COMPONENT MAINTENANCE MANUAL
AVIATION RECORDERS
Model FA5000
Initial Issue Page 6
Sep. 30/11
Introduction
23−70–40
Use or disclosure of information on this sheet is subject to
the restrictions on the cover page of this document.
6. DOCUMENT VERIFICATION
All CMM drawings, illustrations, wiring diagrams, and block diagrams were validated
against existing engineering source material. All Testing & Fault Isolation, Disassembly
and Assembly procedures have been verified against the actual performance of the unit
under test conditions as indicated in Table 1 below.
Table 1 identifies the sections of the CMM that underwent a Shop Verification process
and the date of the verification. In addition, a Component Maintenance Manual Verifica-
tion Report that identifies the technician who performed the procedure and Engineer/
Technical Writer who verified the procedure along with a Quality Assurance Engineer ap-
proval signature is kept on file with the CMM sign−off release form. For a copy of the
Component Maintenance Manual Verification Report for this version of the CMM, please
address inquiries to the following:
L-3 Communications
Aviation Recorders Publications
100 Cattlemen Rd.
Sarasota, Florida 34230
Phone: (941) 371–0811
FAX: (941) 377–5591
Table 1. Shop Verification
Procedure Chapter Date of Verification
Testing & Fault Isolation 100 Feb. 11/14
Disassembly 300 Feb. 12/14
Assembly 700 Feb. 12/14
Note: Contact L-3 Communications, Aviation Recorders, to verify this date sensi-
tive information when using this manual to develop other documentation.
The L−3AR Publication index may be located at www.L−3.com or L−3ar.net.
7. COMPONENT MAINTENANCE MANUAL (CMM) EFFECTIVITY
Effectivity of the CMM is based on effectivity dates and product serial number. Effectivity
of the manual is identified by a list of effective pages in the front of the manual.
The document reference is online, please check the correspondence between the online documentation and the printed version.
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