AD 95-22-08
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
Reduced structural capability of the fuselage pressure vessel due to fatigue and corrosion in components of the fuselage pressure vessel.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform visual, eddy current, dye penetrant, and x-ray inspections per specified PTLs; install modifications to reduce cabin pressure maximum setting to 3.5 psi; and modify components as per applicable PTLs. Repairs must be done before further flight if cracks or corrosion are found.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Required as indicated, unless accomplished previously. Actions must be done at the later of specified intervals or within 60/30 days after the AD's effective date (November 27, 1995).
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Model Viscount 744, 745D, and 810 airplanes, certificated in any category.
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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