Mar 2017 Page 35
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.
4 INSTALLATION
CAUTION:
CARE MUST BE TAKEN WHEN UNPACKING AND
HANDLING THE DATA ACQUISITION FLIGHT RECORDER
TYPE D51615-202-XXX TO ENSURE THAT THE UNIT
DOES NOT SUFFER UNDUE SHOCK.
4.1 INSTALLATION APPROVAL
The design of each aircraft installation will need to comply with
the requirements of the relevant Certification Authority.
The conditions and tests required for TSO approval of this
article are minimum performance standards. It is the
responsibility of those performing the installation of this article
either on or within a specific type or class of aircraft to
determine that the aircraft installation conditions are within the
TSO standards. The article may be installed only if an
acceptable installation is documented and is approved by the
Administrator.
4.2 SYSTEM DESIGN
A detailed system design is beyond the scope of this manual.
For guidance, a typical system block diagram for a DAFR
system is shown in Figure 8.
Typical wiring diagram for single DAFR installation with a
Control Unit is shown in Figure 7. Aircraft specific drawings will
be provided on request.
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