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Aircraft record

N390AL1990 Bell 214ST

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:No NTSB accidents or incidents since 198210 ADs may apply20 service difficulty reports

Registration
Valid
expires Sep 30, 2029
Based in
Salt Lake City, UT
owner city / state
Engine
CT7 SERIES · 1560 hp
Ge
Owners
1
since 2022
NTSB events
None
since 1982
ADs may apply
10
confirm with A&P
Service reports
20
since 1995

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
Standard · Transport
Airworthiness date
Apr 5, 2024

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 data

Airframe

Manufacturer
Bell
Model
214ST
Year
1990
Serial number
28198
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
A482D4

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
  1. 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, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs 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.

ADSubjectEffectiveApplies to
2020-14-01Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.)…Aug 11, 2020Airframe (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.
2014-12-01Bell Helicopter Textron, Inc. (Bell) HelicoptersJul 14, 2014Airframe (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.
99-04-13Bell Helicopter Textron, Inc. Model 214ST HelicoptersMar 4, 1999Airframe (214ST)Certain serial numbers: 214ST 28101–on
98-23-18Bell Helicopter Textron, Inc. Model 214B, 214B-1, and 214ST HelicoptersNov 30, 1998Airframe (214ST)
98-18-01Bell Helicopter Textron, Inc. Model 214B, 214B-1, and 214ST HelicoptersAug 25, 1998Airframe (214ST)Only with: Main rotor trunnion P/N 214-010-230-101 installed.
Show all 10 ADs
ADSubjectEffectiveApplies to
97-19-09Bell Helicopter Textron, Inc. Model 214ST HelicoptersOct 16, 1997Airframe (214ST)Only with: Pillow block bearing bolts P/N 20-057-12-48D or 20-057-12-50D installed.
97-17-06Bell Helicopter Textron, Inc. Model 214ST HelicoptersSep 24, 1997Airframe (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.
97-15-04Bell Helicopter Textron, Inc. Model 214B, 214B-1, and 214ST HelicoptersAug 19, 1997Airframe (214ST)Only with: Main transmission upper planetary carrier P/N 214-040-077-007 or 214-040-077-101 installed.
97-06-02Bell Helicopter Textron, Inc. Model 214B, 214B-1 and 214ST HelicoptersApr 16, 1997Airframe (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).
96-07-12Bell Helicopter Textron, Inc., Model 214ST HelicoptersMay 10, 1996Airframe (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 (20)

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 drive · stud · brokenOct 29, 2016

    DURING SCHEDULED INSPECTION, FOUND BROKEN STUD FROM FORWARD RIGHT HAND OUTBOARD COMBINING GEARBOX MOUNT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · panel · crackedJul 2, 2016

    FUSELAGE LOWER PANEL BELOW LEFT FUEL BLADDER HAS A 30 INCHES LONGITUDINAL CRACK.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin panel · crackedJul 2, 2016

    DURING A POST FLIGHT INSPECTION, FUSELAGE LOWER PANEL, BELOW LT FUEL BLADDER FOUND TO HAVE A 30" LONGITUDINAL CRACK.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Engine fuel and control · ecu · faultyMay 12, 2016

    ENGINE 1 INDICATED EXCESSIVE TORQUE SPLIT WITH YAW MOTION OF THE ACFT. ENG 1 THROTTLE WAS MANUALLY BROUGHT DOWN TO 10% BELOW NR 2 & SAFELY RETURNED TO BASE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · elbow · wornDec 23, 2014

    OIL COOLER CAUTION PANEL LIGHT CAME ON DURING FLIGHT. ENGAGED SECONDARY OIL COOLER SYS & RETURNED TO BASE IAW EMER PROCEDURES IN ROTOR FLIGHT CRAFT MANUAL.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · skin · crackedMay 16, 2014

    FOUND CRACK IN SKIN OF RT ELEVATOR. CRACK IS LOCATED AT THE AFT INBD BOTTOM SIDE OF THE ELEVATOR, JUST FWD OF THE RIVETS ATTACHING THE TAB.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · fitting · crackedAug 21, 2013

    CRACK ON THE VERTICAL SPAR OF THE TAIL IT IS LOCATED IN THE COLD WORK AREA JUST ABOVE THE OUTPUT QUILL OF THE 42 DEG GEARBOX. LOCATED ON THE LEFT SIDE AT BS 569.689, WL 95 ON FIN STATION 32. CRACK IS .040 DEEP AND 1.1 INCHES LONG.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · line · leakingJul 30, 2005

    ENROUTE, A HOWLING NOISE STARTED AND BECAME LOUDER, THE PILOT NOTICED NR 1 HYD PRESSURE FLUCTUATED BETWEEN 200-300 PSI. THE PILOT TURNED OFF NR 1 HYD NOISE WENT AWAY. UPON LANDING THE MECHANIC FOUND NR 1 PRESSURE LINE TO THE COLLECTIVE SERVO IS LEAKING. HE TIGHTENED THE LINE AND REPLACED THE HYD…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Starting · starter · brokenJul 4, 2003

    REPAIR DUE TO THE STARTER WOULD NOT ENGAGE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Autoflight · amplifier · will not testJun 29, 2003

    NR 2 ELEVATOR WILL NOT TEST AND ALSO KICKS OFF.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 20 reports.

Related aircraft

Show all 8 related aircraft
All 19 registered Bell 214ST aircraft

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

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