- Effective
- June 11, 1970
- Models
- BN-2, BN-2A, BN-2A-2, BN-2A-20, BN-2A-21, BN-2A-26 and 8 more
- Registered aircraft
- 52 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-1006
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 | 20 KB | c63f499b…543db11 | FAA DRS (API key needed) |
On this page
The airworthiness directive
70-12-11 BRITTEN-NORMAN, LTD: Amdt. 39-1006. Applies to BN-2 and BN-2A airplanes, serial numbers up to and including S/N C231. Compliance is required within the next 50 hours' time in service after the effective date of this AD, unless already accomplished. To prevent failure of the flap actuating system, replace flap lever drive attachment bolt P/N A111-6G with a serviceable bolt, P/N A111-9G, and replace the flap center operating lever P/N NB-45-D-997 with either - (1) A serviceable flap center operating lever P/N NB-45-D-997 modified and remarked as P/N NB-45-D-2173 (MOD.NB/M/417) in accordance with Britten Norman Modification Leaflet No. BN-2/NB/M/417, Part 2, Issue 1, dated April 8, 1970, or a later ARB- approved issue or an FAA-approved equivalent; or (2) A serviceable flap center operating lever P/N NB-45-D-2173. This amendment becomes effective June 11, 1970.
Affected TCDS · 2
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 52
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1968 | 1 |
|---|---|
| 1969 | 5 |
| 1970 | 5 |
| 1971 | 3 |
| 1972 | 2 |
| 1973 | 5 |
| 1974 | 3 |
| 1975 | 1 |
| 1976 | 7 |
| 1977 | 2 |
| 1978 | 3 |
| 1979 | 3 |
| 1980 | 3 |
| 1983 | 1 |
| 1988 | 1 |
7 with no year recorded