AD 63-26-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Vickers-Armstrongs (Aircraft Limited) | Viscount 810 | Airworthiness Directives; VICKERS Model 810 Series Aircraft |
Unsafe Condition
Fatigue failures have been reported on flap beams in the areas shown in figures 4 and 5 of Vickers Preliminary Technical Leaflet No. 107 Issue 2 (800/810 Series).
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct dye penetrant or FAA approved equivalent inspection for cracks in accordance with PTL 107 Issue 2. Reinspect at intervals not exceeding specified landings, and incorporate modification FG.1946 or repair/reinforcing scheme defined in the referenced PTL.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 200 landings after the effective date of this AD for aircraft with 10,000 or less landings, and within 50 landings after the effective date for aircraft over 10,000 landings. Reinforcing scheme must be incorporated within 2,000 landings after the effective date.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Vickers-Armstrongs (Aircraft Limited) Viscount Model 810 Series 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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.