AD 81-03-03

Active

Brake Assemblies

Key Information
81-03-03
Active
January 28, 1981
Not specified
Unknown
39-4027
Applicability
["Appliance"]
Not specified
The Boeing Company Lockheed Martin Corporation
727-100 Series 727-100C Series 727-200 Series 727-200F Series 727 Series 727C Series L-1011-385-1 L-1011-385-1-14 L-1011-385-1-15 L-1011-385-3
Regulatory Text

81-03-03 B.F. GOODRICH: Amendment 39-4027. Applies to the following brake assemblies with the following brake lining cups: \n\n\tBrake Assembly P/Ns \n\n\t2-1195-7, 2-1195-8, 2-1367, 2-1367-1, 2-1367-2, 2-1147, 2-1147-3 and 2-1190 \n\n\tBrake Lining Cups with part no./date codes as follows: \n\t\n\n342-58\n342-64\n342-94\n342-95 \nE12 80\nD18 80\nD10 80\nE7 80 \nE19 80\nD28 80 \n\n\nE20 80\nE17 80 \n\n\nG19 80\nG13 80 \n\n\nH9 80\nG19 80\n\n\n\n\tThese brake assemblies are used on but not limited to Boeing 727 and Lockheed L-1011 aircraft. \n\n\tWithin 60 days from the effective date of this AD, the above identified lining cups shall not be used on TSO'd brake assemblies unless the following has been accomplished: \n\n\ta)\tAll spare assemblies (i.e. brakes, pressure plates, lining carriers and torque plates) which have been assembled from inventory containing suspected cups, to be visually inspected at the lining cup button cavity for cracks using 4X or greater magnification. Remove cups with visible cracks and replace with serviceable parts. An alternative to the inspection is replacement of suspected cups with parts which are not in the suspected part no./date code groups. \n\n\tb)\tRecords must be kept to assure traceability of inspections and rework of all assemblies and brake assemblies which were assembled from inventory containing suspected cups. \n\n\tc)\tBrake assemblies installed on aircraft prior to the effective date of this AD do not require removal or inspection. \n\n\tB.F. Goodrich Service Bulletins No. 390 (for the Lockheed L-1011) and No. 391 (for the Boeing 727) dated October 9, 1980 also apply to the subject matter of this AD. \n\n\tThis amendment becomes effective January 28, 1981.

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