User's Manual Part 6

Page D-4

3 Mar 2017

23-15-29

SYSTEM DESCRIPTION AND INSTALLATION MANUAL

JetWave™ System

NOTE:

• All zenith view (from above) angles, except for “e,” are measured from the aircraft

longitudinal axis, being 0 degrees at the stern.

• All side view angles are measured from the aircraft lon

gitudinal axis, being 0 degrees at

the plane where the antenna emitter is located.

Refer to ARINC Characteristic 791 Mark I Aviation Ku-band and Ka-Band Satellite Communication System,

Part 1-

Physical Installation and Aircraft Interfaces for Aircraft blockage map parameters.

Table D-6. Weight on Wheels

Weight on Wheels Discrete Input Available Y/N

Polarity of Weight on Wheels Discrete

Signal

Table D-7. Ground Transmit Enable

Ground Transmit Enable Discrete Y/N

Polarity of Ground Transmit Enable

Discrete

Table D-8. ARINC Tx Mute and Tail Sector Mute Switch

ARINC Tx Mute Connected Yes/No

Tail Sector Mute Switch Wired Yes/No

Table D-9 ARINC791 Equipped

Y N Frame Number for Fittings 3 and 4 Frame Number

Draft as of 31 May 2017