AD 68-04-02

final rule
Data completeness: 70%

Airworthiness Directives; Bell Model 206A Helicopters

AD Number
68-04-02
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

Failure of the exhaust stack clamps which attach the exhaust ducts to the engine exhaust flanges could cause hazardous damage to the main rotor or the tail rotor.

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

Required Actions

Replace exhaust stack clamps P/N N3657 with National Utilities Corporation P/N 4656AA. Install new clamps with studs facing outboard, tighten nuts evenly to 30 inch-pounds, and safety wire nuts using P/N MS20995C32. Repeat torque checks until torque is maintained at 30 inch-pounds after shaking the stack and tapping the clamp with a plastic mallet.

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

Compliance Time

within the next 25 hours time in service after the effective date of this Airworthiness Directive

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, Serial Numbers 4 through 110, 112 through 116, 118, 119, 122, 124 through 126, 128, 129 and 133.

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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