# N257PS: 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: 7939
- Year built: 2004
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 23, 2004
- Certificate issued: August 12, 2023
- Last registry action: August 12, 2023
- Mode S code: A272D5
- 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/N257PS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=257PS
- Page: https://openairdocs.org/deregistered/N257PS-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 (61, newest 50)

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

- [SDR VNAA202003119995](https://openairdocs.org/sdr/VNAA202003119995), Mar 11, 2020: DOOR SILL. CORRODED. AFT CARGO DOOR FLOOR SILL CORRODED IN MULTIPLE LOCAITONS FROM FS 574 - 621 UNDER FLOORBOARD 281LLF. 03/02/20 (ROSEM) M/A: 1. N/A. C/A: 1. FOUND AFT CARGO DORO F
- [SDR VNAA202003119994](https://openairdocs.org/sdr/VNAA202003119994), Mar 11, 2020: DOOR SILL. CORRODED. LH PRESSURE FLOOR SILL HAS 3 AREAS OF CORROSION FS449-FS473. 02/20/20 (AS) M/A: 1. N/A C/A: 1. REMOVED CORROSION @ L/H PRESSURE FLOOR SILL BETWEEN FS 409+129 AN
- [SDR VNAA202003119993](https://openairdocs.org/sdr/VNAA202003119993), Mar 11, 2020: DOOR SILL. CORRODED. RH PRESSURE FLOOR SILL HAS 9 AREAS OF CORROSION BETWEEN FS428 AND FS530. 02/20/20 (AS) M/A: 1. N/A C/A: 1. REMOVED CORROSION @ R/H PRESSURE FLOOR SILL AND FLOOR
- [SDR VNAA202003119992](https://openairdocs.org/sdr/VNAA202003119992), Mar 11, 2020: BULKHEAD. CRACKED. FOUND REAR PRESSURE BUCKHEAD HAS INDICATIONS NOTED AT BLOO WL112-110 5090 FSH AND LBL18 WL141-142.510090FSH BOTH AREAS FAILED NOT INSPECTIONS. 2/17/20 (TK) M/A:
- [SDR VNAA202003119991](https://openairdocs.org/sdr/VNAA202003119991), Mar 11, 2020: SKIN. CORRODED. CORROSION FOUND ON OUTER SKIN UNDER FWD WATER DRAIN MAST. 2/15/20 (PCC) M/A: 1. CORROSION FOUND TO BE OUT OF LIMITS IAW CRJ200 SRM 53-00-31. 2/15/20 C/A: 1. REM
- [SDR VNAA2019110761102](https://openairdocs.org/sdr/VNAA2019110761102), Nov 6, 2019: WARNING MESSAGE. FALSE ACTIVATION. APU FIRE RED WARNING MESSAGE IN FLIGHT. DEFERRED APU. PER FIM VISABLY INSPECTED APU FIRE LOOP NO DEFECTS NOTED PERFORMED OPS CHECK OF APU FIRE-DETECTION SYSTEM 
- [SDR VNAA2019071811101](https://openairdocs.org/sdr/VNAA2019071811101), Jul 18, 2019: BATTERY. DISCHARGED. EMERGENCY LIGHTS WON'T STAY ON. R&R ALL 4 EMERGENCY POWER SUPPLY BATTERIES IAW CRJ 200 AMM 33-51-04-000/400-801. OPS CHECK GOOD AT THIS TIME. S/N 169577, 121949
- [SDR VNAA2019060911101](https://openairdocs.org/sdr/VNAA2019060911101), Jun 9, 2019: INVERTER. FAILED. LH LOWER EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED LH FLOOR LEVEL FLOOD EXIT SIGN IAW CRJ 200 AMM 33-51-10-000/400-801 REMOVED AND REPLACED
