AD 69-08-08

final rule
Data completeness: 70%

Airworthiness Directives; Fairchild-Hiller Models UH-12D, UH-12E, UH-12E-L, UH-12L and UH-12L4 Helicopters

AD Number
69-08-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12D Airworthiness Directives; Fairchild-Hiller Models UH-12D, UH-12E, UH-12E-L, UH-12L and UH-12L4 Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12L Airworthiness Directives; Fairchild-Hiller Models UH-12D, UH-12E, UH-12E-L, UH-12L and UH-12L4 Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12L4 Airworthiness Directives; Fairchild-Hiller Models UH-12D, UH-12E, UH-12E-L, UH-12L and UH-12L4 Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12E Airworthiness Directives; Fairchild-Hiller Models UH-12D, UH-12E, UH-12E-L, UH-12L and UH-12L4 Helicopters
aircraft Hiller Aviation | Siam Hiller Holdings, Inc. UH-12E-L Airworthiness Directives; Fairchild-Hiller Models UH-12D, UH-12E, UH-12E-L, UH-12L and UH-12L4 Helicopters

Unsafe Condition

Fatigue failures of the tail rotor yoke, P/N 55046 and P/N 55046-5.

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

Required Actions

Conduct a magnetic-particle inspection and measure the tail rotor yoke fillet radius within 10 hours time in service after the effective date. If a crack is found or the fillet radius is less than 0.030 inches, remove the yoke from service. For fillet radii between 0.030 and 0.050 inches, conduct subsequent inspections every 50 hours and remove the yoke within 250 hours. Ensure replacement yokes have a fillet radius of at least 0.050 inches.

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

Compliance Time

within the next 10 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

Fairchild-Hiller Models UH-12D, UH-12E, UH-12E-L, UH-12L, and UH-12L4 helicopters with P/N 55046 and P/N 55046-5 tail rotor yokes.

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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