- Effective
- February 22, 1970
- Models
- 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 and 4 more
- Data sheet
- TCDSA-807
- Registered aircraft
- 3 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-928
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| FAA DRS HTML | 19 KB | 1349b8cb…e5365d3 | FAA DRS (API key needed) |
On this page
The airworthiness directive
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.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 3
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.