Safety record in brief:1 NTSB accident (substantial damage, Oct 2020)17 ADs may apply2 service difficulty reports
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Improper torquing of the “B” nut at the fuel control unit, which led to a total loss of engine power and subsequent autorotation that resulted in substantial damage.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA21LA023)
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 (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. |
| 2021-11-01 | Bell Textron Canada Limited Helicopters | Jul 15, 2021 | Airframe (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. |
| 2019-08-10 | Bell Helicopter Textron Canada Limited Helicopters | Jun 24, 2019 | Airframe (206B) |
| 2018-25-17 | Air Comm Corporation Air Conditioning Systems | Jan 22, 2019 | Airframe (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). |
| 2017-05-04 | Bell Helicopter Textron Canada Limited Helicopters | Mar 17, 2017 | Airframe (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. |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2013-22-21 | Bell Helicopter Textron, Inc., Helicopters | Dec 13, 2013 | Airframe (206B)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 (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. |
| 2012-12-11 | Bell Helicopter Textron Canada, Limited, Helicopters | Jul 24, 2012 | Airframe (206B)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 (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. |
| 2009-07-52 | Bell Helicopter Textron Canada Limited Model 206A Series, 206B Series, 206L Series, 407… | May 1, 2009 | Airframe (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. |
| 2009-08-03 | Bell Helicopter Textron Canada Limited Model 206A, 206B, 206L, 206L-1, 206L-3, 206L-4… | Apr 24, 2009 | Airframe (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. |
| 2008-14-03 | Bell Helicopter Textron Canada Model 206A, 206B, 206L, 206L-1, 206L-3, and 206L-4… | Aug 14, 2008 | Airframe (206B)Only with: Upper left-hand tailboom attachment CRES steel fitting P/N 407-030-750-103 installed. |
| 2007-25-07 | Bell Helicopter Textron Canada Limited Model 206A and 206B Helicopters | Jan 14, 2008 | Airframe (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. |
| 2007-23-17 | Bell Helicopter Textron Canada Model 206A and 206B Helicopters | Dec 6, 2007 | Airframe (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. |
| 2003-13-14 | Bell Helicopter Textron Canada Model 206A, 206A-1, 206B, 206B-1, 206L, 206L-1, 206L-3… | Aug 12, 2003 | Airframe (206B) |
| 81-18-01 R1 | Bell Helicopter Textron, Inc. Model 206A, 206B, 206A-1, 206B-1, 206L, and 206L-1… | Dec 11, 2001 | Airframe (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. |
| 95-09-06 | Bell Helicopter Textron, Inc. Model 206A, 206B, 206L, 206L-1, and 206L-3 Helicopters | Jun 8, 1995 | Airframe (206B) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
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.
DURING HOVERING ON A TRAINING FLIGHT, THE PILOT NOTICED THAT TOT TEMPERATURE WAS HIGHER THAN NORMAL. AFTER TROUBLESHOOTING WHICH INCLUDED CHANGING BLEED VALVE AND CHECKING ANTI-ICE FOR PROPER CLOSING, THERE WAS NO CHANGE. POWER CHECK ON ENGINE INDICATED SUBSTANTIAL POWER LOSS. THIS WAS A RENTAL…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING DAILY CLEANING OF HELICOPTER, PILOT NOTICED WHAT APPEARED TO BE A CRACK IN TH E T/R YOKE. AFTER REMOVING PAINT AND INSPECTING WITH A MAGNIFYING GLASS, A CRACK WAS DEFINITELY VISIBLE. CRACK STARTED AT CENTER LINE OF OUTBOARD BOLT HOLE, EXTENDIING TO OUTER END OF YOKE AND STARTING TO TRAVEL…
From FAA Service Difficulty Reports; matched by N-number and serial number.