Mar 2017 Page 12
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.
Table 2 DAFR Connector pin allocation
PIN SIGNAL
CABLE
REQUIREMENTS
NOTES
1 Potentiometer #1 +3.3V Configurable
5
2 Reserved
3 Potentiometer #1 Return Configurable
5
4 Chassis GND
1
22 AWG
5 Chassis GND
1
22 AWG
6 Pre-Amp Power Out Hot 24 AWG Configurable
5
7 Pre-Amp Power Out GND 24 AWG Configurable
5
8 0V Signal
1
22 AWG
9 Accelerometer In Lo 22 AWG Configurable
5
10 Rotor Speed In Hi
24 AWG S.T.P.
Configurable
5
11 Rotor Speed In Lo Configurable
5
12 28 VDC Power In 22 AWG
13 FDR Fault Out 24 AWG Configurable
5
14 CVR Fault Out 24 AWG Configurable
5
15 Voice Erase A 24 AWG Configurable
5
16 Voice Erase C 24 AWG Configurable
5
17 Audio Out Hi
24 AWG S.T.P.
Configurable
5
18 Audio Out Lo Configurable
5
19 Push-to-Test 24 AWG Configurable
5
20 MTI Tx+
3
24 AWG F.T.P.
21 MTI Tx-
3
22 MTI Rx+
3
24 AWG F.T.P.
23 MTI Rx-
3
24 Stop CVR Recording 24 AWG
25 ARINC 429 #1 In A Configurable
5
26 ARINC 429 #2 In A Configurable
5
27 Channel 1 Audio In Hi
24 AWG S.T.P.
WITH 36
Configurable
5
28 Channel 2 Audio In Hi
24 AWG S.T.P.
WITH 37
Configurable
5
29 Channel 3 Audio In Hi
24 AWG S.T.P.
WITH 38
Configurable
5
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