- Effective
- December 10, 1977
- Models
- B.206 Series 1, B.206 Series 2
- Data sheet
- TCDSA11EU
- Registered aircraft
- 4 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-3076
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 | 21 KB | e35d29cf…0964c63 | FAA DRS (API key needed) |
On this page
The airworthiness directive
77-23-05 SCOTTISH AVIATION, LTD. (Formerly BEAGLE AVIATION, LTD.): Amendment 39-3076. Applies to Beagle Model B206 Series 1 and Series 2 airplanes, certificated in all categories.
Compliance is required as indicated.
To prevent possible fatigue failure of the outer wing, wing center section, and empennage assemblies, accomplish the following:
(a) Prior to the accumulation of 11,000 hours total time in service on the outer wing, wing center section, or empennage assemblies, replace the affected assembly with an assembly of the same part number, or a part number approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Region, which has accumulated less than 11,000 hours total time in service.
(b) Operators who have not kept records of hours of time in service on any assembly to which a provision of this AD applies shall substitute airplane hours time in service in lieu thereof.
(Scottish Aviation, Limited, Mandatory Service Bulletin No. B206/54, dated October 21, 1975, covers the same subject.)
This amendment becomes effective December 10, 1977.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 4
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1966 | 1 |
|---|---|
| 1969 | 1 |
| 1975 | 1 |
1 with no year recorded