AD 59-22-02

final rule
Data completeness: 60%

Airworthiness Directives; VICKERS Model 810 Series Aircraft

AD Number
59-22-02
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

A gap of less than 0.25 inch between the end of No. 3 flap and the aileron may produce a condition where the flap could foul or contact the inboard end of the aileron under certain flight conditions.

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

Required Actions

Inspect for adequate clearance between the outboard end of the No. 3 flap at the No. 4 flap beam unit and the inboard end of the aileron on both sides. Modify the outboard end of the No. 3 flap to provide proper clearance if the gap is less than 0.25 inch.

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

Compliance Time

Within the next 500 flight-hours but not later than December 15, 1959

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

Affected Aircraft

All Viscount 810 Series Aircraft which do not embody Modification FG.1447

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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