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Aircraft record

N5000G1978 Bell 206L-1

Registration validUnclaimedSource: FAA, updated Oct 16, 2026

Safety record in brief:No NTSB accidents or incidents since 198222 ADs may apply8 service difficulty reports

Registration
Valid
expires Jul 31, 2033
Based in
Ashland, OR
owner city / state
Owners
1
since 2026
NTSB events
None
since 1982
ADs may apply
22
confirm with A&P
Service reports
8
since 1995

Registration

FAA Aircraft Registry · Oct 16, 2026
Registered owner
Timberland Helicopters INC
Owner type
Corporation
City, state
Ashland, OR
Certificate issued
Jul 8, 2026
Expires
Jul 31, 2033
Airworthiness
Standard · Normal
Airworthiness date
Jul 24, 1978

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
206L-1
Year
1978
Serial number
45163
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
7
Engines
1
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
H2SW
Mode S code
A63C4F

Engine

Make and model
Allison 250 Ser 400hp
Type
Turbo-shaft
Power
400 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. 2026 – nowTimberland Helicopters INCAshland, OR · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 16, 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 (22)

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 (206L-1)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.
2019-08-10Bell Helicopter Textron Canada Limited HelicoptersJun 24, 2019Airframe (206L-1)
2018-25-17Air Comm Corporation Air Conditioning SystemsJan 22, 2019Airframe (206L-1)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 (206L-1)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.
2015-12-02Bell Helicopter Textron Canada LimitedJul 14, 2015Airframe (206L-1)Certain serial numbers: 206L-3 51001–51612; 206L-4 52001–52313. Only with: 206L-1 only with Engine Upgrade Kit P/N 206-706-520-101 installed; 206L-3 and 206L-4 excluded if Rolls-Royce 250-C20R engine installed under STC No. SR00036SE.
Show all 22 ADs
ADSubjectEffectiveApplies to
2014-02-02Bell Helicopter Textron Canada Limited (Bell) HelicoptersMar 7, 2014Airframe (206L-1)Serial numbers per Bell Helicopter Alert Service Bulletin No. 206L-09-163, Revision A, Tables 1 and 2. Only with: Main rotor blade P/N 206-015-001-115, -117, -119, or -121 installed with S/N listed in the ASB.
2013-25-10Bell Helicopter Textron Canada Limited HelicoptersJan 31, 2014Airframe (206L-1)Only with: Upper left attachment fitting part number 206-032-409-001 installed.
2013-22-21Bell Helicopter Textron, Inc., HelicoptersDec 13, 2013Airframe (206L-1)Only with: Apical Industries, Inc. emergency float kit installed under STC SR01535LA.
2013-18-06Bell Helicopter Textron Canada Limited (Bell) HelicoptersOct 17, 2013Airframe (206L-1)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.
2013-02-01Bell Helicopter Textron Canada Limited (Bell) HelicoptersFeb 7, 2013Airframe (206L-1)Certain serial numbers: 206L-4 52001–52430. Only with: Hydraulic servo actuator assembly P/N 206-076-062-103 installed.
2012-12-11Bell Helicopter Textron Canada, Limited, HelicoptersJul 24, 2012Airframe (206L-1)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 (206L-1)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.
96-18-05 R1Bell Helicopter Textron Canada Model 206L, 206L-1, and 206L-3 HelicoptersDec 21, 2010Airframe (206L-1)Only with: Tailboom P/N 206-033-004-003, -011, -45, -045, or -103 installed.
2009-07-52Bell Helicopter Textron Canada Limited Model 206A Series, 206B Series, 206L Series, 407…May 1, 2009Airframe (206L-1)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 (206L-1)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 (206L-1)Only with: Upper left-hand tailboom attachment CRES steel fitting P/N 407-030-750-103 installed.
2008-14-06Bell Helicopter Textron Canada Model 206L, L-1, L-3, L-4, and 407 HelicoptersAug 14, 2008Airframe (206L-1)Only with: Horizontal stabilizer P/N 206-023-119-167 installed (206L series models) or P/N 407-023-801-109 installed (Model 407).
2004-22-13Bell Helicopter Textron Canada Model 206L-1 and 206L-3 HelicoptersDec 7, 2004Airframe (206L-1)Only with: With IFR Kit P/N 206-705-001, -101, or -103 and magnetic brake P/N 204-001-376-003 (Memcor Truohm P/N MP 498-3) installed.
2003-13-14Bell Helicopter Textron Canada Model 206A, 206A-1, 206B, 206B-1, 206L, 206L-1, 206L-3…Aug 12, 2003Airframe (206L-1)
2002-25-07Bell Helicopter Textron Canada Limited Model 206L, L-1, L-3, and L-4 HelicoptersJan 27, 2003Airframe (206L-1)Certain serial numbers: 206L 45004–45049; 206L 45051–45153; 206L 46601–46617; 206L-1 45154–45790; 206L-3 51001–51612; 206L-4 52001–52163; …. Only with: Tailboom P/N 206-033-004 all dash numbers installed, except P/N 206-033-004-181.
81-18-01 R1Bell Helicopter Textron, Inc. Model 206A, 206B, 206A-1, 206B-1, 206L, and 206L-1…Dec 11, 2001Airframe (206L-1)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 (206L-1)

