# N260JS: 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: 7957
- Year built: 2004
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 29, 2004
- Certificate issued: June 27, 2023
- Last registry action: July 6, 2023
- Mode S code: A27FD6
- 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/N260JS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=260JS
- Page: https://openairdocs.org/deregistered/N260JS-2025-12-09

From the FAA registry file of October 29, 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 (63, newest 50)

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

- [SDR VNAA2019111521102](https://openairdocs.org/sdr/VNAA2019111521102), Nov 12, 2019: TUBE. CONTAMINATED. DURING TAKEOFF ROLL ON RWY 01, THE CREW INDICATED A FAULTY AIRSPEED INDICATOR BETWEEN 80-100 KIAS. THE CREW THEN REJECTED THE TAKEOFF AND WAS ABLE TO TAXI BACK 
- [SDR VNAA2019110111103](https://openairdocs.org/sdr/VNAA2019110111103), Nov 1, 2019: SENSOR. FAILED. WHILE CLIMBING OUT OF CAK, LEFT HAND ENGINE HAD N1 FLUCTUATIONS. THEY DECLARED AN EMERGENCY BUT DID NOT SHUT DOWN THE ENGINE AND LANDED SAFELY BACK IN CAK. THEY
- [SDR VNAA2019090211102](https://openairdocs.org/sdr/VNAA2019090211102), Sep 2, 2019: WIRE HARNESS. FAILED. CREW GOT WOW INPUT CAUTION MSG ON WHEELS-UP OUT OF TYS, THAT WENT AWAY AS SOON AS MLG WAS UP. CREW RAN QRH. DETERMINED NO ISSUE AS LONG AS MSG WENT AWAY. CREW N
- [SDR VNAA2019083081101](https://openairdocs.org/sdr/VNAA2019083081101), Aug 28, 2019: WARNING MESSAGE. FALSE ACTIVATION. CREW RECEIVED A WEIGHT ON WHEEL MESSAGE. INFORMED AIR TRAFFIC CONTROL THAT THEY WOULD NEED A QUICK TURN OFF THE RUNWAY TO IN CASE THEY LOST THEIR NOSE WHEEL STE
- [SDR VNAA2019081631102](https://openairdocs.org/sdr/VNAA2019081631102), Aug 13, 2019: BALLAST. FAILED. REPORTED ELECTRICAL BURNING SMELL COMING FROM ROW 10 IN CABIN. R&R BALLAST IN ROW 10 IAW CRJ 200 AMM 33-21-04-000/400-801. NO SMELL DETECTED AT THIS TIME, OP CH
- [SDR VNAA2018083111101](https://openairdocs.org/sdr/VNAA2018083111101), Aug 31, 2018: UNKNOWN. ODOR. CREW REPORTED AN ELECTRIC SMELL IN COCKPIT WHEN SWITCHING POWER FROM APU TO GROUND POWER. MX INSPECTED FLIGHT DECK AND SURROUNDING AREA FOR ELECTRIC SMELL. NO S
- [SDR VNAA2018051599912](https://openairdocs.org/sdr/VNAA2018051599912), May 15, 2018: INTERCOSTAL. CRACKED. INTERCOSTAL BETWEEN FS 621 AND FS 625 AT LBL45 WL 94 IS CRACKED. REMOVED AND REPLACED OBLIQUE ANGLE IAW SRM 51-42-06.
- [SDR VNAA2018051599911](https://openairdocs.org/sdr/VNAA2018051599911), May 15, 2018: INTERCOSTAL. CRACKED. INTERCOSTAL BETWEEN FS 621 AND FS 625 AT RBL45 WL 94 IS CRACKED. REMOVED AND REPLACED OBLIQUE ANGLE IAW SRM 51-42-06.
