- Effective
- July 13, 1970
- Models
- BAC 1-11 200 Series, BAC 1-11 400 Series
- Data sheet
- TCDSA5EU
- Product
- Aircraft · Large airplane
- Amendment
- 39-1012
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.
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The airworthiness directive
70-13-01 BRITISH AIRCRAFT CORPORATION: Amdt. 39-1012. Applies to Models BAC 1-11 200 and 400 series airplanes having razor socket supply transformer P/N RD.10590 installed.
To prevent overheating of the razor socket supply transformer when a non-compatible electrical appliance is connected into a razor socket, within the next 1500 hours' time in service after the effective date of this AD, unless already accomplished, accomplish either of the following:
(a) De-activate the razor sockets by disconnecting, insulating, and tying back the socket supply cable from the appropriate circuit breaker and fitting a locking clamp to the circuit breaker knob; or
(b) Modify the razor socket circuit to provide a 1/4 ampere fuse in the positive line of the rectified output of the transformer in accordance with British Aircraft Corporation Model BAC 1-11 Service Bulletin No. 25-PM4458 dated February 9, 1970, or a later ARB-approved issue, or an FAA-approved equivalent.
(British Aircraft Corporation Model BAC 1-11 Service Bulletin No. 25-A-PM4458 refers to this subject.)
This amendment becomes effective July 13, 1970.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.