AD 68-06-04

Active

Static Inverter Panel

Key Information
68-06-04
Active
March 26, 1968
Not specified
Unknown
39-567
Applicability
["Aircraft"]
["Large Airplane"]
Airbus SAS
BAC 1-11 200 Series BAC 1-11 400 Series
Regulatory Text

68-06-04 BRITISH AIRCRAFT: Amendment 39-567. Applies to Model BAC 1-11 200 and 400 Series airplanes.

Within the next 300 hours' time in service after the effective date of this AD, unless already accomplished, install "P" clips, P/N VGS 6750-2, to the static inverter panel, in accordance with British Aircraft Corporation BAC 1-11 Service Bulletin No. 34-PM 2709, Revision 1, or later ARB-approved issue, or an FAA-approved equivalent.

This amendment becomes effective March 26, 1968.

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