| AD Number | 69-09-02 | Status | Active |
| Effective Date | May 29, 1969 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-760 |
| Product Type | ["Aircraft"] | Product Subtype | ["Large Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Vickers-Armstrongs (Aircraft Limited) |
| Model(s) | Viscount 744 Viscount 745D Viscount 810 |
69-09-02 VICKERS: Amdt. 39-760. Applies to Viscount Models 744, 745D, and 810 Series airplanes.
Compliance required within the next 1,000 hours' time in service after the effective date of this AD, unless already accomplished.
To prevent the jamming of the aileron control system due to small objects entering the control column housings through lightening holes in the housings, install covers P/N's 70133- 807, 809, 811, and 813 over the housings in accordance with British Aircraft Corp. Modification D.3223 Issue 2 dated August 10, 1968 (700 Series) or Modification FG.2098 Issue 2 dated August 20, 1968 (800/810 Series) or later ARB-approved issues or an equivalent approved by the Chief, Aircraft Certification Staff, FAA Europe, Africa, and Middle East Region.
This amendment becomes effective May 29, 1969.