# N247JS: 2004 Bombardier CL-600-2B19, registration cancelled 2022-05-14

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 14, 2022
- 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: 7922
- Year built: 2004
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 30, 2004
- Certificate issued: January 28, 2022
- Last registry action: January 28, 2022
- Mode S code: A24AD9
- Owner when cancelled: [Beautech Power Systems LLC](https://openairdocs.org/faa-owner/BEAUTECH%20POWER%20SYSTEMS%20LLC)
- Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas)
- Owner type: LLC
- Owner's area on the map: 32.7883° N, 96.7996° W: Placed by OpenAirDocs at the center of ZIP code 75201, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N247JS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=247JS
- Page: https://openairdocs.org/deregistered/N247JS-2022-05-14

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 (79, newest 50)

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

- [SDR VNAA2020012711103](https://openairdocs.org/sdr/VNAA2020012711103), Jan 27, 2020: CONTROL LEVER. FAILED. FLAPS FAIL IN FLIGHT, RETURNED TO FIELD, DEFERRED THE SYSTEM. MAINTENANCE REMOVED AND REPLACED THE FLAP CONTROL LEVER.
- [SDR VNAA2019120651102](https://openairdocs.org/sdr/VNAA2019120651102), Dec 5, 2019: UNKNOWN. ODOR. SMELL SMOKE IN CABIN JUST PRIOR TO PUSH BACK. PERFORMED OPS TEST OF THE AIR CONDITIONING SYS IAW CRJ 200 AMM 21-51-00-710-801 NO SMELL OF SMOKE DETECTED AT THIS
- [SDR VNAA2019051099913](https://openairdocs.org/sdr/VNAA2019051099913), May 10, 2019: BULKHEAD. CRACKED. FS 621 REAR PRESSURE BULKHEAD FWD FACE BLO.00 WL127.5-WL113.5 INDICATIONS NOTED APPROX 6" LONG 50% FULL SCREEN HEIGHT, LBL9.5 WL76.50 INDICATION NOTED .6" LONG 
- [SDR VNAA2019051099912](https://openairdocs.org/sdr/VNAA2019051099912), May 10, 2019: SEAT TRACK. CORRODED. LBL 9 FLOOR SEAT TRACK FROM FS 399- FS 399 +128 SEGMENT IS CORRODED. C/A: INSTALLED NEW SEAT TRACK IAW REO 601R-53-00-485.
- [SDR VNAA2019051099911](https://openairdocs.org/sdr/VNAA2019051099911), May 10, 2019: SEAT TRACK. CORRODED. RBL 9 FLOOR SEAT TRACK FS 364- FS 399 SEGMENT IS CORRODED. C/A: INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR VNAA2019051099910](https://openairdocs.org/sdr/VNAA2019051099910), May 10, 2019: ANGLE. CORRODED. PAX DOOR LOWER SILL MID ANGLE IS CORRODED BEYOND LIMITS. C/A: REMOVED AND REPLACED MID ANGLE IAW SRM 51-42-06 AND 51-42-21.
- [SDR VNAA2019051099909](https://openairdocs.org/sdr/VNAA2019051099909), May 10, 2019: BRACKET. CRACKED. HYD SYS NR 3 PRESSURE TRANSDUCER BRACKET CRACKED IN LT MLG WHEEL WELL CEILING. C/A: REMOVED AND REPLACED BRACKET IAW SRM 51-42-06.
- [SDR VNAA2019051099908](https://openairdocs.org/sdr/VNAA2019051099908), May 10, 2019: BRACKET. CRACKED. HYD SYS NR 3 TRANSDUCER BRACKET CRACKED IN RT MLG CEILING. C/A: REMOVED AND REPLACED BRACKET IAW SRM 51-42-06.