- [SDR VNAA2018102211102](https://openairdocs.org/sdr/VNAA2018102211102), Oct 22, 2018: EXHAUST VALVE. MALFUNCTIONED. DURING CLIMB CREW RECEIVED AN OVERBOARD COOL AMBER MSG. AFTER RUNNING THE QRH THE MSG STILL PERSISTED. CREW DECIDED TO CONTINUE TO CLT PRESSURIZED AND DECLARED 
- [SDR VNAA2018011499912](https://openairdocs.org/sdr/VNAA2018011499912), Jan 14, 2018: TRUNNION. CRACKED. ONE INDICATION NOTED IN FASTENER HOLE OTBD OF MLG CUT OUT ON RT SIDE 5TH HOLE GOING FWD FROM AFT HOLE IN STEEL STRAP ON O/B AFT SIDE OF HOLE .550 INCH UP FROM L
- [SDR VNAA2018011499911](https://openairdocs.org/sdr/VNAA2018011499911), Jan 14, 2018: TRUNNION. CRACKED. ONE INDICATION NOTED IN FASTENER HOLE O/B OF MLG CUT OUT ON LT SIDE FIRST HOLE AFT OF STEEL STRAP. ON AFT SIDE OF HOLE .300 INCH UP FROM LOWER SURFACE OF PLANK 
- [SDR VNAA2018011499910](https://openairdocs.org/sdr/VNAA2018011499910), Jan 14, 2018: BULKHEAD WEB. CRACKED. REAR PRESSURE BULKHEAD WEB HAS CRACK INDICATIONS, LBL 27.5, WL 130. ONE INCH IN LENGTH. CUT OUT DAMAGE IAW REO 601R-53-61-1541, REV F. PERFORMED AN EDDY CURRENT
- [SDR VNAA2018011499909](https://openairdocs.org/sdr/VNAA2018011499909), Jan 14, 2018: BULKHEAD WEB. CRACKED. REAR PRESSURE BULKHEAD WEB HAS MULTIPLE CRACK INDICATIONS NOTED AT LBL 9.5, WL 109, ONE INCH IN LENGTH. CUT OUT DAMAGE IAW REO 601R-53-61-1285, REV E. PERFORMED
- [SDR VNAA2018011499908](https://openairdocs.org/sdr/VNAA2018011499908), Jan 14, 2018: BULKHEAD WEB. CRACKED. REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT LBL 36.20, WL 76, ONE INCH LONG. CUT OUT DAMAGE IAW REO 601R-53-61-1285, REV E, SHEET 13, SECTION 5D.
- [SDR VNAA2018011499907](https://openairdocs.org/sdr/VNAA2018011499907), Jan 14, 2018: DRAG ANGLE. CRACKED. PAX DOOR AFT DRAG ANGLE CRACKED ADJACENT TO POWER ASSIST PULLEY BRACKET. REPAIRED THE DRAG ANGLE IAW EO 2B19-52-L05444A, PART B, AND REO 601R-52-11-513 REV B.
- [SDR VNAA2018011499906](https://openairdocs.org/sdr/VNAA2018011499906), Jan 14, 2018: FRAME. CRACKED. FRAME CRACKED AT BS 718, STRINGER 11L. REMOVED AND INSTALLED A NEW FRAME SECTION IAW SRM 51-42-06 & 51-23-16.
- [SDR VNAA2018011499905](https://openairdocs.org/sdr/VNAA2018011499905), Jan 14, 2018: FRAME. CRACKED. FRAME CRACKED AT BS 718, STRINGER 11R. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-06, AND SRM 51-40-11.
- [SDR VNAA2018011499903](https://openairdocs.org/sdr/VNAA2018011499903), Jan 14, 2018: ANGLE. CRACKED. FLOORBEAM AT BS 484, LBL27 HAS A CRACKED ANGLE. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-21.
- [SDR VNAA20180114999](https://openairdocs.org/sdr/VNAA20180114999), Jan 14, 2018: SEAT TRACK. CORRODED. CORROSION ON LEFT SEAT TRACK FWD AND AFT OF BS 409 + 128 AT VARIOUS LOCATIONS. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-055, REV C.
