INOPERATIVE AND WEIGHT ON WHEELS, INPUT CAUTION MESSAGES JUST AFTER ROTATION. MESSAGE CLEARED WHEN GEAR WAS SELECTED DOWN. CREW RETURNED 
- [SDR VNAA2014102800018](https://openairdocs.org/sdr/VNAA2014102800018), Oct 28, 2014: ELEMENT. OUT OF POSITION. CREW REPORTED RIGHT FOURTEENTH DUCT MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND RT FOURTEENTH PYLON L
- [SDR VNAA2014102800017](https://openairdocs.org/sdr/VNAA2014102800017), Oct 28, 2014: RESERVOIR. LEAKING. CREW REPORTED LOSS OF FLUID FROM HYDRAULIC SYSTEM NR 2 WITH QUANTITY AT ZERO PERCENT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED,
- [SDR VNAA2014041100011](https://openairdocs.org/sdr/VNAA2014041100011), Apr 11, 2014: COMPUTER. FAULTED. DURING CRUISE AT FL290 AND WITH APU OFF, CREW REPORTED YAW DAMPER NR 2 AND AUTOPILOT WENT OFF AND EFIS COMPUTER MONITOR MESSAGE AND HDG AND PIT BOXES DISPLAYED.
- [SDR VNAA2014032900021](https://openairdocs.org/sdr/VNAA2014032900021), Mar 29, 2014: FEEDER CABLE. DAMAGED. CREW REPORTED FLOOR EMERGENCY LIGHTS WOULD NOT ILLUMINATE PAST ROW 8. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHT CABLE ASSEMBLY IN FRONT OF LAVATORY AND PERFO
- [SDR VNAA2014032300019](https://openairdocs.org/sdr/VNAA2014032300019), Mar 23, 2014: CARGO TRACK. CORRODED. DURING SCHEDULED MAINTENANCE, AT THE CARGO COMPARTMENT FLOOR TRACKS AND TIE DOWNS CORROSION WAS FOUND. THE AREA WAS INSPECTED AND TRACKS AND TIEDOWNS REPLACED U
- [SDR VNAA2014032300018](https://openairdocs.org/sdr/VNAA2014032300018), Mar 23, 2014: SILL. CORRODED. DURING SCHEDULED MAINTENANCE, AT THE CARGO DOOR LOWER SILL CORROSION WAS FOUND AROUND FASTENER HOLES. THE AREA WAS INSPECTED AND CARGO DOOR SILL WAS REPLACED US
- [SDR VNAA20130323](https://openairdocs.org/sdr/VNAA20130323), Mar 23, 2014: SILL. CORRODED. DURING SCHEDULED MAINTENANCE, AT THE CARGO DOOR LOWER SILL CORROSION WAS FOUND AROUND FASTENER HOLES. THE AREA WAS INSPECTED AND CARGO DOOR SILL WAS REPLACED US
- [SDR VNAA2014032300017](https://openairdocs.org/sdr/VNAA2014032300017), Mar 23, 2014: SKIN. CRACKED. DURING SCHEDULED MAINTENANCE, SKIN AT FS 235 WAS FOUND CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014032300016](https://openairdocs.org/sdr/VNAA2014032300016), Mar 23, 2014: SKIN. DAMAGED. DURING SCHEDULED MAINTENANCE, AREA AFT OF NOSE LANDING GEAR DAMAGED, CAUSED BY LIGHTNING STRIKE. THE AREA WAS INSPECTED AND REPAIRED USING AMM. A PERMANENT REPA
- [SDR VNAA2014032300015](https://openairdocs.org/sdr/VNAA2014032300015), Mar 23, 2014: SKIN. CRACKED. DURING SCHEDULED MAINTENANCE, THE RT FORWARD CABIN WINDOW SKIN CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014010500003](https://openairdocs.org/sdr/VNAA2014010500003), Jan 3, 2014: CONTROLLER. FAILED. CREW REPORTED CAPTAIN’S WINDSHIELD CRACKED AT FL29. DESCENDED, DECLARED AN EMERGENCY AND LANDED AT NEAREST SUITABLE AIRPORT WITHOUT INCIDENT. MAINTENANCE INSPEC
- [SDR VNAA2013090800004](https://openairdocs.org/sdr/VNAA2013090800004), Sep 8, 2013: RELAY. FAILED. CREW REPORTED ODOR OF BURNING RUBBER NEAR EXIT ROW. LIGHTS OUT ABOVE BINS ON ROW 8 D/F. MX INSPECTED, R & R POWER RELAY AT ROW 8 D/F AND PERFORMED CHECKS IAW AM
- [SDR VNAA2013053100018](https://openairdocs.org/sdr/VNAA2013053100018), May 31, 2013: FUEL CONTROL. FAILED. CREW REPORTED RIGHT ENGINE OVERSPEED MASTER WARNING MESSAGE BELOW 80 KNOTS ON TAKEOFF. CREW REJECTED TAKEOFF AND SAFELY RETURNED TO GATE. MAINTENANCE INSPECTED,