- [SDR VNAA2019051099907](https://openairdocs.org/sdr/VNAA2019051099907), May 10, 2019: BRACKET. CRACKED. HYD SYS NR 3 PRESSURE TRANSDUCER Z-BRACKET CRACKED IN RT MLG WHEEL WELL CEILING. C/A: REMOVED AND REPLACED Z-BRACKET IAW SRM 51-42-06 AND 51-42-04.
- [SDR VNAA2019051099906](https://openairdocs.org/sdr/VNAA2019051099906), May 10, 2019: SEAT TRACK. CORRODED. LBL 9 FLOOR SEAT TRACK FS 364- FS 399 SEGMENT IS CORRODED. C/A: INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR VNAA2019051099905](https://openairdocs.org/sdr/VNAA2019051099905), May 10, 2019: SEAT TRACK. CORRODED. RBL 9 FLOOR SEAT TRACK FROM FS399- FS409+128 SEGMENT IS CORRODED. C/A: REMOVED AND REPLACED RBL9 FLOOR SEAT TRACK FS399-FS409+128 SEGMENT IAW SRM 51-40-11, AMM 
- [SDR VNAA2019051099904](https://openairdocs.org/sdr/VNAA2019051099904), May 10, 2019: FLOORBEAM. CORRODED. RBL 9 FLOORBEAM, I/B FLOOR SUPPORT FLANGE, IS CORRODED AT FS 591 TO FS 621 AROUND NUT PLATE PULL RIVETS. C/A: INSTALLED NEW SERVICEABLE FLOORBEAM AT RBL 9 BETWE
- [SDR VNAA2019051099903](https://openairdocs.org/sdr/VNAA2019051099903), May 10, 2019: FLOORBEAM. CORRODED. LBL 9 FLOORBEAM, I/B FLOOR SUPPORT FLANGE, IS CORRODED AT FS 595 AROUND NUT PLATE PULL RIVETS. C/A: INSTALLED NEW SERVICEABLE FLOORBEAM AT LBL 9 BETWEEN FS 574-
- [SDR VNAA2019051099902](https://openairdocs.org/sdr/VNAA2019051099902), May 10, 2019: FLOORBEAM. CORRODED. RBL9 FLOORBEAM HAS CORROSION AROUND FLOOR NUTPLATE HOLES BETWEEN FS409 AND FS409+128. C/A: REMOVED AND REPLACED RBL9 FLOORBEAM CAP IAW SRM 51-40-11, 51-42-06, 5
- [SDR VNAA2019051099901](https://openairdocs.org/sdr/VNAA2019051099901), May 10, 2019: FLOORBEAM. CORRODED. LBL9 FLOORBEAM HAS CORROSION AROUND FLOOR NUTPLATE HOLES BETWEEN FS409 AND FS409+128. C/A: REMOVED AND REPLACED LBL9 FLOORBEAM CAP IAW SRM 51-40-11, 51-42-06, 5
- [SDR VNAA2019030811101](https://openairdocs.org/sdr/VNAA2019030811101), Mar 8, 2019: LIGHT. INOPERATIVE. SUPPLEMENTAL INFORMATION:L/H FWD EMERGENCY LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED L/H FWD EXTERIOR EMERGENCY LIGHT IAW CRJ200 AMM 33-51-21-000/400-801.
- [SDR VNAA20181112101](https://openairdocs.org/sdr/VNAA20181112101), Oct 29, 2018: NONE. NONE. ON TAKEOFF ABOUT 600 FEET THE CREW OBSERVED A LARGE BIRD GO PAST AND HEARD A "THUMP" AND BEGAN TO RECEIVE ENGINE INDICATIONS THAT THE BIRD MADE IMPACT WITH THE 
- [SDR VNAA2017062911101](https://openairdocs.org/sdr/VNAA2017062911101), Jun 29, 2017: BRACKET. BENT. AFTER TAKEOFF, THE CREW SELECTED GEAR UP AND THE GEAR DID NOT RETRACT. 6 SECONDS AFTER SELECTING THE HANDLE UP THE MAIN GEAR RETRACTED AND THE NOSE GEAR DID NOT
- [SDR VNAA2017062999902](https://openairdocs.org/sdr/VNAA2017062999902), Jun 29, 2017: FITTING. CRACKED. CARGO DOOR UPPER FWD FITTING CRACKED. INSTALLED NEW SERVICEABLE CARGO DOOR UPPER FORWARD FITTING.