- [SDR VNAA2018011499902](https://openairdocs.org/sdr/VNAA2018011499902), Jan 14, 2018: SEAT TRACK. CORRODED. CORROSION ON RT SEAT TRACK FWD AND AFT OF BS 409 + 128 AT VARIOUS LOCATIONS. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-055, REV C.
- [SDR VNAA2018011499901](https://openairdocs.org/sdr/VNAA2018011499901), Jan 14, 2018: ANGLE. CRACKED. AFT EQUIPMENT BAY LEFT BS 621 - 625 OBLIQUE ANGLE CRACKED. REMOVED AND REPLACED THE OBLIQUE ANGLE IAW SRM 51-42-21.
- [SDR VNAA2017070911101](https://openairdocs.org/sdr/VNAA2017070911101), Jul 9, 2017: CONNECTOR. DIRTY. CREW RECEIVED A CARGO BOTTLE LOW CAUTION MESSAGE AT FLIGHT LEVEL 290. DECLARED AN EMERGENCY AND DIVERTED. LANDED WITH OUT INCIDENT. FOUND NO EVIDENCE OF FIRE OR
- [SDR VNAA2016081800020](https://openairdocs.org/sdr/VNAA2016081800020), Aug 18, 2016: CONTROL LEVER. FAULTY. FLAPS FAILED DURING APPROACH AT 30 DEGREES AND 160 KNOTS. LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE FLAP CONTROL LEVER AND PREF
- [SDR VNAA2016081100009](https://openairdocs.org/sdr/VNAA2016081100009), Aug 11, 2016: INVERTER. INOPERATIVE. EMERGENCY FLOOR TRACK LIGHTING OUT AFTER ROW 5 TO THE BACK SIDEWALL. MAINTENANCE R & R THE NR 3 INVERTER IAW AMM AND THE NR 4 POWER SUPPLY BATTERY FOR THE EMERG
- [SDR VNAA2016081100008](https://openairdocs.org/sdr/VNAA2016081100008), Aug 11, 2016: INVERTER. INOPERATIVE. RIGHT LOWER FLOODLIGHT INOPERATIVE. MAINTENANCE R & R THE NR 3 INVERTER IAW AMM, OPS CHECK GOOD.
- [SDR VNAA2016060400005](https://openairdocs.org/sdr/VNAA2016060400005), Jun 4, 2016: CONTROLLER. INOPERATIVE. CAPTAIN SIDE WINDSHIELD SHATTERED IN FLIGHT. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R &
- [SDR VNAA2016060400004](https://openairdocs.org/sdr/VNAA2016060400004), Jun 4, 2016: WINDSHIELD. CRACKED. CAPTAIN SIDE WINDSHIELD SHATTERED IN FLIGHT. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R &
- [SDR VNAA2016041600017](https://openairdocs.org/sdr/VNAA2016041600017), Apr 16, 2016: A/C PACK. MALFUNCTIONED. DURING CLIMBOUT, THE CREW RECEIVED A RT PACK FAULT AND RT PACK HIGH PRESSURE WHEN COMPLYING WITH MEL PROCEDURES FOR THE LT PACK. MAINTENANCE INTEROGATED AND FOU
- [SDR VNAA2016030300003](https://openairdocs.org/sdr/VNAA2016030300003), Mar 3, 2016: PLATE. CORRODED. PASSENGER DOOR FWD ANCHOR FITTING SERRATED PLATE CORRODED. R & R PASSENGER DOOR FWD ANCHOR FITTING SERRATED PLATE, PN 600-38061-11 IAW AMM 52-11-17-400-804.
- [SDR VNAA2016030200002](https://openairdocs.org/sdr/VNAA2016030200002), Mar 2, 2016: ANGLE. CORRODED. PAX DOOR UPPER SILL ANGLE CORRODED BETWEEN BS 310 AND 349. REPAIRED PAX DOOR UPPER SILL ANGLE, PN 601R31527-221 IAW SRM 51-42-10, 51-42-21, AND 51-42-06.
