N393ALBell 214ST
Safety record in brief:No NTSB accidents or incidents since 198210 ADs may apply7 service difficulty reports
Registration
FAA Aircraft Registry · Oct 17, 2026- Registered owner
- Bank Of Utah Trustee
- Owner type
- Corporation
- City, state
- Salt Lake City, UT
- Certificate issued
- Sep 8, 2022
- Expires
- Sep 30, 2029
- Airworthiness
- Experimental · To show compliance with FAR
- Airworthiness date
- Apr 14, 1997
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
- 28117
- 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
- A48DF9
Engine
- Make and model
- Ge Ct7 Series
- Type
- Turbo-shaft
- Power
- 1560 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2022 – nowBank Of Utah TrusteeSalt Lake City, UT · current
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 (7)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Engine fuel and control · fuel filter · restrictedMay 17, 2015
NUMBER 2 ENG FUEL FILTER MASTER CAUTION LIGHT CAME ON WHEN THE ENG WAS AT 60 % TQ , INDICATING A FUEL FLOW RESTRICTION.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor · plate · tornApr 1, 2015
DURING CRUISE FLIGHT , PILOT REPORTED UNUSUAL VIBRATIONS. DURING INSPECTION, NODAL BEAM PLATES & HELPER SPRING FOUND TO HAVE TORN ELASTOMERIC RUBBER.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuel · pump · wornJan 1, 2015
DURING FLIGHT, NR 1 FUEL TRANSFER PUMP LIGHT FLICKERED. ACFT WAS ON LAST MISSION RETURNING TO BASE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 7 reportsShow fewer reports
- Fire protection · wire · brokenJan 4, 2003
ON THE PREFLIGHT CHECK, NR 2 FIRE DETECTION SYSTEM INOPERATIVE. A WIRE WAS FOUND BROKEN AT THE NR 2 FIRE DETECTION AMPLIFIER.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Tail rotor · bearing · failedDec 10, 2002
DURING DAILY INSPECTION. BEARINGS OUTER LINER COMING APART DUE TO HIGH VIBRATION, SCRAPPED 4 EACH BEARINGS. CLOSER DAILY INSPECTION OF TAILROTOR ASSEMBLY.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Tail rotor · bolt · brokenJul 11, 2002
DURING THE DAILY SERVICE CHECK. BROKEN TAIL ROTOR YOKE PLATE BOLT.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fire protection · light · inoperativeApr 16, 2001
ON PRE-START CHECK, LEFT HAND BAGGAGE FIRE DETECTION SYSTEM WOULD NOT TEST, TEST LAMP BURNED OUT AND WIRE BROKEN ADJACENT TO SMOKE DETECTOR.
From FAA Service Difficulty Reports; matched by N-number and serial number.
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