Mar 2017 Page 101
DATA ACQUISITION FLIGHT RECORDER Type D51615-202-XXX or D51615-
202-XXX-090 with CCU Type D51616-XXXX and CAM Type D51623-XXXX
Installation and Operating Manual with Illustrated Parts
List
Commercial in Confidence
PIM434-I
© Penny & Giles Aerospace Ltd. No part of this work may be reproduced or distributed by any
means without prior permission in writing from the copyright owner.
5 MAINTENANCE
The concept of on-condition maintenance applies to the
Cockpit Control Unit.
6 REPAIR
The Cockpit Control Unit may be repaired at third line.
7 FAULT FINDING
The unit must be returned to Penny & Giles Aerospace
Limited for repairs.
NOTE:
It is advisable that headphones are not plugged into
the Control Unit jack socket during the application of
power or at system reset as this may cause the CVR
POST to fail.
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4=[e’Part 3: Cockpit Area Microphone
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