- [SDR VNAA2018051599910](https://openairdocs.org/sdr/VNAA2018051599910), May 15, 2018: BULKHEAD. CRACKED. REPAIRED FS621 BULKHEAD IAW REO 601R-53-61-1240 REV D DATED 10/31/16. AND INCORPORATED DEVIATION REPAIR IAW REO 601R-53-61-6554 REV-- DATED 5/8/18 AT RBL 27.5 W
- [SDR VNAA2018051599909](https://openairdocs.org/sdr/VNAA2018051599909), May 15, 2018: RIB. CRACKED. RIGHT WING BATT RIB CAP ANGLE AT WS 48.30 IS CRACKED. REMOVED AND REPLACED CAP ANGLE IAW SRM 51-42-21.
- [SDR VNAA2018051599908](https://openairdocs.org/sdr/VNAA2018051599908), May 15, 2018: RIB. CRACKED. LEFT WING BATT RIB CAP ANGLE AT WS 48.30 IS CRACKED. REMOVED AND REPLACED CAP ANGLE IAW SRM 51-42-21
- [SDR VNAA2018051599907](https://openairdocs.org/sdr/VNAA2018051599907), May 15, 2018: ANGLE. CRACKED. CLIP ANGLES AT FS 200 LBL6 AND RBL6 WL79 ARE CRACKED . REMOVED AND REPLACED CLIP ANGLES PN: 600-33101-89 AND CLIP ANGLE PN 600-33101-90 IAW SRM 51-42-06.
- [SDR VNAA2018051599906](https://openairdocs.org/sdr/VNAA2018051599906), May 15, 2018: CROSSBEAM. CRACKED. FS 280 CROSSBEAM IS CRACKED JUST O/B OF LBL 9. REPAIRED FS 280 CROSSBEAM IAW REO 601R-53-11-926 REV B DATED 2006/05/10.
- [SDR VNAA2018051599905](https://openairdocs.org/sdr/VNAA2018051599905), May 15, 2018: DOOR SILL. CORRODED. RT FLOOR SILL HAS AREA OF CORROSION AND SOME CHAFING, DAMAGE FROM FLOOR BOARD BETWEEN FS 559+112 TO FS 621. REMOVED AND REPLACED SILL IAW EO CL-600-2B19-53-L056
- [SDR VNAA2018051599904](https://openairdocs.org/sdr/VNAA2018051599904), May 15, 2018: STRINGER. CORRODED. STGR 27 IS CORRODED BETWEEN FS 559+112 AND FS 574. REMOVED AND REPLACED ANGLE CLIP IAW SRM 200 51-42-06.
- [SDR VNAA2018051599903](https://openairdocs.org/sdr/VNAA2018051599903), May 15, 2018: STRINGER. CRACKED. PAX DOOR UPPER SILL (STR 3L) IS CRACKED JUST AFT OF FS 379.00. REPAIRED CRACKED STRINGER IAW REO 601R-53-21-2976. REV-- DATED 2018-04-28.
- [SDR VNAA2018051599902](https://openairdocs.org/sdr/VNAA2018051599902), May 15, 2018: FRAME. CORRODED. FUSELAGE FRAME FS574 IS CORRODED BETWEEN STGR 25L AND STGR 18R. REMOVED AND REPLACED FRAME SECTOR P/N 601R36024-61 IAW SRM 51-40-11, 51-42-06 AND 51-42-21.
- [SDR VNAA2018051599901](https://openairdocs.org/sdr/VNAA2018051599901), May 15, 2018: SKIN. CRACKED. FORWARD FUSELAGE SKIN IS CRACKED AT THE LT TRU DOOR AFT LATCH LOCATION. REMOVED AND REPLACED DOOR LANDING IAW SRM 51-42-06 AND 51-42-13.
