AD 69-11-04

final rule
Data completeness: 70%

Airworthiness Directives; Bell Model 206A Helicopters

AD Number
69-11-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Bell Helicopter Textron Canada Limited 206A Airworthiness Directives; Bell Model 206A Helicopters

Unsafe Condition

Unbalanced directional control pedal forces at cruise flight could cause pedal creep and interference between the pilots' feet and protruding head screws in the instrument console.

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

Required Actions

Install and adjust spring P/N 206-001-721 and friction clamp P/N 206-001-710; inspect and adjust the spring and clamp if not done in last 50 hours; replace protruding head screws with flat head screws using specified service bulletins or FAA-approved methods.

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

Compliance Time

within 50 hours' time in service after the effective date of this AD

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

Affected Aircraft

Bell Helicopter Textron Canada Limited Model 206A helicopters

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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