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Aircraft record

N346981994 Bell 206B

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Nov 14, 2012.

Safety record in brief:1 NTSB accident (destroyed damage, Aug 2004)20 ADs may apply3 service difficulty reports

Registration
Deregistered
Last based in
Portland, OR
owner city / state
Owners
1
since 1995
NTSB events
1
destroyed, 2004
ADs may apply
20
confirm with A&P
Service reports
3
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Last registered owner
United States Department Of Energy
Owner type
Government
City, state
Portland, OR
Certificate issued
Jun 8, 1995
Canceled
Nov 14, 2012
Airworthiness
Standard · Normal
Airworthiness date
Dec 14, 1994

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
206B
Year
1994
Serial number
4324
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
5
Engines
1
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
H2SW
Mode S code
A3D74C

Engine

Make and model
Allison 250-C20 Ser
Type
Turbo-shaft
Power
420 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. 1995 – 2012United States Department Of EnergyPortland, OR
  2. 1970 – 1971Individual ownerDayton, OH · different airframe: Stinson 10a S/N 7998
  3. 1946 – 1948Colonial Airlines INCNew York, NY · different airframe: Douglas Dc3d-R-1830-90c S/N 42964

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 (1)

Accident · destroyed

Aug 17, 2004 · Mead, WA

The reversal of the reel machine during a sock line pull which resulted in a loss of control while hovering out of ground effect. Factors were the failure of company management to develop adequate procedures for conducting sock line pulls, the inadequate communication between the chief pilot and the pilot, the inadequate communication between the ground personnel and the pilot, and the pilot's…

Damage
Destroyed
Injuries
Fatal
Report
SEA04TA163

From NTSB records; matched by serial number.Read NTSB report (search CAROL for SEA04TA163)

Accident history for this model

ADs published since 1998 that may apply (20)

