AD 80-22-11

final rule
Data completeness: 70%

Airworthiness Directives; BELL Model 206 L-1 Helicopters

AD Number
80-22-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
80-ASW-44
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Bell Helicopter Textron Canada Limited 206L-1 Airworthiness Directives; BELL Model 206 L-1 Helicopters

Unsafe Condition

Fatigue failure of the main rotor grip, part number 206-011-132-009.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Replace main rotor grips with serial numbers listed in the AD. For grips with less than 1,150 hours' total time in service on the effective date, replace before accumulating 1,200 hours. For those with 1,150 or more hours, replace within 50 hours' time in service. Compliance can be achieved by following Bell Helicopter Textron Alert Service Bulletin 206L-80-15.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Prior to accumulating 1,200 hours' total time in service or within 50 hours' time in service, depending on the existing hours on the main rotor grip as of the effective date.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Bell Helicopter Textron Canada Limited Model 206L-1 helicopters with main rotor grips having the specified serial numbers listed in the AD.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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