AD 69-14-03

Active

Windshield Heating Circuit

Key Information
69-14-03
Active
August 10, 1969
Not specified
Unknown
39-794
Applicability
["Aircraft"]
["Large Airplane"]
Airbus SAS
BAC 1-11 200 Series BAC 1-11 400 Series
Regulatory Text

69-14-03 BRITISH AIRCRAFT CORPORATION: Amdt. 39-794. Applies to Model BAC 1-11 200 and 400 Series Airplanes.

Compliance required within the next 1,500 hours' time in service after the effective date of this AD, unless already accomplished.

To prevent the failure of the windshield heating circuit, install 20K ohm resistors and 1 mfd capacitors into both phases of the heating circuit for pilot's and copilot's main windshield in accordance with British Aircraft Corporation Modification Bulletin No. 30-PM 3092, Revision 8, dated July 22, 1968 or later ARB-approved revision or an FAA approved equivalent.

This amendment becomes effective August 10, 1969.

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References
This information is not available.
--- - Part 39
FAA Documents