- [SDR VNAA2017062999901](https://openairdocs.org/sdr/VNAA2017062999901), Jun 28, 2017: BULKHEAD. CRACKED. CRACK INDICATIONS AT LBL 36.20, LBL 18.0 AND RBL 18.0 AND WL 74. REPAIRED AREAS AT LBL 36.20 LBL 18.00 AND RBL 18.0 AT WL 74 IAW REO 601R-53-61-6070.
- [SDR VNAA2017062899912](https://openairdocs.org/sdr/VNAA2017062899912), Jun 28, 2017: CHANNEL. CRACKED. BS 621 DOOR SUPPORTS CHANNEL, LOWER ANGLE CRACKED. REMOVED AND REPLACED THE CHANNEL.
- [SDR VNAA2017062899911](https://openairdocs.org/sdr/VNAA2017062899911), Jun 28, 2017: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT RBL 27.5, WL 80, APPROXIMATELY 2 INCHES LONG, 50% FSH. REPAIRED THE BULKHEAD WEB IAW REO 601R-5
- [SDR VNAA2017062899910](https://openairdocs.org/sdr/VNAA2017062899910), Jun 28, 2017: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT RBL 18, WL 74, APPROXIMATELY 2.5 INCHES LONG, 70% FSH. COMPLIED WITH REO 601R-53-61-6070.
- [SDR VNAA2017062899909](https://openairdocs.org/sdr/VNAA2017062899909), Jun 28, 2017: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT BL 0, WL 112, APPROXIMATELY 4.0 INCHES LONG, 50% FSH. REPAIRED THE BULKHEAD WEB IAW REO 601R-53
- [SDR VNAA2017062899908](https://openairdocs.org/sdr/VNAA2017062899908), Jun 28, 2017: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT LBL 18, WL 74, APPROX 2 INCHES LONG, 90% FSH. REPAIRED THE BULKHEAD WEB IAW REO 601R-53-61-6070
- [SDR VNAA2017062899907](https://openairdocs.org/sdr/VNAA2017062899907), Jun 28, 2017: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION AT LBL 18.00, WL 106, APPROX 2.5 INCHES LONG, 50% FSH. REPAIRED REAR PRESSURE BULKHEAD IAW REO 601R-53-6
- [SDR VNAA2017062899906](https://openairdocs.org/sdr/VNAA2017062899906), Jun 28, 2017: BULKHEAD WEB. CRACKED. FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION OF A CRACK NOTED AT LBL 36.20, WL 74, APPROX 2.5 INCHES LONG, 90% FSH. REPAIRED THE REAR PRESSURE BULHEAD IAW RE
- [SDR VNAA2017062899905](https://openairdocs.org/sdr/VNAA2017062899905), Jun 28, 2017: SKIN. CRACKED. NLG WHEEL CUTOUT HAS VISIBLE SIGNS OF POSSIBLE CRACK IN BOTH AFT CORNERS AT FS 235.00. REPAIRED IAW REO 601R-53-11-010
- [SDR VNAA2017062899904](https://openairdocs.org/sdr/VNAA2017062899904), Jun 28, 2017: FLOOR SUPPORT. CORRODED. CORROSION ON RT SIDE PRESSURE FLOOR SUPPORT IN MULTIPLE LOCATIONS BETWEEN BS 461 AND 529. REPAIRED PER REO 601R-53-41-666
- [SDR VNAA2017062899903](https://openairdocs.org/sdr/VNAA2017062899903), Jun 28, 2017: FLOOR SUPPORT. CORRODED. CORROSION ON LT PRESSURE FLOOR SUPPORT IN MULTIPLE LOCATIONS BETWEEN BS 461 TO 529. REPAIRED IAW REO 601R-53-41-666
- [SDR VNAA2017062899902](https://openairdocs.org/sdr/VNAA2017062899902), Jun 28, 2017: FRAME. CRACKED. LEFT BS 718 FRAME CRACKED AT STRINGER 11L. REPLACED THE FRAME SECTION.
