Extra EA 500 - Flight Instruments

Pilot’s Operating Handbook Section 7
EXTRA 500 Description of Airplane and Systems
LO VOLTAGE
ALTERN ON
LOW PITCH
WINDSHIELD
OVERTEMP
HEAT FAIL
FUEL TRANS
FUEL FILTER
FUEL LOW
GENERATOR
GEAR
BYPASS
LEFT
LEFT
WARN
FLAPS
FAIL
PNEUMATIC
FUEL TRANS
FUEL LOW
STALL WARN
PRESSURE
LOW
RIGHT
RIGHT
CABIN
STANDBY
BLEED
DOOR
AFT STALL
HEAT
WINDSHIELD
PITOT HEAT
DETECTION
STATIC HEAT
FUEL
EXTERNAL
POWER
IGNITION
ACTIVE
PRESS
DEICE
BOOTS
HEAT
INTAKE
HEAT ON
LEFT
LEFT
PRESS
OIL CHIP
PITOT HEAT
STATIC HEAT
LANDING
LIGHT
LIGHT
RECOGN
RIGHT
RIGHT
HYDRAULIC
PUMP
r
r
r
r
r
r
r
r
r
r
r
y
y
y
y
y
y
y
y
y
y
y
y
y
y
y
ggg
gg
gg
r = red, y = yellow, g = green
Figure 7-2
Annunciator Panel
7.5 Flight Instruments
The aircraft is equipped with an integrated ‘glass cockpit’
consisting of two Integrated Flight Displays (IFD) on the main
panel and a keyboard on the center console. These units present
the normal flight information and also feature COM/NAV/GPS
functions and a flight management system. In addition,
conventional back-up flight instruments are placed on the LH
main panel.
26. January 2011 7-9