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Operation
Move the momentary switch on the throttle
control lever knob aft to EXT (extend) and forward
to RET (retract). The speedbrakes extend
when the speedbrake switch is pushed to EXT
and the throttle levers are set for less than approximately
85% N2 engine power.
When a direction is commanded, the actuator
moves to that position and remains there until
commanded (extend or retract) to the opposite
direction. The pilot does not need to hold
the speedbrake switch forward or aft during
the entire cycle; only a momentary push or pull
is required to initiate a sequence.
NOTE
A commanded extension can immediately
be reversed by the pilot and
the speedbrakes will stow. However,
when a retraction is commanded, the
speedbrakes cannot be reversed
(opened) until fully stowed (closed).
15-12 510OM-00
CITATION MUSTANG OPERATING MANUAL
Figure 15-12. Rotary TEST Knob
Figure 15-13. Speedbrakes (Extended)
510OM-00 15-13
The speedbrakes control-and-monitoring circuit
monitors speedbrake positions and commands
retraction when either throttle is set for
greater than approximately 85% N2.
The speedbrake system is DC-powered three
ways:
• The left speedbrake actuator and the
speedbrakes control-and-monitoring circuit
are powered from the left electrical
bus No. 1, through the L SPEED BRAKE
circuit breaker in the FLIGHT CONTROL
section of the left (pilot) CB panel.
• The right speedbrake actuator is powered
from the right electrical bus No. 1,
through the R SPEED BRAKE circuit
breaker in the FLIGHT CONTROL section
of the left (pilot) CB panel.
• The speedbrake position sensors (proximity
switches) are powered from the left
feed bus No. 2, through the SPD BRK
SW circuit breaker in the aft J-box.
In the event of DC power failure, the speedbrakes
remain in their current position.
Emergency/Abnormal
For specific information on emergency/abnormal
procedures, refer to the appropriate
FAA-approved abbreviated checklists or the
Airplane Flight Manual (AFM).
CITATION MUSTANG OPERATING MANUAL
RETRACT
GA GA
RH THROTTLE KNOB
LH THROTTLE KNOB
SPEEDBRAKE
MOMENTARY SWITCH
SPD BRK
R
E
T
E
X
T
FWD
EXTEND
Figure 15-14. Throttle Knob Speedbrake Switch (Left Throttle)
15-14 510OM-00
CITATION MUSTANG OPERATING MANUAL
INTENTIONALLY LEFT BLANK
CHAPTER 16
AVIONICS
CONTENTS
Page
INTRODUCTION................................................................................................................. 16-1
GENERAL ............................................................................................................................ 16-1
G1000 Integrated Flight Deck Overview....................................................................... 16-3
Standby Flight Instruments Overview ........................................................................... 16-3
Air Data Reference Sensors........................................................................................... 16-3
G1000 ARCHITECTURE..................................................................................................... 16-4
Data Communications.................................................................................................... 16-4
Garmin Integrated Avionics Units ................................................................................. 16-4
Displays ......................................................................................................................... 16-7
Other Units..................................................................................................................... 16-7
AVIONICS POWER SWITCHES......................................................................................... 16-9
Battery Switch................................................................................................................ 16-9
Avionics Power Switch................................................................................................ 16-10
Standby Flight Instruments Switch.............................................................................. 16-10
PRIMARY FLIGHT DISPLAY .......................................................................................... 16-10
Description................................................................................................................... 16-10
Graphical Flight Instrumentation................................................................................. 16-12
Inset Map ..................................................................................................................... 16-20
　
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