- Effective
- December 7, 1977
- Model
- HS 748 Series 2A
- Data sheet
- TCDSA24EU
- Registered aircraft
- 2 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-3072
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 | d553b4da…87a9998 | FAA DRS (API key needed) |
On this page
The airworthiness directive
77-23-02 HAWKER SIDDELEY AVIATION, LIMITED: Amendment 39-3072. Applies to Hawker Siddeley Aviation Limited H.S. 748 Series 2A airplanes certificated in all categories.
Compliance is required within the next 300 hours time in service after the effective date of this AD, unless already accomplished.
To prevent failure of propeller feathering, install an electrical back-up to the primary manual feathering system in accordance with the instructions contained in Hawker Siddeley Aviation Service Bulletin No. 61/18, Modification 4609, as revised April 11, 1974, or an equivalent approved by the Chief, Aircraft Certification Staff, AEU-100, Europe, Africa, and Middle East Region, FAA, c/o American Embassy, APO New York, N.Y. 09667.
This amendment becomes effective December 7, 1977.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 2
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.