| AD Number | 66-22-03 | Status | Active |
| Effective Date | September 03, 1966 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-281 |
| Product Type | ["Aircraft"] | Product Subtype | ["Large Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Textron Aviation Inc. |
| Model(s) | DH.125 Series 1A |
66-22-03 HAWKER SIDDELEY: Amdt. 39-281 Part 39 Federal Register September 3, 1966. Applies to Model DH.125-1A Airplanes Equipped With Aileron and Elevator Systems Gust Lock, P/N 25CF-1793AB.
Compliance required within the next 300 hours' time in service after the effective date of this AD, unless already accomplished.
To prevent operation with the elevator and aileron gust lock engaged, accomplish the following:
(a) Remove gust lock assembly, P/N 25CF-1793AB, located on left side of cockpit.
(b) Modify pilot's control wheel and seat rail, and install gust lock stowage box assembly, P/N 25.MM. 333, in accordance with Hawker Siddeley Aviation Ltd. Service Bulletin No. 27-34-(1716), dated May 18, 1966, or later ARB-approved issue.
(c) Equip airplane with aileron and elevator gust lock assembly P/N 25.MM. 2583.
This directive effective September 3, 1966.