- [SDR VNAA2017062899901](https://openairdocs.org/sdr/VNAA2017062899901), Jun 28, 2017: FRAME. CRACKED. RIGHT BS 718 FRAME CRACKED AT STRINGER 11R. REPLACED THE FRAME SECTION.
- [SDR VNAA2017012400033](https://openairdocs.org/sdr/VNAA2017012400033), Jan 24, 2017: TIRE. FAILED. LEFT NOSE TIRE BLEW ON TAKE OFF. REMOVED AND REPLACED BOTH NLG WHEEL AND TIRE ASSEMBLIES.
- [SDR VNAA2016062600028](https://openairdocs.org/sdr/VNAA2016062600028), Jun 26, 2016: LIGHT. BROKEN. SEGMENT OF EMERGENCY LIGHTING GLOW STICK AND COVER, BROKEN AND MISSING AT SEAT 1D. MAINTENANCE INSPECTED, R & R EMERGENCY FLOOR LIGHT LAMP AND PERFORMED CHECKS 
- [SDR VNAA2016053100034](https://openairdocs.org/sdr/VNAA2016053100034), May 31, 2016: APU. FAULTY. APU LOW OIL PRESSURE CAUTION MESSAGE. THE CREW DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, PROPERLY SERVICED THE APU AND PER
- [SDR VNAA2016011300010](https://openairdocs.org/sdr/VNAA2016011300010), Jan 13, 2016: SEAL. DETACHED. CREW REPORTED TOP 8" OF SERVICE DOOR SEAL DETACHED IN FLIGHT. MADE A VERY LOUD NOISE. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REATTACH
- [SDR VNAA2015121600010](https://openairdocs.org/sdr/VNAA2015121600010), Dec 16, 2015: BATTERY PACK. FAILED. CREW REPORTED EMERGENCY LIGHT FLOOR STRIP NOT WORKING FROM ROW 9 TO THE AFT OF AIRCRAFT. MAINTENANCE INSPECTED, R & R NR 4 EMERGENCY LIGHT BATTERY PACK AND PERF
- [SDR VNAA2015083000038](https://openairdocs.org/sdr/VNAA2015083000038), Aug 30, 2015: CONNECTOR. DISCONNECTED. CREW REPORTED EMERGENCY FLOOR LIGHTS INOPERATIVE FROM ROW 9 AND AFT. MAINTENANCE INSPECTED, FOUND RT AFT EMERGENCY LIGHT CONNECTOR DISCONNECTED, RECONNECTED CON
- [SDR VNAA2015081700018](https://openairdocs.org/sdr/VNAA2015081700018), Aug 17, 2015: SKIN. DAMAGED. LIGHTENING STRIKE DAMAGE TO RT AILERON UPPER SKIN AND T/E. REPAIRED THE AILERON IAW REO 601R-57-61-528, REV.
- [SDR VNAA2015081700017](https://openairdocs.org/sdr/VNAA2015081700017), Aug 17, 2015: POST. CRACKED. FS 409+128, BL 0, VERTICAL POST LT AND RT SIDES HAVE INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL 69 .250" LONG 60 PERCENT FSH FAILED NDT. R & R VERTICAL PO
- [SDR VNAA2015081700016](https://openairdocs.org/sdr/VNAA2015081700016), Aug 17, 2015: CARGO TRACK. CORRODED. CARGO TRACK ON RBL 9BETWEEN BS 559+80 AND 559+96 AND CARGO TRACK HAD CORROSION. R & R CARGO TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.
