# N709PS: 2004 Bombardier CL-600-2C10, registration cancelled 2025-04-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 3, 2025
- Status when cancelled: Valid registration
- Airframe: [Bombardier CL-600-2C10](https://openairdocs.org/model/bombardier-cl-600-2c10) (registry code 1390015)
- 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: 10165
- Year built: 2004
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 1, 2004
- Certificate issued: January 24, 2022
- Last registry action: July 7, 2023
- Mode S code: A97753
- Owner when cancelled: [Umb Bank Na Trustee](https://openairdocs.org/faa-owner/UMB%20BANK%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.6171° N, 111.6866° W: Placed by OpenAirDocs at the center of ZIP code 84121, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N709PS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=709PS
- Page: https://openairdocs.org/deregistered/N709PS-2025-04-03

From the FAA registry file of October 31, 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-600-2C10: https://openairdocs.org/model/bombardier-cl-600-2c10.md

## Service difficulty reports (150, newest 50)

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

- [SDR VNAA20250116075](https://openairdocs.org/sdr/VNAA20250116075), Jan 16, 2025: ANGLE. CORRODED. FS 280.00 J ANGLE CORRODED LBL 9 TO RBL 9 INCLUDING BOTH WALL CLIPS. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42
- [SDR VNAA20250116074](https://openairdocs.org/sdr/VNAA20250116074), Jan 16, 2025: PLATE. CORRODED. MULTIPLE AREAS OF CORROSION R/H SILL PLATE F.S. 280 -333 RBL 34 CORRECTIVE ACTION: REMOVED AND REPLACED R/H SILL PLATE P/N SH670-32172-5 AT FS 280-333 RBL 34 IA
- [SDR VNAA20250116073](https://openairdocs.org/sdr/VNAA20250116073), Jan 16, 2025: TIE DOWN. CORRODED. RIGHT INBD FWD GALLEY TIE DOWN CORRODED JUST AFT OF F.S.280 APPROX RBL 14. REMOVED CORRODED TIE DOWN. LOCATED AND REPLACED WITH NEW SERVICEABLE R/H INBD FWD GAL
- [SDR VNAA20250116072](https://openairdocs.org/sdr/VNAA20250116072), Jan 16, 2025: ANGLE. CORRODED. FS 280.00 J ANGLE CORRODED LBL 9 TO RBL 9 INCLUDING BOTH WALL CLIPS. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42
- [SDR VNAA20250116071](https://openairdocs.org/sdr/VNAA20250116071), Jan 16, 2025: TORQUE BOX. DAMAGED. 3 EA TOOLING MARKS ON AFT BOTTOM SIDE OF L/H TORQUE BOX BELOW LOOKING UP F.S.295 APPOX LBL12. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-
- [SDR VNAA20250116070](https://openairdocs.org/sdr/VNAA20250116070), Jan 16, 2025: STRINGER. CORRODED. STR 25R CORRODED F.S. 280 -333. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR VNAA20250116069](https://openairdocs.org/sdr/VNAA20250116069), Jan 16, 2025: SUPPORT ANGLE. CORRODED. FS 632-655 WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE FLANGE IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-4
- [SDR VNAA20250116068](https://openairdocs.org/sdr/VNAA20250116068), Jan 16, 2025: SPLICE. CORRODED. DISCREPANCY: FS 629 STGR 19L -27 ON WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE FLANGES FWD AND AFT HAVE MULTIPLE AREAS OF CORROSION AROUND THE FASTENER HOLES CO
- [SDR VNAA20250116067](https://openairdocs.org/sdr/VNAA20250116067), Jan 16, 2025: SEAT TRACK. CORRODED. R/H I/B SEAT TRACK @ FS 538 HAS SOME GOUGING AND MINOR CORROSION WHICH REQUIRES EVALUATION. CORRECTIVE ACTION: REMOVED RBL 9 SEAT TRACK BETWEEN FS485 AND FS581 