- [SDR VNAA2016030200001](https://openairdocs.org/sdr/VNAA2016030200001), Mar 2, 2016: FLOOR SUPPORT. CORRODED. RIGHT PRESSURE FLOOR SILL STRAP CORRODED BEYOND LIMITS AT FS 513.00. R & R RT PRESSURE SILL STRAP IAW SRM 51-42-16, 51-42-22, AND 51-77-00.
- [SDR VNAA2016021400017](https://openairdocs.org/sdr/VNAA2016021400017), Feb 14, 2016: CONNECTOR. DAMAGED. CREW REPORTED BACK HALF OF FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE TROUBLESHOT, REPAIRED AFT CONNECTOR ON EMERGENCY LIGHT STRIP AND PERFORMED CHEC
- [SDR VNAA2015111100004](https://openairdocs.org/sdr/VNAA2015111100004), Nov 11, 2015: WIRE. DISCONNECTED. CREW REPORTED FLOOR EMERGENCY LIGHTS HAD A DISCONNECTED WIRE AND AFT HALF OF LIGHTS BEYOND ROW NINE INOPERATIVE. MAINTENANCE INSPECTED, SPLICED IN WIRE SPLICE C
- [SDR VNAA2015050700001](https://openairdocs.org/sdr/VNAA2015050700001), May 7, 2015: SENSOR. FAILED. CREW REPORTED ANTI-ICE DUCT WARNING MESSAGE DURING CLIMB. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R FUSELAGE SENSING EL
- [SDR VNAA2014102800016](https://openairdocs.org/sdr/VNAA2014102800016), Oct 28, 2014: LIGHT. BROKEN. CREW REPORTED ENTRY LIGHT BROKEN. MAINTENANCE INSPECTED, R & R ENTRY FLOOR EMERGENCY FLOODLIGHT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2014061400012](https://openairdocs.org/sdr/VNAA2014061400012), Jun 14, 2014: ACCESS DOOR. OUT OF ADJUST. CREW REPORTED FORWARD F/A EMERGENCY EQUIPMENT ACCESS, LATCHES AND DOOR, STICKS AND HARD TO OPEN. MAINTENANCE INSPECTED, ADJUSTED EMERGENCY EQUIPMENT ACCESS DOOR
- [SDR VNAA2014052000014](https://openairdocs.org/sdr/VNAA2014052000014), May 20, 2014: CARGO TRACK. CORRODED. DURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND ON THE CARGO TRACKS AT BS 559+80, 559.0+96 AND FS 574 - 605. THE AREA WAS INSPECTED AND CARGO FLOOR TRACKS WER
- [SDR VNAA2014052000013](https://openairdocs.org/sdr/VNAA2014052000013), May 20, 2014: FLOOR SUPPORT. CORRODED. DURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND AROUND CARGO FLOOR SUPPORT FASTENER HOLES. THE AREA WAS INSPECTED AND CARGO FLOOR SUPPORT WAS REPLACED USING A
- [SDR VNAA2014012600017](https://openairdocs.org/sdr/VNAA2014012600017), Jan 26, 2014: COVER. BROKEN. CREW REPORTED EMERGENCY LIGHT AT ROW 1 INOPERATIVE AND COVER BROKEN. MAINTENANCE INSPECTED, R & R ROW 1 FLOOR-TRACK EMERGENCY LIGHT AND COVER AND PERFORMED CHEC
- [SDR VNAA2013121000005](https://openairdocs.org/sdr/VNAA2013121000005), Dec 10, 2013: CONNECTOR. DAMAGED. CREW REPORTED EMERGENCY FLOOR LIGHTING INOPERATIVE FROM ROW 5 TO ROW 9. MAINTENANCE INSPECTED, R & R J391Y CONNECTOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED
- [SDR VNAA2013091300006](https://openairdocs.org/sdr/VNAA2013091300006), Sep 13, 2013: SELECTOR VALVE. FAILED. CREW REPORTED GEAR DISAGREE RED CAS MESSAGE. MAIN GEAR INDICATED DOWN AND LOCKED AND NOSE GEAR INDICATED UP. STEERING INOPERATIVE AMBER CAS MESSAGE ALSO REPORTE
