AD 73-12-01

final rule
Data completeness: 70%

Airworthiness Directives; Bell Model 206A and 206B Helicopters

AD Number
73-12-01
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 and 206B Helicopters
aircraft Bell Helicopter Textron Canada Limited 206A-1 (OH-58A) Airworthiness Directives; Bell Model 206A and 206B Helicopters
aircraft Bell Helicopter Textron Canada Limited 206B Airworthiness Directives; Bell Model 206A and 206B Helicopters
aircraft Bell Helicopter Textron Canada Limited 206B-1 Airworthiness Directives; Bell Model 206A and 206B Helicopters

Unsafe Condition

Fatigue cracks in the skin of the vertical fin in the area of the tail boom attachment, particularly aft of the upper rear attachment insert.

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

Required Actions

Inspect the inboard skin of the vertical fin in the area of attachment for cracks, paying particular attention to the area aft of the upper rear attachment insert. Replace or repair the fin if cracks exceed 3.5 inches in length before further flight. If cracks are less than 3.5 inches, repair or replace per Bell Helicopter Company Service Letter No. 206-203, Revision C, or FAA-approved revision before further flight. Repeat inspections at intervals not exceeding 25 hours' time in service.

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 A.D., unless already accomplished within the last 25 hours' time in service

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

Affected Aircraft

Bell Helicopter Textron Canada Limited Model 206A, 206A-1 (OH-58A), 206B, 206B-1 helicopters with serial numbers 4 through 865 and 867 through 873, equipped with vertical fin P/N 206-020-113-5, -7, or -9.

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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