- Registered owner
- Umb Bank Na Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 10178
- Year built
- 2004
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- November 1, 2004
- Certificate issued
- December 17, 2021
- Expires
- December 31, 2028
- Mode S code
- A9A4E2
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every GE CF34 model are included below.
On this page
Airworthiness directives that may apply · 164
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1988 | 1 |
|---|---|
| 1997 | 2 |
| 1999 | 3 |
| 2000 | 2 |
| 2001 | 4 |
| 2002 | 4 |
| 2003 | 10 |
| 2004 | 6 |
| 2005 | 5 |
| 2006 | 7 |
| 2007 | 5 |
| 2008 | 8 |
| 2009 | 11 |
| 2010 | 17 |
| 2011 | 10 |
| 2012 | 10 |
| 2013 | 4 |
| 2014 | 7 |
| 2015 | 4 |
| 2016 | 10 |
| 2017 | 7 |
| 2018 | 13 |
| 2019 | 6 |
| 2020 | 7 |
| 2021 | 7 |
| 2022 | 10 |
| 2023 | 9 |
| 2024 | 6 |
| 2025 | 8 |
| 2026 | 7 |
Airframe · Bombardier CL-600-2C10
AD 2026-15-16Time Limits/Maintenance ChecksAD 2026-13-02NavigationAD 2026-08-02StabilizersInformation bulletins that may apply · 4
Advisory, not mandatory.
Airframe · Bombardier CL-600-2C10
SAIB NM-09-06Landing gear: Inspect body fairing seal common to the main landing gear (MLG) inboard doorsSAIB NM-09-03Engine Fuel and Control - Implementing Fuel Tank System Airworthiness LimitationsSAIB NM-07-11Brake System AccumulatorsEngine · GE CF34 series
SAIB NE-04-77NTSB investigations
No NTSB investigations matched to N720PSMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Bombardier CL-600-2C10 aircraft
FAA incident reports
No FAA accident or incident reports matched to N720PSMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Bombardier CL-600-2C10 aircraft
Service difficulty reports · 92
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR VNAA2026020511802Skin · dentedNOSE FUSELAGE UPPER RH PANEL SKIN, DENT AT STR-13R AND FWD OF FS281.65. C/W PERMANENT REPAIR IAW REO 670-3-11-2262_REV-A. NO DEFECTS NOTED AT THIS TIME.SDR VNAA2025123111101Sensor · faultedLEFT WING ANTI-ICE CAUTION MESSAGE AND WING ANTI-ICE FAULT. REMOVED AND REPLACED THE LT INBD WING TEMP SENSOR IAW AMM 30-12-06-000/400-801-A01-PSA. OPS CHECKED GOOD.SDR VNAA2025060911102Controller · faultedSTEERING INOP CAUTION, PERFORMED RESET, SYSTEM FAILED AGAIN. / REMOVED AND REPLACED NWS ECU IAW AMM 32-51-10-000/400-801-A01. FUNCTIONAL CHECK OF NWS GOOD. OPS CHECK OF RVDT WHILE TAXIING GOOD.
See all 92 reportsSTCs that may be installed · 166
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Bombardier CL-600-2C10
STC ST01305WI-DModification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.STC ST12461IBInstallation of Cockpit Voice Recorder with optional RIPS UpgradeSTC ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.