N5000G1978 Bell 206L-1
Safety record in brief:No NTSB accidents or incidents since 198222 ADs may apply8 service difficulty reports
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 dataAirframe
- 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- 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, 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 (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.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2021-15-06 | Bell Textron Canada Limited (Type Certificate Previously Held by Bell Helicopter Textron… | Aug 27, 2021 | Airframe (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. |
| 2019-08-10 | Bell Helicopter Textron Canada Limited Helicopters | Jun 24, 2019 | Airframe (206L-1) |
| 2018-25-17 | Air Comm Corporation Air Conditioning Systems | Jan 22, 2019 | Airframe (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). |
| 2017-05-04 | Bell Helicopter Textron Canada Limited Helicopters | Mar 17, 2017 | Airframe (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. |
| 2015-12-02 | Bell Helicopter Textron Canada Limited | Jul 14, 2015 | Airframe (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 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2014-02-02 | Bell Helicopter Textron Canada Limited (Bell) Helicopters | Mar 7, 2014 | Airframe (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. |
| 2013-25-10 | Bell Helicopter Textron Canada Limited Helicopters | Jan 31, 2014 | Airframe (206L-1)Only with: Upper left attachment fitting part number 206-032-409-001 installed. |
| 2013-22-21 | Bell Helicopter Textron, Inc., Helicopters | Dec 13, 2013 | Airframe (206L-1)Only with: Apical Industries, Inc. emergency float kit installed under STC SR01535LA. |
| 2013-18-06 | Bell Helicopter Textron Canada Limited (Bell) Helicopters | Oct 17, 2013 | Airframe (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. |
| 2013-02-01 | Bell Helicopter Textron Canada Limited (Bell) Helicopters | Feb 7, 2013 | Airframe (206L-1)Certain serial numbers: 206L-4 52001–52430. Only with: Hydraulic servo actuator assembly P/N 206-076-062-103 installed. |
| 2012-12-11 | Bell Helicopter Textron Canada, Limited, Helicopters | Jul 24, 2012 | Airframe (206L-1)Only with: Modified with Aviation Specialties Unlimited, Inc. (ASU) Night Vision Imaging System (NVIS) lighting installed per STC SR01383SE. |
| 2010-26-51 | Bell Helicopter Textron Canada Limited (BHTC) Model 206A, 206B, 206L, 206L-1, 206L-3… | Mar 25, 2011 | Airframe (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 R1 | Bell Helicopter Textron Canada Model 206L, 206L-1, and 206L-3 Helicopters | Dec 21, 2010 | Airframe (206L-1)Only with: Tailboom P/N 206-033-004-003, -011, -45, -045, or -103 installed. |
| 2009-07-52 | Bell Helicopter Textron Canada Limited Model 206A Series, 206B Series, 206L Series, 407… | May 1, 2009 | Airframe (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. |
| 2009-08-03 | Bell Helicopter Textron Canada Limited Model 206A, 206B, 206L, 206L-1, 206L-3, 206L-4… | Apr 24, 2009 | Airframe (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. |
| 2008-14-03 | Bell Helicopter Textron Canada Model 206A, 206B, 206L, 206L-1, 206L-3, and 206L-4… | Aug 14, 2008 | Airframe (206L-1)Only with: Upper left-hand tailboom attachment CRES steel fitting P/N 407-030-750-103 installed. |
| 2008-14-06 | Bell Helicopter Textron Canada Model 206L, L-1, L-3, L-4, and 407 Helicopters | Aug 14, 2008 | Airframe (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). |
| 2004-22-13 | Bell Helicopter Textron Canada Model 206L-1 and 206L-3 Helicopters | Dec 7, 2004 | Airframe (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. |
| 2003-13-14 | Bell Helicopter Textron Canada Model 206A, 206A-1, 206B, 206B-1, 206L, 206L-1, 206L-3… | Aug 12, 2003 | Airframe (206L-1) |
| 2002-25-07 | Bell Helicopter Textron Canada Limited Model 206L, L-1, L-3, and L-4 Helicopters | Jan 27, 2003 | Airframe (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 R1 | Bell Helicopter Textron, Inc. Model 206A, 206B, 206A-1, 206B-1, 206L, and 206L-1… | Dec 11, 2001 | Airframe (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. |
| 95-09-06 | Bell Helicopter Textron, Inc. Model 206A, 206B, 206L, 206L-1, and 206L-3 Helicopters | Jun 8, 1995 | Airframe (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 reportsShow fewer 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