- [SDR VNAA20250116066](https://openairdocs.org/sdr/VNAA20250116066), Jan 16, 2025: FRAME. CORRODED. FRAME AT FS 661 BOTTOM CL AFT END OF FWD CARGO COMPARTMENT IS CORRODED COMPLETELY THROUGH TO THE SHEAR TIE ON THE FRONT SIDE WITH A HOLE APPROXIMATELY 1". CORRE
- [SDR VNAA20250116065](https://openairdocs.org/sdr/VNAA20250116065), Jan 16, 2025: BEAM. CHAFED. FOUND R/H FLAP VANE ACTUATOR AT FLS 140.40 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE. CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIR
- [SDR VNAA20250116064](https://openairdocs.org/sdr/VNAA20250116064), Jan 16, 2025: BEAM. CHAFED. FOUND R/H FLAP VANE ACTUATOR AT FLS 102.90 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE. CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIR
- [SDR VNAA20250116063](https://openairdocs.org/sdr/VNAA20250116063), Jan 16, 2025: BEAM. CHAFED. FOUND R/H FLAP VANE ACTUATOR AT LWS 65.50 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE. CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIRJ
- [SDR VNAA20250116062](https://openairdocs.org/sdr/VNAA20250116062), Jan 16, 2025: BEAM. CHAFED. FOUND L/H FLAP VANE ACTUATOR AT LWS 140.40 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE. CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIR
- [SDR VNAA20250116061](https://openairdocs.org/sdr/VNAA20250116061), Jan 16, 2025: BEAM. CHAFED. FOUND L/H FLAP VANE ACTUATOR AT LWS 65.50 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE. CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIRJ
- [SDR VNAA20250116060](https://openairdocs.org/sdr/VNAA20250116060), Jan 16, 2025: BEAM. CHAFED. FOUND L/H FLAP VANE ACTUATOR AT LWS 102.90 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE. CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIR
- [SDR VNAA20250116059](https://openairdocs.org/sdr/VNAA20250116059), Jan 16, 2025: BEAM. CHAFED. FOUND L/H FLAP VANE ACTUATOR AT FLS 24.00 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIRJ 
- [SDR VNAA20250116057](https://openairdocs.org/sdr/VNAA20250116057), Jan 16, 2025: CHANNEL. DAMAGED. PILOT RUDDER FEEL UNIT CHANNEL CC670-94223 REQUIRES REMOVAL DUE TO DOUBLE DRILLED HOLE. CORRECTIVE ACTION: REMOVED PILOT RUDDER FEEL UNIT LWR CHANNEL CC670-9422
- [SDR VNAA20250116056](https://openairdocs.org/sdr/VNAA20250116056), Jan 16, 2025: ANGLE. CRACKED. PAX DOOR INNER ANGLE ON VENT FLAP COVER FOUND CRACKED AND REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED CRACKED INNER ANGLE IAW CRJ 700 SRM 51-42-06-001-001-
- [SDR VNAA20250116055](https://openairdocs.org/sdr/VNAA20250116055), Jan 16, 2025: STEP. CRACKED. PAX DOOR TOP STEP PANEL CRACKED REQUIRES REPLACEMENT CORRECTIVE ACTION: LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR TOP STEP PANEL P/N:601R317075-3 IAW CRJ700 
- [SDR VNAA20250116054](https://openairdocs.org/sdr/VNAA20250116054), Jan 16, 2025: SEAT TRACK. CRACKED. R/H I/B SEAT TRACK @ FS 538 HAS SOME GOUGING AND MINOR CORROSION WHICH REQUIRES EVALUATION. REMOVED RBL 9 SEAT TRACK BETWEEN FS485 AND FS581 IAW CRJ-700 SRM 53-
- [SDR VNAA20250116053](https://openairdocs.org/sdr/VNAA20250116053), Jan 16, 2025: DRAG ANGLE. CRACKED. PAX DOOR AFT DRAG ANGLE FOUND WITH CRACK AT UPPER END. CORRECTIVE ACTION: LOCATE, DRILL, AND INSTALLED NEW SERVICEABLE DRAG ANGEL P# 601R31772-5S IAW CRJ 700 SR
