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STRIKE FINDER
Operation
Upon system start-up or reboot, a five minute warm-up is needed to
achieve full stabilization (note that
the first minute after power-up). If the aircraft heading is changed during
the five minute warm-up period, the strike dots may drift somewhat from
correct positioning. Use the clear function before take-off, pausing to
acquire strike information and storm locations if the warm-up period is not
complete.
In-flight operation is fully automatic.
RBS Module Technical Specifications
SIZE:
Internal Module 2000-050:
3.00 (7.62 cm) high
3.00 (7.62 cm) wide
1.40 (3.56 cm) deep
Note: This module mounts inside
the SF2000 Display, and
therefore does not affect its
outside dimensions.
EXTERNAL MODULE 2000-051:
3.19 (8.10 cm) high
3.19 (8.10 cm) wide
1.60 (4.06 cm) deep
Note: This positions the SF2000
Display connector
0.80 (2.03cm.) further to the rear.
MOUNTING:
Internal Module:
Integral with SF2000 Display main
board. (SF 2000 Mod "D" or later).
EXTERNAL MODULE:
Interfaces directly with the SF2000
Display connector and the
Sensor cable connector.
PILOT'S
GUIDE
DIGITAL WEATHER AVOIDANCE
RBS
action is completely locked out for
WEIGHT:
0.3 lbs. (0.13 kg.)
TEMPERATURE:
-20 to +55C (-4 to +131F)
ALTITUDE:
-1,000 to 55,000 feet (maximum)
COOLING:
Conduction
BEARING STABILITY:
Within +/-10˚, for 90˚ of heading
change.
TSO COMPLIANCE:
TSO-C110a
RTCA COMPLIANCE:
Environmental:
DO-160B Category
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SOFTWARE:
DO-178B Level 2
POWER REQUIREMENTS:
Power:
0.5 Watts
59
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