AD 62-22-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Vickers-Armstrongs (Aircraft Limited) | Viscount 744 | Airworthiness Directives; VICKERS Model 700 Series Aircraft |
| aircraft | Vickers-Armstrongs (Aircraft Limited) | Viscount 745D | Airworthiness Directives; VICKERS Model 700 Series Aircraft |
Unsafe Condition
Wing flap attachment difficulties due to cracking of bolts and flap support attachment fittings.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace specific bolts with new ones every 1,500 or 2,500 landings depending on part number. Inspect for cracks in flap support attachment fittings at specified intervals. Incorporate Modification D.2175 within 400 hours' time in service and replace cracked fittings.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Compliance required as indicated.
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Affected Aircraft
Vickers-Armstrongs (Aircraft Limited) Viscount 700 Series Aircraft (Viscount 744, Viscount 745D models).
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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