- [SDR VNAA2025F00005](https://openairdocs.org/sdr/VNAA2025F00005), Jan 16, 2025: STRINGER. CORRODED. STR 26R @ FS. 333 + 6 FOUND TO HAVE PITTING/CORROSION ON ATTACH FLANGE. CORRECTIVE ACTION: REMOVED CORRODED STRINGER AND INSTALLED A NEW STGR26R BETWEEN FS 333 
- [SDR VNAA20250116052](https://openairdocs.org/sdr/VNAA20250116052), Jan 16, 2025: DRAG ANGLE. CRACKED. PAX DOOR FWD STAIR WEB DRAG ANGLE FOUND CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR VNAA20250116051](https://openairdocs.org/sdr/VNAA20250116051), Jan 16, 2025: DRAG ANGLE. CRACKED. PAX DOOR FWD STAIR WEB DRAG ANGLE FOUND CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR VNAA20250116049](https://openairdocs.org/sdr/VNAA20250116049), Jan 16, 2025: COVER. CRACKED. PAX DOOR AFT CORNER COVER FOUND CRACKED UPON REMOVAL. REQUIRES REPLACEMENT. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-13-001-001-A01.
- [SDR VNAA20250116048](https://openairdocs.org/sdr/VNAA20250116048), Jan 16, 2025: CLEAT. CORRODED. CLEAT LOCATED AT STR19L ON FWD SIDE OF FS1047 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-021-001-001-A
- [SDR VNAA20250116047](https://openairdocs.org/sdr/VNAA20250116047), Jan 16, 2025: WINDOW POST. CRACKED. LH WINDSHIELD SIDE POST P/N 601R33223 IS CRACKED APPROX. 6" FROM TOP AND 2" LONG AT 100% FSH FAILING NDT. REPAIRED BY CUTTING OUT DAMAGED PORTION AND SPLICING I
- [SDR VNAA20250116046](https://openairdocs.org/sdr/VNAA20250116046), Jan 16, 2025: RETAINER. CORRODED. MAIN AVIONICS DOOR L/H FWD SEAL RETAINER IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR VNAA20250116045](https://openairdocs.org/sdr/VNAA20250116045), Jan 16, 2025: SUPPORT. CORRODED. FS 909 RBL 2- RBL 22 WING TO FUSELAGE SUPPORT STRUCTURE FLANGE FAYING SURFACE (BOTTOM) IS CORRODED ALONG LENGTH. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-
- [SDR VNAA20250116044](https://openairdocs.org/sdr/VNAA20250116044), Jan 16, 2025: SUPPORT. CORRODED. FS 909 RBL 2- RBL 22 WING TO FUSELAGE SUPPORT STRUCTURE FLANGE FAYING SURFACE (BOTTOM) IS CORRODED ALONG LENGTH. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-
- [SDR VNAA20250116043](https://openairdocs.org/sdr/VNAA20250116043), Jan 16, 2025: SUPPORT. CORRODED. FS 939 ON CL WING TO FUSELAGE SUPPORT STRUCTURE FLANGE IS CORRODED AROUND 2 EA. FASTENER HOLES AND REQUIRES EVALUATION. CORRECTIVE ACTION: REMOVED AND REPLACED 
- [SDR VNAA20250116042](https://openairdocs.org/sdr/VNAA20250116042), Jan 16, 2025: SUPPORT. CORRODED. FS 879 LBL 10- RBL 28 WING TO FUSELAGE SUPPORT STRUCTURE FLANGE FAYING SURFACE (BOTTOM) IS CORRODED ALONG LENGTH AND REQUIRES EVALUATION CORRECTIVE ACTION: REMO
- [SDR VNAA20250116041](https://openairdocs.org/sdr/VNAA20250116041), Jan 16, 2025: FRAME. CRACKED. FS 333.00 FRAME IS CRACKED BETWEEN STRINGER 2R AND 3R. REPAIRED BY CUTTING OUT DAMAGED PORTION AND SPLICING IN NEW REPAIR PARTS IAW MHIRJ REO 670-53-21-2465 REV
- [SDR VNAA20250116040](https://openairdocs.org/sdr/VNAA20250116040), Jan 16, 2025: RETAINER. CORRODED. MAIN AVIONICS DOOR, R/H SEAL RETAINER IS CORRODED. REMOVED AND REPLACED RETIANER I.A.W. CRJ700 SRM 51-42-06-001-001-A01.
- [SDR VNAA20250116039](https://openairdocs.org/sdr/VNAA20250116039), Jan 16, 2025: SKIN. DENTED. THE LEFT WING INBOARD FLAP LOWER SKIN IS DENTED 6 X 6 X .035 JUST AFT OF THE MLG TIRES. CORRECTIVE ACTION: REPAIRED IAW CRJ-700 SRM 57-52-01-201-005-A01.
