AD 78-08-01

Active

Engine Blow-Off Valve Switches

Key Information
78-08-01
Active
May 10, 1978
Not specified
Unknown
39-3180
Applicability
["Aircraft"]
["Large Airplane"]
Textron Aviation Inc.
BH.125 Series 600A HS.125 Series 600A
Regulatory Text

78-08-01 HAWKER SIDDELEY AVIATION LIMITED: Amendment 39-3180. Applies to BH/HS 125-600A airplanes, certificated in all categories.

Compliance required within one month after the effective date of this AD, unless already accomplished.

To prevent possible inability to activate the engine blow-off valve switches in the event that birds are ingested into the engines on take-off, accomplish the following:

Remove the existing switch guards for the engine blow-off valve switches and replace with the new design guard, P/N 25-6 NF 2629, in accordance with the section entitled "Accomplishment Instructions" and the associated drawing, contained in Hawker Siddeley Aviation, Ltd. Service Bulletin 75-3(2580), dated June 21, 1977, or an FAA-approved equivalent.

This amendment becomes effective May 10, 1978.

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