- [SDR VNAA2015081700014](https://openairdocs.org/sdr/VNAA2015081700014), Aug 17, 2015: MOUNT. CORRODED. WARDROBE OTBD MOUNT PAD AT FS 310 HAS CORROSION AROUND BOLT HOLE. R & R 200 DWG 601R38670 AND SRM 51-40-11. INSTALLED NEW PAD IAW SRM 51-42-13 AND 51-21-16.
- [SDR VNAA2015041100014](https://openairdocs.org/sdr/VNAA2015041100014), Apr 11, 2015: WIRE. BROKEN. CREW REPORTED MAIN CABIN DOOR EMERGENCY EXIT STRIP WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED, FOUND BROKEN WIRE ON EMERGENCY LIGHT, INSTALLED NEW WIRE SPLICE 
- [SDR VNAA2014090500001](https://openairdocs.org/sdr/VNAA2014090500001), Sep 5, 2014: WIRE HARNESS. DAMAGED. CREW REPORTED EMERGENCY FLOOR LEVEL LIGHTING AFT OF EMERGENCY EXIT ROW WOULD NOT ILLUMINATE WHEN TESTED. MAINTENANCE TROUBLESHOT, R & R LIGHT WIRE HARNESS AND P
- [SDR VNAA2014060600005](https://openairdocs.org/sdr/VNAA2014060600005), Jun 6, 2014: CONNECTOR. BROKEN. CREW REPORTED FLOOR LEVEL EMERGENCY LIGHTS ROW 9, AND AFT INOPERATIVE. MAINTENANCE TROUBLESHOT AND FOUND EMERGENCY LIGHT CONNECTOR PIN BROKEN AT END OF ROW BY L
- [SDR VNAA2014040900008](https://openairdocs.org/sdr/VNAA2014040900008), Apr 9, 2014: WARNING LIGHT. FALSE ACTIVATION. CREW REPORTED AMBER STEERING INOPERATIVE MESSAGE ON TAKEOFF. LANDED AT DESTINATION AIRPORT WITHOUT INCIDENT. MAINTENANCE PERFORMED OPS CHECK OF NOSEWHEEL STEERI
- [SDR VNAA2013121400007](https://openairdocs.org/sdr/VNAA2013121400007), Dec 14, 2013: SHUTOFF VALVE. FAILED. CREW REPORTED RED WING OVERHEAT MESSAGE DURING CLIMB. CREW RAN QRH, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R MODULATING AND
- [SDR VNAA2013101700007](https://openairdocs.org/sdr/VNAA2013101700007), Oct 17, 2013: PDU. FAILED. CREW REPORTED LT THRUST REVERSER UNLOCK CAUTION MESSAGE IN DESCENT OUT OF FL200. CREW DECLARED EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MX TROUBLESHOT, R 
- [SDR VNAA2013091600007](https://openairdocs.org/sdr/VNAA2013091600007), Sep 16, 2013: INVERTER. INOPERATIVE. CREW AND MX REPORTED ROWS 6 THROUGH 8 EMERGENCY LIGHT INOPERATIVE AND LOWER RT EMERGENCY LIGHT BY OVERWING EXIT INOPERATIVE. MX TROUBLESHOT, R & R NR 3 EMERGENC
- [SDR VNAA2013020500002](https://openairdocs.org/sdr/VNAA2013020500002), Feb 5, 2013: FUEL CONTROL. LEAKING. CREW REPORTED SMOKE TOILET CAUTION MESSAGE ON DESCENT AFTER SWITCH TO APU BLEED. NO SMOKE IN CABIN, BUT FAIRLY STRONG SMELL WHEN BLEEDS WERE SWITCHED. MESSAGE W

All 79: https://openairdocs.org/deregistered/N247JS-2022-05-14/reports.md

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