5
The remote cable is normally left connected to the 6600 at the “Remote” connector on the top
panel and is wrapped around four cord posts on the lid of the 6600 case. The cord retainers
on top of these posts swivel in either direction and latch at 180 degree positions, allowing easy
wrapping and unwrapping of the remote cable. A cord clamp allows the cable to be held in
place after it is wrapped. It is easier to wrap the remote cable around the posts after
disconnecting the cable from the Remote unit.
If the remote cable needs to be disconnected and removed from the 6600 completely for
storage elsewhere then opening the Interface Connectors cover allows the cable to be
dislodged from the cable guide.
[5]
Primary Static ports (Ps1) :
The Primary Static output is provided on two ports that are internally connected. Both ports
have #4 AN fittings. At least one of these ports must be connected through a hose to the Static
port (Ps1 and PN1 on smart-probe) on the aircraft. The hose must be connected
after
performing the Self Test on the 6600. The hose, once connected, must not be disconnected
while the aircraft Static system is not at “Ground” level. An unused port must remain closed.
Caution:
Do not connect this output to the aircraft before performing the Self Test.
Caution:
Do not disconnect this output from the aircraft unless the aircraft’s Pitot Static
system is at “Ground” level and the tester is OFF.
[6]
Secondary Static ports (Ps2) :
The Secondary Static output is provided on two ports that are internally connected. Both
ports have #4 AN fittings. These ports are typically used when the aircraft has “smart-
probes” requiring a differential static input. These ports may also be used either as a
secondary static output or a secondary airspeed output. When using the tester with aircraft
with “smart-probes”, at least one of these ports must be connected through a hose to the PN2
port of the smart-probe on the aircraft. The hose must be connected
after
performing the Self
Test on the 6600. The hose, once connected, must not be disconnected while the aircraft Static
system is not at “Ground” level. An unused port must remain closed.
WARNING: If the Ps2 output is not being used then it must be capped-off (closed).
Caution:
Do not connect this output to the aircraft before performing the Self Test.
Caution:
Do not disconnect this output from the aircraft unless the aircraft’s Pitot Static
system is at “Ground” level and the tester is OFF.
Summary of Contents for 6600
Page 10: ...3 Figure 2 1 A...
Page 11: ...4 Figure 2 1 b...
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