AD 68-15-02

final rule
Data completeness: 70%

Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Models 744, 745D and 810 Series Airplanes

AD Number
68-15-02
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 744 Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Models 744, 745D and 810 Series Airplanes
aircraft Vickers-Armstrongs (Aircraft Limited) Viscount 745D Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Models 744, 745D and 810 Series Airplanes
aircraft Vickers-Armstrongs (Aircraft Limited) Viscount 810 Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Models 744, 745D and 810 Series Airplanes

Unsafe Condition

Cracks in the elevator root and ribs P/Ns 60920-65, 60920-63, 72420-11 for Models 744 and 745D, and 81020 Shts. 81 and 83 for Model 810.

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

Required Actions

Inspect the root end ribs for cracks visually in accordance with specified technical leaflets. Repair/reinforce cracks within 10 landings if detected. Incorporate repair/reinforcement within 3,000 landings if not done earlier. Repeat inspections at intervals not exceeding 475 or 3,000 landings depending on repair status.

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

Compliance Time

Within the next 150 landings after the effective date (July 23, 1968) for airplanes with 7850+ landings; prior to 8000 landings for those with less. Subsequent inspections at intervals not exceeding 475 landings. Repair/reinforcement must be done within 10 landings if cracks found or within 3,000 landings otherwise.

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

Affected Aircraft

Vickers-Armstrongs (Aircraft Limited) Viscount Models 744, 745D, and 810 Series airplanes.

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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