N214EBBell 214ST
Safety record in brief:No NTSB accidents or incidents since 198210 ADs may apply11 service difficulty reports
Registration
FAA Aircraft Registry · Oct 19, 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
- Standard · Transport
- Airworthiness date
- Jun 29, 1996
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
- 28130
- 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
- A1C8C4
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 19, 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 (11)
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.
- Main rotor · stud · shearedFeb 19, 2016
TWO MAIN ROTOR TRANSMISSION MAST STUDS FOUND SHEARED OFF DURING 25 HOUR INSPECTION.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Tail rotor drive · chip detector · activatedDec 1, 2015
PILOT REPORTED MOMENTARY TAIL ROTOR GEAR BOX CHIP LIGHT ON MASTER CAUTION PANEL.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine fuel and control · fuel filter · dirtyNov 24, 2015
NUMBER 1 ENG FUEL FILTER MASTER CAUTION LIGHT CAME ON, INDICATING FUEL FLOW RESTRICTION.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Engine · engine · failedSep 16, 2015
DURING CRUISE FLIGHT IN A SHALLOW RIGHT HAND TURN, NR 2 ENG EXPERIENCED HIGH SIDE FAILURE IMMEDIATELY, FOLLOWED BY UNCOMMANDED SHUTDOWN. ACFT RECOVERED 26 MILES BACK TO BASE IN SINGLE ENG CONFIGURATION.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor drive · case · crackedMar 27, 2015
DURING PREFLIGHT OIL WAS NOTICED ON THE UPPER TRANSMISSION CASE. UPON FURTHER INVESTIGATION, PAINT WAS BUBBLED ON RING GEAR CASE. CLEANED PAINT & DYE PENETRANT WAS USED REVEALING A SUSPECTED CRACK. ACFT WAS RUN AT 100% NR & OIL WAS NOTICED COMING FROM A CRACK IN THE TRANSMISSION RING GEAR CASE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · debondedDec 25, 2014
TAIL BOOM, EMPENNAGE METALLIC SKIN, HONEYCOMB STRUCTURE ON RT SIDE JUST AFT OF THE FWD VOR ANTENNA MOUNT WL 74, BS 294 HAS DISBONDED. INSPECTION WAS PERFORMED IAW BHT ALL SRM 2-13. TAIL BOOM IS BEING REPLACED WITH REPAIRED SERVICE TAIL BOOM. DAMAGED TAIL BOOM IS BEING SENT TO REPAIR FACILITY.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · pump · failedNov 14, 2014
ON APPROACH, CREW NOTICED LOW PRESS ON NR 2 HYD SYS & THE MASTER CAUTION LIGHT, CONSULTED THE EMER CHECKLIST & SHUTOFF NR 2 HYD SYS. LANDED THE ACFT AT ANOTHER LOCATION.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · access panel · missingOct 26, 2014
AFTER A ROUTINE MISSION AN ACCESS PANEL LOCATED ON THE AFT PYLON FAIRING ON THE RT SIDE, WAS FOUND NOT INSTALLED ON THE ACFT. THE PANEL IS SECURED AT THE TOP BY A HINGE TO THE AFT PYLON FAIRING. THE HINGE CONSISTS OF 8 SECTIONS ATTACHED TO THE FAIRING AND HAS A WIRE THROUGH EACH SECTION AS WELL AS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · hydraulic line · rupturedAug 9, 2014
INFLIGHT CREW NOTED NR 1 HYD SYS FAIL LIGHT ILLUMINATED & PROCEEDED TO SHUT DOWN NR 1 SYS. EXECUTED UNEVENTFUL LANDING. VISUALLY FOUND NR 1 HYD SYS PRESSURE LINE PN 70-060T000Y4B4 TO LT CYCLIC SERVO RUPTURED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor · tab · missingAug 23, 2013
WHILE CONDUCTING A "POST FLIGHT" INSPECTION, MECHANICS NOTICED THAT ONE OF THE MAIN ROTOR BLADES WAS MISSING A TRIM TAB.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 11 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026