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
2021-15-06Bell Textron Canada Limited (Type Certificate Previously Held by Bell Helicopter Textron…Aug 27, 2021Airframe (206B)Certain serial numbers: 206A 004–660; 206A 672–715; 206L 45004–45153; 206L 46601–46617; 206L-1 45154–45790; 206L-3 51001–51612. Only with: Model 206B all serial numbers including those converted from Model 206A; Model 206L-4 all serial numbers.
2021-11-01Bell Textron Canada Limited HelicoptersJul 15, 2021Airframe (206B)Certain serial numbers: 206B 004–4690; 206L 45001–45153; 206L 46601–46617. Only with: Model 206B includes helicopters converted from Model 206A and helicopters with a 206B3 designation.
2019-08-10Bell Helicopter Textron Canada Limited HelicoptersJun 24, 2019Airframe (206B)
2018-25-17Air Comm Corporation Air Conditioning SystemsJan 22, 2019Airframe (206B)Only with: Air Comm air conditioning system installed: P/N AS350-202-1 through -5 or AS350-204-1 through -12 (AS350), EC130-202-1 through -8 (EC130B4), 206EC-200 through 206EC-212 (Bell 206), or 407 EC-201 through 407 EC-203 (Bell 407).
2017-05-04Bell Helicopter Textron Canada Limited HelicoptersMar 17, 2017Airframe (206B)Only with: Tension-torsion strap P/N 206-011-147-005 with S/N BTFS-23868 through BTFS-24277 or P/N 206-011-147-007 with S/N BT-22719 through BT-23437 installed.
Show all 20 ADs
ADSubjectEffectiveApplies to
2013-22-21Bell Helicopter Textron, Inc., HelicoptersDec 13, 2013Airframe (206B)Only with: Apical Industries, Inc. emergency float kit installed under STC SR01535LA.
2013-18-06Bell Helicopter Textron Canada Limited (Bell) HelicoptersOct 17, 2013Airframe (206B)Only with: Applies only to helicopters with specified flight control bellcrank, link, idler, bearing, swashplate link, or engine bipod mount fitting assemblies (various P/Ns by model) installed.
2012-12-11Bell Helicopter Textron Canada, Limited, HelicoptersJul 24, 2012Airframe (206B)Only with: Modified with Aviation Specialties Unlimited, Inc. (ASU) Night Vision Imaging System (NVIS) lighting installed per STC SR01383SE.
2010-26-51Bell Helicopter Textron Canada Limited (BHTC) Model 206A, 206B, 206L, 206L-1, 206L-3…Mar 25, 2011Airframe (206B)Serial numbers per RBI document attached to Bell Helicopter Textron ASBs 206-07-116, 206L-07-148, 222-07-106, 222U-07-77, 230-07-38, 407-07-81, 427-07-18, 430-07-41. Only with: Tail rotor blade with part number and serial number listed in the RBI document attached to the Bell ASBs installed.
2009-07-52Bell Helicopter Textron Canada Limited Model 206A Series, 206B Series, 206L Series, 407…May 1, 2009Airframe (206B)Only with: Model 206A/206B/206L series with cyclic control lever assembly P/N 206-001-401-111, 206-001-400-115, or 206-001-400-111, and Model 407/427 with lever assembly P/N 407-001-320-105 or 407-001-320-109, with less than 50 hours TIS.
2009-08-03Bell Helicopter Textron Canada Limited Model 206A, 206B, 206L, 206L-1, 206L-3, 206L-4…Apr 24, 2009Airframe (206B)Serial numbers per Rotor Blades, Inc. (RBI) document attached to Bell Helicopter Textron ASBs 206-07-116, 206L-07-148, 222-07-106, 222U-07-77, 230-07-38, 407-07-81, 427-07-18, 430-07-41. Only with: Tail rotor blade installed with a part number and serial number listed in the RBI document attached to the applicable Bell ASB.
2008-14-03Bell Helicopter Textron Canada Model 206A, 206B, 206L, 206L-1, 206L-3, and 206L-4…Aug 14, 2008Airframe (206B)Only with: Upper left-hand tailboom attachment CRES steel fitting P/N 407-030-750-103 installed.
2007-25-07Bell Helicopter Textron Canada Limited Model 206A and 206B HelicoptersJan 14, 2008Airframe (206B)Certain serial numbers: 0004–3906. Only with: Two-piece vertical stabilizer (fin) supports P/N 206-031-417-003 or -007, or P/N 206-031-418-001 or -005, installed.
2007-23-17Bell Helicopter Textron Canada Model 206A and 206B HelicoptersDec 6, 2007Airframe (206B)Certain serial numbers: …–3216. Only with: Main rotor latch bolt P/N 206-010-169-001, 206-010-169-003, or 206-011-122-003 installed.
2006-16-04Rolls-Royce Corporation (Formerly Allison Engine Company, Allison Gas Turbine Division…Sep 7, 2006Engine (250-C20 SER)
2006-13-06Rolls-Royce Corporation (Formerly Allison Engine Company, Allison Gas Turbine Division…Jul 26, 2006Engine (250-C20 SER)Only with: Engines with gas producer rotor assembly tie bolt P/Ns A23008020, E23008020 (EXTEX), 23008020, 6843388, 6876991 (RRC), A23008020 (SAP), or 23008020P (Pacific Sky Supply) installed.
2005-10-13Rolls-Royce Corporation (Formerly Allison Engine Company) 250-B17B, -B17C, -B17D, -B17E…Jun 22, 2005Engine (250-C20 SER)Only with: Engines that do not have turbine energy absorbing ring RRC P/N 23035175, or an equivalent FAA-approved serviceable ring, installed.
2003-13-14Bell Helicopter Textron Canada Model 206A, 206A-1, 206B, 206B-1, 206L, 206L-1, 206L-3…Aug 12, 2003Airframe (206B)
81-18-01 R1Bell Helicopter Textron, Inc. Model 206A, 206B, 206A-1, 206B-1, 206L, and 206L-1…Dec 11, 2001Airframe (206B)Only with: Main rotor trunnion P/N 206-010-104-3, 206-011-113-001, 206-011-120-001, or 206-011-113-103 installed.
95-09-06Bell Helicopter Textron, Inc. Model 206A, 206B, 206L, 206L-1, and 206L-3 HelicoptersJun 8, 1995Airframe (206B)

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (3)

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 · engine · malfunctionedJun 23, 2001

    DEPARTING THE AIRPORT, THE ENGINE FLAMED OUT OR SURGED. THE ENGINE WAS RUN ON A TEST CELL. TEST CELL SHOWED: 1)A CYCLING ANTI-ICE VALVE SOLENOID. 2) A RICH FUEL FLOW. 3) A WARPED OUTER COMBUSTION CHAMBER. THIS TOGETHER, COULD CAUSE A SURGE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor drive · transmission · leakDec 21, 1995

    TRANSMISSION OIL LEAKING THROUGH CORK. CORK SEEMS SATURATED WITH OIL. APPEARS CORK NEEDS TO BE SEALED WITH SOMETHING BETTER THAN SHELLAC.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · engine · flame-outAug 25, 1995

    HELICOPTER EXPERIENCED 3 ENGINE FLAME-OUTS WITHIN APPROXIMATELY 5 MINUTES. THE AUTO RE-IGNITION STARTED THE ENGINE IN-FLIGHT EACH TIME. NORMAL LANDING WAS ACCOMPLISHED. A COMPLETE INSPECTION OF THE FUEL SYSTEMS, CONTROL SYSTEMS, FUEL FILTERS, AIR FILTERS, FUEL NOZZLE, FUEL CONTROL, GOVERNOR, FUEL…

    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

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