AD 95-14-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Vickers-Armstrongs (Aircraft Limited) | Viscount 744 | Airworthiness Directives; British Aerospace Model Viscount 744, 745D, and 810 Airplanes |
| aircraft | Vickers-Armstrongs (Aircraft Limited) | Viscount 745D | Airworthiness Directives; British Aerospace Model Viscount 744, 745D, and 810 Airplanes |
| aircraft | Vickers-Armstrongs (Aircraft Limited) | Viscount 810 | Airworthiness Directives; British Aerospace Model Viscount 744, 745D, and 810 Airplanes |
Unsafe Condition
Fatigue cracking of the undercarriage bracing of the nose wheel could result in failure of the structure and fittings, and subsequent collapse of the nose landing gear.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a visual inspection and non-destructive testing (NDT) inspection of the actuator beam structure and actuator attachment fittings of the nose landing gear. If discrepancies are found, replace discrepant parts with new parts as specified in the referenced technical leaflets.
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Compliance Time
Prior to the accumulation of 2,050 landings after the effective date of this AD, or within 12 months after the effective date of this AD, whichever occurs first. Thereafter, repeat inspections at intervals not to exceed 2,050 landings.
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Affected Aircraft
British Aerospace Model Viscount 744, 745D, and 810 airplanes, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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