N276STBell 214ST
Safety record in brief:No NTSB accidents or incidents since 198210 ADs may apply
Registration
FAA Aircraft Registry · Oct 17, 2026- Registered owner
- Bank Of Utah Trustee
- Owner type
- Corporation
- City, state
- Salt Lake City, UT
- Certificate issued
- Apr 1, 2026
- Expires
- Apr 30, 2033
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Bell
- Model
- 214ST
- Serial number
- 28107
- Aircraft type
- Rotorcraft
- Category
- Land
- Certification
- Type Certificated
- Seats
- 18
- Engines
- 2
- Max takeoff weight
- 12,500 - 19,999 lb
- Type certificate data sheet
- H10SW
- Mode S code
- A2BE68
Engine
- Type
- Turbo-shaft
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2026 – nowBank Of Utah TrusteeSalt Lake City, UT · current
- 1975 – 1980Individual ownerWest Covina, CA · different airframe: 1975 Menefee Scorpion Too 1976j S/N 484309601
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (10)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2020-14-01 | Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.)… | Aug 11, 2020 | Airframe (214ST)Only with: Spindle to yoke bolt P/N 214-010-262-103 with bolt S/N BH179163, BH179164, BH179169, BH179170, BH179171, BH179175, BH179176, BH179178, BH224783, BH224751, BH224756, BH224764, BH224765, BH383851, BH383853, BH383855, BH383856, BH383857, BH383858, BH383860, BH383861, BH383862, BH383864, BH383865, BH383868, BH383872, BH383873, BH383878, or BH383879 installed. |
| 2014-12-01 | Bell Helicopter Textron, Inc. (Bell) Helicopters | Jul 14, 2014 | Airframe (214ST)Certain serial numbers: 214B 28001–28070; 214B-1 28001–28070; 214ST 28101–28200. Only with: Tail rotor hanger bearing P/N 214-040-606-005 or 214-040-606-101 installed. |
| 99-04-13 | Bell Helicopter Textron, Inc. Model 214ST Helicopters | Mar 4, 1999 | Airframe (214ST)Certain serial numbers: 214ST 28101–on |
| 98-23-18 | Bell Helicopter Textron, Inc. Model 214B, 214B-1, and 214ST Helicopters | Nov 30, 1998 | Airframe (214ST) |
| 98-18-01 | Bell Helicopter Textron, Inc. Model 214B, 214B-1, and 214ST Helicopters | Aug 25, 1998 | Airframe (214ST)Only with: Main rotor trunnion P/N 214-010-230-101 installed. |
Show all 10 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 97-19-09 | Bell Helicopter Textron, Inc. Model 214ST Helicopters | Oct 16, 1997 | Airframe (214ST)Only with: Pillow block bearing bolts P/N 20-057-12-48D or 20-057-12-50D installed. |
| 97-17-06 | Bell Helicopter Textron, Inc. Model 214ST Helicopters | Sep 24, 1997 | Airframe (214ST)Only with: Equipped with emergency float kit P/N 214-706-120 containing emergency float inflation solenoid valves P/N 214-073-929-103 or -105 in solenoid valve assemblies P/N 214-073-940-101 or -103. |
| 97-15-04 | Bell Helicopter Textron, Inc. Model 214B, 214B-1, and 214ST Helicopters | Aug 19, 1997 | Airframe (214ST)Only with: Main transmission upper planetary carrier P/N 214-040-077-007 or 214-040-077-101 installed. |
| 97-06-02 | Bell Helicopter Textron, Inc. Model 214B, 214B-1 and 214ST Helicopters | Apr 16, 1997 | Airframe (214ST)Only with: Lower planetary spider P/N 214-040-080-001 or -101 installed (214B, 214B-1); P/N 214-040-080-101 installed (214ST). |
| 96-07-12 | Bell Helicopter Textron, Inc., Model 214ST Helicopters | May 10, 1996 | Airframe (214ST)Certain serial numbers: 214ST 28101–28132. Only with: With tailboom assembly P/N 214-031-003-111 or 214-031-003-277 and emergency float kit P/N 214-706-120 installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (0)
No Service Difficulty Reports found for this airframe since 1995.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026