User's Manual

Airbus Iridium SATCOM System
165E5733-00 L-3 Aviation Recorders Proprietary
Issue, Rev. 02
21 January 2014
Page 24
Figure 3-5 – SCM Oblique View (Note 1: Resistance between mounting plate and module not to exceed
20 milli-ohms. Also, resistance between mounting plate and aircraft structure not to exceed 20 milli-ohms.)
Figure 3-6 – SCM Connector View Showing Location of Pin 1 (Note 2: Connector is a 9-pin D-Sub,
P/N ABS1145A09P03B.)