AD 79-19-08

Active

Pressure Relief Door

Key Information
79-19-08
Active
September 24, 1979
Not specified
Unknown
39-3561
Applicability
["Aircraft"]
["Large Airplane"]
Lockheed Martin Corporation
L-1011-385-1 L-1011-385-1-14 L-1011-385-1-15
Regulatory Text

79-19-08 LOCKHEED-CALIFORNIA COMPANY: Amendment 39-3561. Applies to all L-1011-385-1, L-1011-385-1-14, and L-1011-385-1-15 airplanes certificated in all categories, configured with a C-1A cargo door.

Compliance required as indicated.

To assure the retention of "fail-safe" operational capability of the pressure relief door, accomplish the following:

(a) Within the next 300 hours time in service, unless already accomplished, install the antifriction gasket on the flange of the pressure relief door in accordance with the FAA approved Lockheed-California Company Service Bulletin 093-52-133 dated May 30, 1979.

(b) Special flight permits may be issued, in accordance with FAR 21.197 and 21.199, to operate airplanes to a base for the accomplishment of modification required by this AD.

(c) Alternate modifications or other actions which provide an equivalent level of safety may be used when approved by the Chief, Aircraft Engineering Division, FAA Western Region.

Thisamendment becomes effective September 24, 1979.

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