- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 28197
- Year built
- 1991
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Multiple
- Airworthiness date
- May 13, 2024
- Certificate issued
- September 8, 2022
- Expires
- September 30, 2029
- Mode S code
- AA05CC
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every GE CT7 model are included below.
On this page
Airworthiness directives that may apply · 48
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1981 | 1 |
|---|---|
| 1982 | 1 |
| 1984 | 2 |
| 1986 | 2 |
| 1987 | 2 |
| 1988 | 2 |
| 1990 | 1 |
| 1994 | 3 |
| 1996 | 1 |
| 1997 | 6 |
| 1998 | 3 |
| 1999 | 1 |
| 2002 | 1 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2011 | 2 |
| 2013 | 3 |
| 2014 | 1 |
| 2017 | 1 |
| 2018 | 1 |
| 2020 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 2 |
| 2025 | 2 |
See all 54 ADs
Information bulletins that may apply · 1
Advisory, not mandatory.
Engine · GE CT7 series
SAIB ANE-98-31NTSB investigations
No NTSB investigations matched to N745HMatched 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 Bell 214ST aircraft
FAA incident reports
No FAA accident or incident reports matched to N745HMatched 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 Bell 214ST aircraft
Service difficulty reports · 20
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR HEEA066526Actuator · frozenACTUATOR MOTOR FROZEN.SDR HEEA0012451Regulator · inoperativeVOLTAGE REGULATOR INOPERATIVE.SDR 97ZZZX3989Rotor Grip · crackedMAIN ROTOR GRIP, DRAG BRACE ATTACHMENT, LOWER LUG CRACKED, 1.25 INCHES LONG. DEFECT IDENTIFIED VISUALLY DURING 5,000 HR/5 YEAR E-CHECK. DEFECT BECAME APPARENT DURING DISASSEMBLY. DEFECTIVE PART BEING RETURNED TO BELL FOR INVESTIGATION.
See all 20 reportsSTCs that may be installed · 50
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 50 STCs