- [SDR VNAA2018032311102](https://openairdocs.org/sdr/VNAA2018032311102), Mar 23, 2018: WINDSHIELD. FAILED. WHILE IN CRUISE FLIGHT, THE CREW NOTICED A CRACK ON THE CAPTAIN`S WINDSHIELD AND NOTICED A FEW SPARKS WHILE THE WINDSHIELD HEAT WAS ON. DECLARED AN EMERGENCY AN
- [SDR VNAA2017112811101](https://openairdocs.org/sdr/VNAA2017112811101), Nov 28, 2017: TARGET. LOOSE. CREW RECEIVED GEAR DISAGREE MESSAGE AFTER DEPARTING CAE, DUE TO THE RIGHT MAIN GEAR NOT RETRACTING. MX INSPECTED AND FOUNG THE RT MAIN GEAR UPLOCK PROXIMITY SEN
- [SDR VNAA2017040900010](https://openairdocs.org/sdr/VNAA2017040900010), Apr 9, 2017: CARBON SEAL. DEFECTIVE. RED RIGHT ENGINE OIL PRESSURE WARNING. REMOVED AND REPLACED THE ACCESSORY DRIVE GEARBOX’S CARBON SEAL ASSEMBLIES.
- [SDR VNAA2016091300012](https://openairdocs.org/sdr/VNAA2016091300012), Sep 13, 2016: PROXIMITY SENSOR. INOPERATIVE. AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE PASSENGER DOOR OUTER HAN
- [SDR VNAA2016041200012](https://openairdocs.org/sdr/VNAA2016041200012), Apr 12, 2016: CONTROL UNIT. FAILED. FLAPS FAIL MESSAGE, MAINTENANCE TROUBLESHOT, R & R THE FLAPS ELECTRONIC CONTROL UNIT, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2015042400040](https://openairdocs.org/sdr/VNAA2015042400040), Apr 24, 2015: SENSOR. FAILED. CREW REPORTED RT 14TH DUCT, RED WARNING MESSAGE ON TAKEOFF. QRH WAS RUN AND MESSAGE PERSISTED. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE T
- [SDR VNAA2014081100007](https://openairdocs.org/sdr/VNAA2014081100007), Aug 11, 2014: SKIN. CRACKED. DURING SCHEDULED MAINTENANCE, LOWER WING PLANK AFT FASTENER WAS FOUND CRACKED. REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014081100006](https://openairdocs.org/sdr/VNAA2014081100006), Aug 11, 2014: SKIN. CRACKED. DURING SCHEDULED MAINTENANCE, THE AFT RIGHT CORNER OF THE NLG CUTOUT SKIN, BS 235 WAS FOUND CRACKED. INSPECTED AND REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVI
- [SDR VNAA2014081100005](https://openairdocs.org/sdr/VNAA2014081100005), Aug 11, 2014: SKIN. DAMAGED. DURING SCHEDULED MAINTENANCE A CREASE WAS FOUND BELOW THE BAGGAGE BAY SCUFF PLATE AT BS 605. REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014081100004](https://openairdocs.org/sdr/VNAA2014081100004), Aug 11, 2014: POST. CRACKED. DURING SCHEDULED MAINTENANCE THE RT VERTICAL POST BS 409+128 WAS FOUND CRACKED. VERTICAL POST R & R IAW AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014081100003](https://openairdocs.org/sdr/VNAA2014081100003), Aug 11, 2014: SEAT TRACK. CORRODED. DURING SCHEDULED MAINTENANCE, CABIN SEAT TRACK BS 409+40 WAS FOUND CORRODED. SEAT TRACK R & R IAW AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014062200020](https://openairdocs.org/sdr/VNAA2014062200020), Jun 22, 2014: WINDSHIELD. MALFUNCTIONED. CREW REPORTED ICE ACCUMULATION INSIDE BLACK AREA OF LT SIDE ON CAPTAIN’S FRONT WINDSHIELD. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R &
