Mar 2017 Page 65
© 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.
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
(1) Connect the Ground replay Cable SA109680 to the
DAFR main connector.
(2) Connect the Power Input plugs to the 28V power supply
(white wire to positive, black wire to negative).
Note: The recorder draws up to 4A on initial switch-on.
To avoid any possible damage to the unit, please ensure
that any power supply current limiting is disabled before
applying power.
(3) Perform the data download procedure identified in FDR
Data Download above.
(4) Perform the data analysis procedure identified in FDR
Data Analysis above.
6.9 INSPECTION
CAUTION:
IT IS NECESSARY TO REMOVE THE DATA ACQUISITION
FLIGHT RECORDER TYPE D51615-202-XXX FOR 72
MONTHS PERIODIC INSPECTION. POWER MUST BE
SWITCHED OFF AT LEAST FIVE SECONDS BEFORE THE
UNIT IS REMOVED FROM THE AIRCRAFT.
DAFR TYPE D51615-202-XXX CONTAINS
ELECTROSTATIC SENSITIVE DEVICES. EITHER CARRY
OUT COMPANY PROCEDURES OR REFER TO BS IEC
61340-5-1:2007.
Inspection is to be carried out at intervals not exceeding 72
months elapsed time, or as agreed with the relevant
Regulatory Authority.
This procedure must be performed by Penny & Giles
Aerospace Limited.
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