- Effective
- January 19, 1976
- 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
- 39-2473
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 | 5c7d8a92…eaeb600 | FAA DRS (API key needed) |
On this page
The airworthiness directive
75-27-01 HAWKER SIDDELEY AVIATION LTD: Amendment 39-2473. Applies to DH-104 Series airplanes certificated in all categories except those modified in accordance with Hawker Siddeley Modification 1723.
Compliance is required within the next 250 hours' time in service after the effective date of this AD, unless already accomplished.
To prevent cracking of the nose gear and main gear adjusting screws, replace the three adjusting screws, P/N 4U.493, with new adjusting screws, P/N 4U.567, in accordance with paragraph No. 5 of Hawker Siddeley Technical News Sheet No. 231, dated March 19, 1973, or with FAA-approved equivalent parts and procedure.
This amendment becomes effective on January 19, 1976.
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.