- [SDR VNAA2013070100001](https://openairdocs.org/sdr/VNAA2013070100001), Jul 1, 2013: IDG. FAILED. DURING CRUISE, NR 1 GENERATOR FELL OFF LINE. ACFT RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. MX TROUBLESHOT, R & R NR 1 IDG IAW ACFT MANUALS. CHECKS WERE 
- [SDR VNAA2013050400001](https://openairdocs.org/sdr/VNAA2013050400001), May 4, 2013: RIB. CRACKED. DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND AT THE RIGHT RIB IN RIGHT WHEEL WELL. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIR
- [SDR VNAA2013013100015](https://openairdocs.org/sdr/VNAA2013013100015), Jan 31, 2013: SENSING ELEMENT. FAULTY. CREW REPORTED LEFT 14TH STAGE BLEED DUCT WARNING MESSAGE WITH ANTI-ICE TURNED ON AND APU STARTED. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MESSAGE WENT OFF 15
- [SDR VNAA2013011100004](https://openairdocs.org/sdr/VNAA2013011100004), Jan 11, 2013: TIRE. SEPARATED. ON CLIMBOUT, SHORTLY AFTER TAKEOFF, CREW HEARD THUMPING NOISE AROUND NOSE GEAR. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND TREAD
- [SDR VNAA2012111800012](https://openairdocs.org/sdr/VNAA2012111800012), Nov 18, 2012: SMOKE DETECTOR. FALSE ACTIVATION. CREW REPORTED LAVATORY SMOKE ALARM SOUNDED ABOUT 7 MINUTES INTO FLIGHT. NO SMELL OR SMOKE SEEN. NO MESSAGES WERE DISPLAYED. AIRCRAFT RETURNED TO AIRPORT LANDING
- [SDR VNAA2012091100008](https://openairdocs.org/sdr/VNAA2012091100008), Sep 11, 2012: HANDLE. OPEN. CREW REPORTED CARGO DOOR CAUTION MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. HANDLE WAS CONFIRMED OPEN BY GROUND PERSONNEL. MAINTENAN
- [SDR VNAA2011102700023](https://openairdocs.org/sdr/VNAA2011102700023), Oct 21, 2011: SENSING ELEMENT. FAULTY. CREW REPORTED RIGHT 14TH DUCT RED CAS MESSAGE IN FLIGHT EN ROUTE FROM DAY TO DCA. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REM
- [SDR VNAA2011072700028](https://openairdocs.org/sdr/VNAA2011072700028), Jul 24, 2011: BEAM. DAMAGED. DURING SCHEDULED MAINTENANCE THE FS 280.0 FLOOR TRAVERSE BEAM WAS FOUND CRACKED AND CORRODED. THE FS 280.0 FLOOR TRAVERSE BEAM WAS INSPECTED AND REPAIRED USING 
- [SDR VNAA20110727](https://openairdocs.org/sdr/VNAA20110727), Jul 24, 2011: BEAM. DAMAGED. DURING SCHEDULED MAINTENANCE THE FS 280.0 FLOOR TRAVERSE BEAM WAS FOUND CRACKED AND CORRODED. THE FS 280.0 FLOOR TRAVERSE BEAM WAS INSPECTED AND REPAIRED USING 
- [SDR VNAA2011072700027](https://openairdocs.org/sdr/VNAA2011072700027), Jul 24, 2011: POST. CRACKED. DURING SCHEDULED MAINTENANCE FS409+128 RBL 18 AND LBL POST WERE CRACKED. REPAIRS WERE MADE. INSPECTION AND REPAIRS WERE ACCOMPLISHED USING THE AIRCRAFT MAINTENA
- [SDR VNAA2011072700026](https://openairdocs.org/sdr/VNAA2011072700026), Jul 24, 2011: SKIN. CORRODED. DURING SCHEDULED MAINTENANCE LEFT WING LOWER PLANK ACCESS HOLE (540BB) WAS PITTED. REPAIRS WERE MADE. INSPECTION AND REPAIRS WERE ACCOMPLISHED USING THE AIRCRAF