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

Service Difficulty Reports (8)

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 · rivet · looseApr 17, 2019

    DURING SCHEDULED INSPECTION WORKING RIVETS WERE FOUND IN CABIN ROOF STRUCTURE STATION 142. THIS IS A COMMON LOCATION FOR WORKING FASTENERS IN THE 206 SERIES AIRCRAFT, ESPECIALLY ON HIGH TIME FUSELAGES. DISCREPANT FASTENERS REPLACE IAW DER STRUCTURAL ENGINEERING REPORT FW-THI709-91 AND BHT-ALL-SRM…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · stiffener · crackedMar 16, 2018

    CRACKS AT SEAT-PAN ATTACHMENT NUTPLATE LOCATION ON TOP FRONT STIFFENER OF CREW SEAT FORWARD BULKHEAD. REPLACED IAW STANDARD RIVETING PRACTICES.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · fitting · crackedAug 10, 2015

    CRACKS RUN FROM 1ST RIVET TO EDGE OF FITTING, ABOUT .5". THE INSPECTION OF THIS PART IS SPECIFICALLY DETAILED IN MFG INSPECTION CHECKLIST. LIKELY CAUSE IS AGE OF ACFT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 8 reports
  • Fuselage · fitting · crackedAug 2, 2015

    DURING SCHEDULED 100 HR INSPECTION, FOUND UPPER LT FUSELAGE, SIDE TAILBOOM MOUNT FITTING, PN 206-031-329-103 CRACKED. INSPECTION OF THIS PART IS ROUTINE IN THE CHECKLIST FOR 100 HR INSPECTION, REF BHT-206L1-MM-1, 5/19, 5-20. THIS PART APPEARED TO BE ORIGINAL EQUIPMENT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor drive · retainer · brokenApr 23, 1999

    THE NYLON RETAINER FOR THE PLANATARY GEAR BEARING WAS FOUND IN THE TRANSMISSION OIL SCREEN IN SMALL PIECES. SUBMITTER STATED THIS IS THE FOURTH TRANSMISSION IN THE LAST 6 MONTHS WITH THIS PROBLEM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor drive · retainer · crackedFeb 28, 1998

    UPON TEAR-DOWN OF TRANSMISSION FOR INSPECTION, SCREEN ASSY WAS FULL OF NYLON PIECES. INVESTIGATION REVEALED RETAINERS ON PLANETARY GEAR, 1 EACH, COMPLETELY MISSING AND, 2 EACH, CRACKED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor · drive link · wornJan 21, 1998

    INSPECTION FOUND DRIVE LINK ASSY WITH EXCESSIVE PLAY AT TWO PLACES. SEE BELL MM L-3 FIG 62-21. ON TEAR DOWN, FOUND BEARINGS AND SPACERS WORN BEYOND LIMITS. TOTAL TIME OF PARTS, LESS THAN 1,000 HRS/1 YEAR SINCE REPLACEMENT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor · drive link · wornApr 13, 1996

    PLAY IN EXCESS OF .025 INCH AT TWO PLACES. SEE BELL MM L3, FIGURE 62.21. AT TEAR DOWN FOUND BEARINGS AND SPACERS WORN. TOTAL TIMES LESS THAN 1,000 HOURS AND 1 YEAR SINCE REPLACED.

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

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 16, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 16, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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