Skip to content
KnownTail
Aircraft record

N825H1984 Bell 214ST

Registration validUnclaimedSource: FAA, updated Oct 19, 2026

Safety record in brief:No NTSB accidents or incidents since 198210 ADs may apply10 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
10
since 1995

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
Jan 6, 2010

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
1984
Serial number
28137
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
AB441D

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
  2. until 1935Individual ownerNew York, NY · different airframe: Moth 60-Gm S/N 1-N

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 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 (10)

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.

  • Fuselage · support · crackedOct 30, 2018

    PN 214-031-240-173 SUPPORT FOUND CRACKED DURING AIRFRAME INSPECTION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor · erosion shield · debondedMay 26, 2017

    DURING PREVENTATIVE TOUCH UP PAINT ON MAIN ROTOR BLADE, DISCOVERED LOWER BLADE EROSION PLATE DEBONDED AT BOND LINE

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · support · crackedAug 7, 2016

    DURING POST FLIGHT DISCOVERED A 4" SKIN CRACK IN FUSELAGE AFT OF RT PILOT DOOR. DURING HIDDEN DAMAGE INSPECTION, FOUND CRACKED BULKHEAD DOOR POST SUPPORT AT STA 142.50, WL 22.00, BL 40.0.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · beam · crackedApr 20, 2016

    DURING INSPECTION OF AIRFRAME FOR SUSPECTED CAUSE FOR TWO REV VIBRATIONS, FOUND A 4.9 INCH X1.25 INCH CRACK IN THE LT BAGGAGE COMPARTMENT & ENG DECK AT FS STATION 278 - 280. FUSELAGE LT UPPER BEAM CAP IS CRACKED IN LT BAGGAGE COMPARTMENT & UNDER ENG DECK.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor drive · case · crackedNov 1, 2013

    DURING INVESTIGATION OF AN OIL LEAK, A CRACK WAS FOUND IN THE MAIN TRANSMISSION UPPER LEFT HAND RING GEAR CASE .

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · hanger assy · mismanufacturedNov 2, 2001

    WILL NOT FIT IN SUPPORT ON AIRCRAFT. HOLES MILLED IN WRONG AREA.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · panel · mismanufacturedAug 17, 1998

    THREE EACH DOUBLER RINGS ON BOTTOM OF PANEL BONDED ON 180 DEGREES OUT - SLOT ON RING NEEDS TO BE FACING OUTBOARD AND AFT CENTER ACCESS HOLE SEPARATED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · track · mismanufacturedJul 30, 1998

    LOWER OUTBOARD FLANGE TOO NARROW TO PICK UP FASTENERS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · track · mismanufacturedJul 21, 1998

    LOWER OUTBOARD FLANGE TOO NARROW TO PICK UP FASTENERS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · stiffener · mismanufacturedJul 21, 1998

    STIFFENER MISMANUFACTURED. PART DOESN'T FIT THE POSITION ON THE AIRFRAME.

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

Related aircraft

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

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

Request owner name removalReport an error in this record

Claim this airplaneWatch