- [SDR VNAA2011060900004](https://openairdocs.org/sdr/VNAA2011060900004), Jun 6, 2011: TRIM SWITCH. DIRTY. CREW REPORTED STAB TRIM CAS MESSAGE OCCURRED REPEATEDLY AFTER TAKEOFF FROM CVG. CREW RETURNED TO CVG AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, CLEAN
- [SDR VNAA2010112900018](https://openairdocs.org/sdr/VNAA2010112900018), Nov 26, 2010: ANGLE. CRACKED. DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND AT FS 559 CAP ANGLE. CRACK WAS REPAIRED USING AIRCRAFT MANUALS AND AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA20101129](https://openairdocs.org/sdr/VNAA20101129), Nov 26, 2010: SKIN. DAMAGED. DURING SCHEDULED MAINTENANCE DAMAGE WAS FOUND FROM FS605 TO FS621 SKIN. DAMAGE WAS REPAIRED USING AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SER
- [SDR VNAA2010011500007](https://openairdocs.org/sdr/VNAA2010011500007), Jan 8, 2010: OIL SYSTEM. LOW. CREW REPORTED AN APU OIL TEMP AMBER MESSAGE DURING CRUISE EN ROUTE FROM CLT TO XNA. AIRCRAFT DIVERTED TO BNA BECAUSE THE RT ENGINE INTEGRATED DRIVE GENERATOR (I
- [SDR VNAA2009092300006](https://openairdocs.org/sdr/VNAA2009092300006), Sep 20, 2009: FAN BLADE. DAMAGED. CREW REPORTED, INGESTED SMALL BIRD(S) IN LEFT ENGINE. AIRCRAFT RETURNED TO DAY WITHOUT INCIDENT. MAINTENANCE INSPECTED LT ENGINE PER THE MANUFACTURER MAINTENANC
- [SDR VNAA2009040200016](https://openairdocs.org/sdr/VNAA2009040200016), Mar 30, 2009: INDICATION SYS. MALFUNCTIONED. CREW REPORTED 10 MIN AFTER T/O AUTO XFLOW INHIBIT WHITE STATUS MSG APPEARED AND THE FUEL QTY INDICATORS LEFT SIDE AS WELL AS TOTAL FUEL WERE BLANK W/AMBER DASHE
- [SDR VNAA2009030900006](https://openairdocs.org/sdr/VNAA2009030900006), Mar 6, 2009: PROBE. FAILED. CREW REPORTED THE FUEL QUANTITY INDICATOR SHOWED DASHES ON LT SIDE AND TOTAL FUEL SYNOPTIC PAGE. AIRCRAFT RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE INSPECTE
- [SDR VNAA2008120900003](https://openairdocs.org/sdr/VNAA2008120900003), Dec 1, 2008: APU. HUNG START. CREW REPORTED ON DESCENT INTO DAY, APU EXPERIENCED A HUNG START. MOMENTS LATER THE CREW TRIED TO START APU AND WAS SUCCESSFUL. BLEED AIR WAS SELECTED TO APU AND
- [SDR VNAA0807009](https://openairdocs.org/sdr/VNAA0807009), Jul 17, 2008: NONE. NONE. CREW REPORTED THE PDF SHOWED FLAPS EXTENDED TO 2 DEG UNCOMMANDED AT 30,000FT WITH NO AURAL WARNING AT CRUISE. THE CREW DIVERTED TO TYS AND LANDED WITHOUT INCIDE

All 63: https://openairdocs.org/deregistered/N260JS-2025-12-09/reports.md

## Other aircraft with N260JS

- [Cancelled 1994-06-09](https://openairdocs.org/deregistered/N260JS-1994-06-09): Pitts Aerobatics S-2B, S/N 5020. Exported to Canada. Owner: [Hardwick Steven F](https://openairdocs.org/faa-owner/HARDWICK%20STEVEN%20F), [Charleston, SC](https://openairdocs.org/faa-place/SC/Charleston)

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