- [SDR VNAA2013031100008](https://openairdocs.org/sdr/VNAA2013031100008), Mar 11, 2013: CONTROLLER. FAILED. CREW REPORTED RIGHT AOA HEAT, RIGHT PITOT HEAT, RIGHT TAT PROBE HEAT AND RIGHT STATIC HEAT CAS MESSAGES AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT
- [SDR VNAA2013030600007](https://openairdocs.org/sdr/VNAA2013030600007), Mar 6, 2013: ENGINE. MALFUNCTIONED. CREW REPORTED LEFT ENGINE OIL PRESSURE CLIMBED TO APPROXIMATELY 133 PSI ON TAKEOFF ROLL. CREW REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED, REMO
- [SDR VNAA2012093000024](https://openairdocs.org/sdr/VNAA2012093000024), Sep 30, 2012: BULKHEAD. CRACKED. DURING SCHEDULED MAINTENANCE FOUND A CRACK AT THE FS 621 BULKHEAD WEB. THE FS 621 BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AI
- [SDR VNAA2012093000023](https://openairdocs.org/sdr/VNAA2012093000023), Sep 30, 2012: BULKHEAD. CRACKED. DURING SCHEDULED MAINTENANCE A CRACK AT FS 202.0 BULKHEAD WAS FOUND. THE FS 202.0 BULKHEAD WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRA
- [SDR VNAA2012081200005](https://openairdocs.org/sdr/VNAA2012081200005), Aug 12, 2012: CONTROL UNIT. FAILED. CREW REPORTED, STEERING INOP MESSAGE ON GEAR EXTENSION. CREW RESET NOSEWHEEL STEERING IN ACCORDANCE WITH QRH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TR
- [SDR VNAA2011110200031](https://openairdocs.org/sdr/VNAA2011110200031), Oct 30, 2011: SKIN. DENTED. CREW REPORTED BIRD STRIKE ON RIGHT WING LEADING EDGE ON APPROACH TO PHL. AIRCRAFT LANDED IN PHL WITHOUT FURTHER INCIDENT. MAINTENANCE COMPLIED WITH BIRD STRIKE 
- [SDR VNAA2011100600007](https://openairdocs.org/sdr/VNAA2011100600007), Oct 2, 2011: SKIN. DAMAGED. AT GSP, CREW REPORTED BIRD STRIKE ON LEADING EDGE OF LEFT WING. MAINTENANCE INSPECTED AIRCRAFT, REPAIRED DENT ON LEFT WING INBOARD LEADING EDGE (L/E ZONE 1) AND
- [SDR VNAA2011060300023](https://openairdocs.org/sdr/VNAA2011060300023), May 28, 2011: ACM. SEIZED. CREW REPORTED STRONG ELECTRICAL SMOKE SMELL IN CABIN AT PHL. GROUND PERSONNEL WITNESSED WHITE SMOKE IN VICINITY OF PACK EXHAUST VENTS. MAINTENANCE INSPECTED, RE
- [SDR VNAA2011060300022](https://openairdocs.org/sdr/VNAA2011060300022), May 27, 2011: BRACKET. DAMAGED. CREW REPORTED WOW INPUT MESSAGE WITH GEAR IN WELL, THEN STEERING INOP CAS MESSAGE, AFTER TAKEOFF FROM DAY. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAI
- [SDR VNAA2011060200020](https://openairdocs.org/sdr/VNAA2011060200020), May 27, 2011: WIRE HARNESS. DEFECTIVE. CREW REPORTED WOW INPUT AND STEERING INOP AMBER CAS MESSAGES AFTER TAKEOFF FROM DAY. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, 
- [SDR VNAA2011021400006](https://openairdocs.org/sdr/VNAA2011021400006), Feb 14, 2011: BEAM. DAMAGED. DURING SCHEDULED MAINTENANCE FS 280.0 J-CHANNEL, TRASVERSE BEAM, AND FLOOR SUPPORT CAPS WERE CRACKED AND CORRODED O/B OF RBL6 AND LBL9. REPAIRS WERE MADE USING 
- [SDR VNAA2011021400007](https://openairdocs.org/sdr/VNAA2011021400007), Feb 14, 2011: CHANNEL. DAMAGED. DURING SCHEDULED MAINTENANCE FS 280.0 J-CHANNEL, TRANSVERSE BEAM, AND FLOOR SUPPORT CAPS WERE CRACKED AND CORRODED O/B OF RBL 6 AND LBL 9. REPAIRS WERE MADE USI

All 67: https://openairdocs.org/deregistered/N215PS-2025-12-09/reports.md

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