| AD Number | 70-03-01 | Status | Active |
| Effective Date | February 22, 1970 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-928 |
| Product Type | ["Aircraft"] | Product Subtype | ["Small Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | de Havilland Aircraft Co., Ltd., The |
| Model(s) | D.H. 104 Dove Series 1A D.H. 104 Dove Series 2A D.H. 104 Dove Series 5A D.H. 104 Dove Series 5BA D.H. 104 Dove Series 6A D.H. 104 Dove Series 6BA D.H. 104 Dove Series 7A D.H. 104 Dove Series 7AXC D.H. 104 Dove Series 8A D.H. 104 Dove Series 8AXC |
70-03-01 HAWKER SIDDELEY: Amdt. 39-928. Applies to Hawker Siddeley Dove Model DH-104 airplanes.
Compliance is required within the next 300 landings after the effective date of this AD, unless already accomplished.
To prevent fatigue failure of the nose landing gear locking lever and jack attachment lever, replace the existing nose landing gear locking lever and jack attachment lever with Modification 978 levers in accordance with Hawker Siddeley Technical News Sheet Series CT(104) No. 155, Issue 4, dated 29 September 1969, or an FAA-approved equivalent.
This amendment becomes effective February 22, 1970.