AD 59-06-06

final rule
Data completeness: 60%

Airworthiness Directives; VICKERS Model 810 Series Aircraft

AD Number
59-06-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Vickers-Armstrongs (Aircraft Limited) Viscount 810 Airworthiness Directives; VICKERS Model 810 Series Aircraft

Unsafe Condition

Manufacturing error on bearing channel 81003-1061 may cause distortion or cracks on vertical bearing channel at wheel bay side of outer rib of inboard nacelles.

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

Required Actions

Inspect for distortion or cracks on vertical bearing channel 81003-1061 every 135 flying hours until outer rib reinforcement is incorporated. Incorporate outer rib reinforcement by July 1, 1959.

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

Compliance Time

Within 135 flying hours and every subsequent 135 flying hours until the outer rib reinforcement is incorporated. The outer rib reinforcement must be incorporated by July 1, 1959.

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

Affected Aircraft

Vickers-Armstrongs (Aircraft Limited) Viscount 810 Series Aircraft

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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