Specifications

SECTION I
DESCRIPTION AND SPECIFICATIONS
MODEL 560
ANGLE-OF-ATTACK / STICK SHAKER SYSTEM
The angle-of-attack and stall warning system must be operable and a satisfactory preflight must be
performed in accordance with Section IV, Operating Information.
The angle-of-attack indicating system may be used as a reference system but does not replace the
airspeed display in the PFD as a primary instrument.
The angle-of-attack system can be used as a reference for approach speed (1.3 V
SI
) at all airplane
weights and center-of-gravity locations at zero, takeoff, takeoff/approach and landing flap positions.
1.3 V
SI
is indicated by approximately 0.6 on the Angle-Of-Attack Gage and by the top of the white tape
on the pilot's and copilot's airspeed indicators.
If the stick shaker does not operate during the warning system test, or the angle-of-attack system is
otherwise inoperative, it must be repaired before flight, except when the airplane is operated with an
Approved Minimum Equipment List.
ENGINE FAN INSPECTION
To ensure accurate fan speed thrust indication, inspect the fan for damage prior to each flight.
NOTE
Refer to the exterior inspection in the Normal Procedures Section of this manual for
engine duct and fan inspection.
GND IDLE SWITCH
The GND IDLE switch must be in the HIGH position when conducting touch and go landings and when
operating on the ground with engine anti-ice bleed ON.
AUDIO CONTROL PANEL
Operation of the audio panel in the passenger speaker (PASS SPKR) mode is limited to required
passenger briefings or emergencies.
NOTE
f The same side cockpit speaker is normally muted when PASS SPKR is selected.
All incoming transmissions and auxiliary audio warnings (GPWS and TCAS, if
installed) will be received through the opposite side speaker. If both audio control
switches are selected to PASS SPKR, both cockpit speakers become muted.
Avoid selecting both switches to PASS SPKR at the same time.
f With passenger speaker mode selected and microphone selector switch selected to
oxygen mask, the same side cockpit speaker will not receive voice interphone
communications from the oxygen mask microphone of the opposite side pilot.
f Headset audio is not affected when (PASS SPKR) mode is selected.
I 1-22 Configuration AA 56OMB-01