Specifications

SECTION II
AIRPLANE AND SYSTEMS
MODEL 560
TEST SYSTEM
The test selector is located in the upper left corner of the pilot’s switch panel and offers several
positions of test. It will function only when the BATT switch is ON. A red light above the test selector
switch illuminates whenever the test selector switch is in any position but OFF.
Figure 2-30. Test Selector Switch
OFF The red light will be off and the test system inoperative.
FIRE WARN The engine fire lights on the upper center instrument panel will illuminate.
LDG GEAR The three green safe lights and the red unlocked light on the landing gear control
panel will illuminate and the warning horn will sound. Horn may be silenced by
pressing horn silence button on landing gear control panel if flap position is less than
15 degrees.
BATT TEMP The red BATT O'TEMP >160 annunciator will flash, the battery temperature gage will
indicate 160°F and the MASTER WARNING lights will flash (cancelable).
STICK SHAKER The stick shaker will operate on the left hand control column. The angle-of-attack
meter needle will swing past the red band and the indexer will flash.
T/REV The ARM, UNLOCK and DEPLOY thrust reverser lights (six) will illuminate and the
MASTER WARNING lights will flash (cancelable).
W/S TEMP The W/S AIR O'HEAT light will illuminate if LOW or HIGH is selected on the
windshield bleed air switch.
OVERSPEED Avionics switch must be on for the check of overspeed warning horn and related EFIS
display information. The following indications will occur:
The audible overspeed warning will sound and the PFD IAS will indicate approximate
V
MO
for the existing pressure altitude (red)
PFD Mach will read .400 (red)
Altitude will read 5000 feet
PFD 1 & 2 vertical speed will read 2000 feet-per-minute.
ANTISKID Initiates a self-test in the antiskid system. ANTISKID INOP will illuminate and remain
illuminated five to seven seconds after the rotary TEST switch is selected to the
ANTISKID position. ANTISKID INOP will then extinguish if the system checks
operational. If the system does not check operational, the light will remain illuminated.
AVN The avionics switch must be selected for this check. MASTER CAUTION and AP
OFF and YD OFF annunciators will illuminate and the altitude alert tone will sound.
ANNU The avionics switch must be selected for this check. All the annunciator panel lights
and the master warning light will illuminate. Both red turbine overspeed lights will
illuminate and the engine instrument digital display will flash 8's. AP OFF annunciators
will illuminate and the altitude alert tone will sound
I 2-68 Configuration AA 56OMB-01