AD 73-19-09

final rule
Data completeness: 70%

Airworthiness Directives; Bell Model 206A, 206B, 206A-1 and 206B-1 Helicopters

AD Number
73-19-09
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, 206B, 206A-1 and 206B-1 Helicopters
aircraft Bell Helicopter Textron Canada Limited 206A-1 (OH-58A) Airworthiness Directives; Bell Model 206A, 206B, 206A-1 and 206B-1 Helicopters
aircraft Bell Helicopter Textron Canada Limited 206B Airworthiness Directives; Bell Model 206A, 206B, 206A-1 and 206B-1 Helicopters
aircraft Bell Helicopter Textron Canada Limited 206B-1 Airworthiness Directives; Bell Model 206A, 206B, 206A-1 and 206B-1 Helicopters

Unsafe Condition

Corrosion and cracks in the main rotor blade pitch link tubes, P/N 206-010-330, could result in failure of the pitch link assemblies.

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

Required Actions

Inspect the ends and outside diameter surface of each tube for corrosion and cracking using a 3 power or higher magnifying glass. Replace corroded or cracked tubes prior to next flight, except under FAR 21.197. Track main rotor blades after replacement or adjustment. Apply corrosion preventive compound as specified. Adjust inspection intervals upon FAA approval.

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

Compliance Time

within 25 hours time in service after the effective date of this A.D., unless previously accomplished and thereafter at intervals not to exceed 50 hours time in service from the last inspection

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

Affected Aircraft

Bell Model 206A, 206B, 206A-1 and 206B-1 helicopters equipped with main rotor blade pitch link assemblies P/N 206-010-330 and 206-010-342

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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