- [SDR VNAA20250116038](https://openairdocs.org/sdr/VNAA20250116038), Jan 16, 2025: STRINGER. CORRODED. F.S. 406-421 STR 19 CORRODED CORRECTIVE ACTION:STRINGER WAS REPAIRED IAW IAW CRJ700 SRM 53-00-03-201-001-A01
- [SDR VNAA20250116037](https://openairdocs.org/sdr/VNAA20250116037), Jan 16, 2025: SLAT TRACK. CORRODED. FOUND R/H SLAT TRACK 3-1 TO HAVE WEAR DAMAGE IN MULTIPLE LOCATIONS. CORRECTIVE ACTION: REPAIRED R/H SLAT TRACK 3-1 IAW REO 670-57-42-1745 REV-DATED 11-11-2024. 
- [SDR VNAA20250116036](https://openairdocs.org/sdr/VNAA20250116036), Jan 16, 2025: FLOORBEAM. CORRODED. RBL 9 FLOOR BEAM IS CORRODED AT FS 1031 CORRECTIVE ACTION: DAMAGE WAS REPAIRED IAW CRJ700 SRM 53-00-41-201-001-001-A01 AND REO 670-53-61-2395 REV-- DATED 2024-1
- [SDR VNAA20250115034](https://openairdocs.org/sdr/VNAA20250115034), Jan 15, 2025: DOOR SILL. CORRODED. UPON REMOVAL OF AFT CARGO DOOR SILL, FOUND THE CENTER INNER CHORD TO BE CORRODED AT NUTPLATE LOCATIONS. DAMAGE WAS REPAIRED BY INSTALLING A SERVICABLE INNER CHO
- [SDR VNAA20250115033](https://openairdocs.org/sdr/VNAA20250115033), Jan 15, 2025: DOOR SILL. CORRODED. UPON REMOVAL OF AFT CARGO DOOR SILL, FOUND THE CENTER INNER CHORD TO BE CORRODED AT NUTPLATE LOCATIONS. CORRECTIVE ACTION: DAMAGE WAS REPAIRED BY INSTALLING A S
- [SDR VNAA20250115032](https://openairdocs.org/sdr/VNAA20250115032), Jan 15, 2025: DOOR SILL. CORRODED. UPON REMOVAL OF AFT CARGO DOOR SILL, FOUND THE CENTER INNER CHORD TO BE CORRODED AT NUTPLATE LOCATIONS. CORRECTIVE ACTION: DAMAGE WAS REPAIRED BY INSTALLING A S
- [SDR VNAA20250115031](https://openairdocs.org/sdr/VNAA20250115031), Jan 15, 2025: DOOR SILL. CORRODED. UPON REMOVAL OF AFT CARGO DOOR SILL, FOUND THE FWD INNER CHORD TO BE CORRODED AT NUTPLATE LOCATIONS. CORRECTIVE ACTION: DAMAGE WAS REPAIRED BY INSTALLING A SERV
- [SDR VNAA20250115030](https://openairdocs.org/sdr/VNAA20250115030), Jan 15, 2025: SEAT TRACK. CORRODED. DISCREPANCY: LH SIDE SEAT RAIL IS CORRODED BETWEEN FS863 AND FS969.00
- [SDR VNAA20250115029](https://openairdocs.org/sdr/VNAA20250115029), Jan 15, 2025: SEAT TRACK. CORRODED. DISCREPANCY: AFT CARGO BAY SEAT TRACK ON LBL27 FROM FS978 TO FS1006 IS CORRODED CORRECTIVE ACTION: REMOVED CORRODED SEAT RAIL AND INSTALLED A SERVICABLE SEAT RA
- [SDR VNAA20250115028](https://openairdocs.org/sdr/VNAA20250115028), Jan 15, 2025: SEAT TRACK. CORRODED. CO # 101651424 BARCODE HN00190434 DISCREPANCY: LH SIDE SEAT RAIL IS CORRODED BETWEEN FS863 AND FS969.00
- [SDR VNAA20250115027](https://openairdocs.org/sdr/VNAA20250115027), Jan 15, 2025: SEAT TRACK. CORRODED. LH SIDE SEAT RAIL IS CORRODED BETWEEN FS 785.15 AND 863. REMOVED CORRODED SEAT RAIL AND INSTALLED A SERVICABLE SEAT RAIL
- [SDR VNAA20250115026](https://openairdocs.org/sdr/VNAA20250115026), Jan 15, 2025: SEAT TRACK. CORRODED. RBL 9 SEAT TRACK IS CORRODED BETWEEN FS 985.00 AND 1015.00. CORRECTIVE ACTION: REMOVED SEAT TRACK ON RBL9 FROM FS985.00 TO FS1015.00 IAW CRJ-700 AMM 53-00-49-00
- [SDR VNAA20250115025](https://openairdocs.org/sdr/VNAA20250115025), Jan 15, 2025: SEAT TRACK. CORRODED. LBL 9 SEAT TRACK IS CORRODED BETWEEN FS 985.00 AND 1015.00. CORRECTIVE ACTION: REMOVED, FABRICATED, AND REPLACED SEAT TRACK IAW MHIRJ REO 670-53-00-589, REV-C, 
- [SDR VNAA20250115024](https://openairdocs.org/sdr/VNAA20250115024), Jan 15, 2025: SEAT TRACK. CORRODED. RBL 27 SEAT TRACK IS CORRODED BETWEEN FS 1031.00 AND 1069.75. CORRECTIVE ACTION: REMOVED, FABRICATED, AND REPLACED SEAT TRACK IAW MHIRJ REO 670-53-00-589, REV-C

