AD 69-14-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Vickers-Armstrongs (Aircraft Limited) | Viscount 745D | Airworthiness Directives; VICKERS VISCOUNT Model 745D and 810 Series Aircraft |
| aircraft | Vickers-Armstrongs (Aircraft Limited) | Viscount 810 | Airworthiness Directives; VICKERS VISCOUNT Model 745D and 810 Series Aircraft |
Unsafe Condition
Fatigue damage to the inner section and center section lower wing spar booms.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the center section and inner section lower spar booms with new ones of the same part number before exceeding 90% of the approved retirement time in the Viscount Instruction Manual (dated before April 1, 1969) or within the next 250 landings, whichever occurs later. New booms must be replaced before accumulating revised retirement times per the latest manual dated after April 1, 1969.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
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Affected Aircraft
Vickers-Armstrongs (Aircraft Limited) Viscount 745D and Viscount 810 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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