AD 70-03-01

Active

Nose Landing Gear Locking Lever

Print / Email Back to ADs
Key Information
70-03-01
Active
February 22, 1970
Not specified
Unknown
39-928
Applicability
["Aircraft"]
["Small Airplane"]
de Havilland Aircraft Co., Ltd., The
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
Regulatory Text

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.

AD Assistant

Get AI-powered answers about this AD, check applicability, and find compliance steps.

Sign Up to Unlock
References
This information is not available.
--- - Part 39
FAA Documents
View Official AD on FAA Website Opens in new tab