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. The radio altitude is less than 500 feet AGL and both throttles are below 25° throttle angle and the flap posiion is not at 30°.
NOTE
The “GEAR”aural can not be muted during any of these conditions.
The “Too low gear”(EGPWS) aural warning is heard if any landing gear is not down and locked with the radio altitude less than 500 feet AGL and the indicated airspeed at less than 190 knots.
If neither radio altimeter is valid, the “GEAR”aural will sound if any gear is not down and locked and the airplane is below 16,500 feet. The landing gear horn may be muted by pressing the mute hornn swith/ light on the landing gear control panel. With both thrust levers at IDLE, (less than three degrees throttle lever angle) the horn cannot be muted.
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2
EICAS DISPLAY
Engine Indicating
Indications of EPR, N1, ITT, N2, FF,
OIL TEMP and OIL PRESSURE. For more
information see Chapter 18, POWER PLANT.
Fuel
Indications of total fuel quantity and individual tank quantity. For more information see Chapter 12, FUEL.
Crew Alerting System Window
14 message lines with Gear/Slats/Flaps pop up displayed.
Slats/Flaps, Spoilers and Gear Position Pop Up
The pop up display will be removed from the primary page (in flight only) 30 seconds after the gear and flaps indicate up, ans no predetermined malfunctions exist, or flight spoilers out.
The pop up display will appear with flap selection greater than zero degrees, gear selected down and/or if any predetermined malfunctions exist.
Trims
Indications for Aileron, Rudder and Stabilizer Trim. For more information see Chapter 10, FLIGHT CONTROLS.
Crew Alerting System Window
24 message lines with Gear/Slats/Flaps pop up not displayed.
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
SYSTEMS DISPLAY (STAT PAGE)
CKPT/CABIN Temperature
Indications of cockpit, cabin forward and cabin aft temperature. For more information see Chapter 2, AIR CONDITIONING AND PRESSURIZATION.
OXYGEN
Indications of oxygen quantity. For more information see Chapter 8, EMERGENCY EQUIPMENT.
OUTFLOW VALVES
Indications of outflow valves position (manual mode only). For more information see Chapter 2,
AIR CONDITIONING
AND PRESSURIZATION.
BRAKE TEMP
Indications of brake temperatures. For more information see Chapter 15, LANDING GEAR.
CAB ALT,
P and CAB RATE
Indications of cabin altitude, cabin differential and cabin rate of climb. For more information see Chapter 2, AIR CONDITIONING AND PRESSURIZATION.
OIL QTY
Indications of engine, APU and reservoir oil quantity. For more information see Chapter 5, APU, and Chapter 18, POWER PLANT.
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