Mar 2017 Page 95
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.
FDR RCRD switch, TEST and ERASE Push-buttons and
Headset Jack.
The CCU Type D51616-2XXX is provided with a toggle switch
to select between the DAFRs.
Separate FDR FAIL, CVR FAIL indicators.
Panel dimensions: 28.2mm (H) x 145.8mm (W) x 63.0mm (D)
(excluding connector)
Connector DCM37P or equivalent.
1.3.3 Environmental Characteristics
The CCU and CAM satisfies the requirements of RTCA DO-
160D, with test categories as shown in Table 12.
SECTION
REQUIREMENT CCU & CAM
4 Temperature/Altitude A2
5 Temperature Variation C
6 Humidity A
7 Operational Shock & Crash Safety B
8 Vibration
U (zone 2,
curves F & F1)
S (zone 2,
curves M & C)
9 Explosionproofness X
10 Waterproofness X
11 Fluids Susceptibility X
12 Sand and Dust X
13 Fungus Resistance F
14 Salt Spray X
15 Magnetic Effect A
16 Power Input X
(1)
17 Voltage Spike X
(1)
18 AF Conducted Susceptibility X
(1)
19 Induced Signal Susceptibility Z
(2)
20 RF Susceptibility UUU
(3)
21 Emission of RF Energy M
22
Lightning Induced Transient
Susceptibility
XXF1
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