Mar 2017 Page 31
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.
SECTION
REQUIREMENT DAFR CATEGORY
11 Fluids Susceptibility F
(2)
12 Sand and Dust D
13 Fungus Resistance F
14 Salt Fog S
15 Magnetic Effect Z
16 Power Input A
17 Voltage Spike A
18 AF Conducted Susceptibility Z
19 Induced Signal Susceptibility ZC
20 RF Susceptibility WW
21 Emission of RF Energy M
22
Lightning Induced Transient
Susceptibility
A2F3X
23 Lightning Direct Effects X
24 Icing A
25 ESD A
26 Fire X
Table 3 Non-Cockpit Equipment Environmental Test Levels
NOTES:
1 Operating temperature: -55C to +71C.
Maximum short term (<30 minutes) operating
temperature -55C to +71C
Survival Temperature: -55C to +85°C (30 minutes)
Altitude: -15,000ft to 80,000ft
2. Aircraft fluids are listed in Table 4
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