- [SDR VNAA2012111200005](https://openairdocs.org/sdr/VNAA2012111200005), Nov 12, 2012: CONTROLLER. FAILED. CREW REPORTED CAPTAIN’S FRONT WINDOW CRACKED AND ELECTRICAL ARCING NOTICED. CREW RETURNED TO GATE. MAINTENANCE INSPECTED, REMOVED AND REPLACED CAPTAIN’S FRONT W
- [SDR VNAA2012050700009](https://openairdocs.org/sdr/VNAA2012050700009), May 7, 2012: LIGHT. INOPERATIVE. CREW REPORTED LEFT AFT EXTERIOR DOOR EMERGENCY LIGHT OUT. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT AFT EXTERIOR EMERGENCY LIGHT BULB AND PERFORMED CHECK
- [SDR VNAA2011071800020](https://openairdocs.org/sdr/VNAA2011071800020), Jul 13, 2011: BPSU. FAILED. CREW REPORTED FLAPS FAILURE DURING APPROACH FLAPS SELECTED FROM 0-08 WHEN FAILURE OCCURED SPEED WAS 190 IAS, ALT 6000 FT. CREW ELECTED TO DIVERT TO CLT WITHOUT 
- [SDR VNAA2011071800016](https://openairdocs.org/sdr/VNAA2011071800016), Jul 12, 2011: COMPUTER. FAILED. CREW REPORTED A FLAPS FAIL AT 10,000FT SPEED 250KNTS. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND PERFORMED OPERATIONAL CH
- [SDR VNAA2011071500013](https://openairdocs.org/sdr/VNAA2011071500013), Jul 11, 2011: BPSU. FAILED. CREW REPORTED FLAPS FAILURE WHEN FLAPS SELECTED FROM ZERO DEGREES TO EIGHT (8) DEGREES DURING APPROACH TO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENA
- [SDR VNAA2011070800005](https://openairdocs.org/sdr/VNAA2011070800005), Jul 2, 2011: CONTROL UNIT. MALFUNCTIONED. CREW REPORTED FLAPS FAIL AT 20 DEGREES WHEN FLAPS WERE SELECTED TO 30 DEGREES WHILE ON APPROACH TO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TRO
- [SDR VNAA2011031600011](https://openairdocs.org/sdr/VNAA2011031600011), Mar 16, 2011: SILL. CORRODED. DURING SCHEDULED MAINTENANCE THE LEFT PRESSURE FLOOR SILL HAD CORROSION AROUND NUT PLATES FROM FS 449.85 TO 473.15. REPAIRS WERE ACCOMPLISHED USING AIRCRAFT MAI
- [SDR VNAA2011031600013](https://openairdocs.org/sdr/VNAA2011031600013), Mar 16, 2011: POST. CRACKED. DURING SCHEDULED MAINTENANCE THE FS 409+128 BULKHEAD VERTICAL POST WAS CRACKED. REPAIRS WERE ACCOMPLISHED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RETUR
- [SDR VNAA2011061600012](https://openairdocs.org/sdr/VNAA2011061600012), Mar 16, 2011: BEAM. CRACKED. DURING SCHEDULED MAINTENANCE, THE FS 280 TRANSVERSE BEAM WAS CRACKED. REPAIRS WERE ACCOMPLISHED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RETURNED TO SER

All 61: https://openairdocs.org/deregistered/N257PS-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 OPS09IA005](https://openairdocs.org/ntsb/OPS09IA005), May 29, 2009: Bombardier CL-600-2B1 (N257PS), Charlotte, NC, incident, no damage. Probable cause: The Charlotte local control east controller's failure to ensure that the runway was clear prior to authorizing N409DR to enter the runway.

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