All 150: https://openairdocs.org/deregistered/N709PS-2025-04-03/reports.md

## NTSB investigations (3)

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 DCA25MA108](https://openairdocs.org/ntsb/DCA25MA108), Jan 30, 2025: Bombardier CL-600-2C10 (N709PS), Washington, DC, destroyed, 67 fatal. Probable cause: The Federal Aviation Administration’s (FAA) placement of a helicopter route in close proximity to a runway approach path; their failure to regularly review and evaluate helicopter routes and…
- [NTSB ENG21LA023](https://openairdocs.org/ntsb/ENG21LA023), Mar 26, 2021: Bombardier CL-600-2C10 (N709PS), North Canton, OH, incident, minor damage. Probable cause: Moisture ingression thru the window humpseal coming into contact with the terminal block braid wires.
- [NTSB DCA17CA064](https://openairdocs.org/ntsb/DCA17CA064), Feb 15, 2017: Bombardier CL 600 2C10 (N709PS), Charlotte, NC, substantial damage. Probable cause: collision with a deer during takeoff.

## FAA accident and incident reports (3)

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.

- [Accident 20250129018192A](https://openairdocs.org/incident/20250129018192A), Jan 29, 2025: Bombardier Inc CL-600-2C10 (N709PS), Arlington, VA, Destroyed, 64 fatal. [privacy data omitted] And a [privacy data omitted], collided in midair and crashed into the potomac river near Washington-Ronald Reagan national airport, DC…
- [Incident 20210326002099I](https://openairdocs.org/incident/20210326002099I), Mar 26, 2021: Bombardier CL-600-2C10 (N709PS), Akron, OH, Minor damage. On the morning of 26 March 2021 flight 5440 cak-phl, aircraft N709PS, experienced a right windshield terminal block failure, leading to sparking, a momentary…
- [Incident 20170215005879I](https://openairdocs.org/incident/20170215005879I), Feb 15, 2017: Bombardier Inc CL-600-2C10 (N709PS), Charlotte, NC, Minor damage. JIA5320 (N709PS) departed RWY36C and struck deer at V1, approximately 133 KTS, on take off roll. Aircraft requested a flyby and it was determined aircraft was…

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