BOEING 767-300 ICE & RAIN, WARNING

Will the GPWS alert you to a normal descent in the landing configuration towards areas without obstacle or terrain DATA? (FCOM, 15.10.14). A.- YES. B.- NO.

Which of the following warnings are indicated by a siren? (FCOM, 15.20.5). A.- Ground proximity warnings. B.- Wheel well fire warnings. C.- Cabin altitude warnings.

Which of the following occurs when a master caution light is pushed? (FCOM, 15.20.4). A.- Only the master caution light extinguish. B.- Only the EICAS caution message disappears. C.- Both the master caution light extinguish and the EICAS caution message disappears.

Which of the following does the GPWS "pull up" aural indicate? (FCOM, 15.20.16). A.- Altitude loss just after takeoff. B.- Deviation below the glide slope. C.- Excessive terrain closure rate.

Which of the following causes the standby engine indicator to operate if the SEI selector is in auto? (FCOM, 15.20.19). A.- An EICAS failure. B.- Exceeding an engine red line limit. C.- Pushing the engine display switch.

Which of the following causes the standby engine indicator (SEI) to operate? (FCOM, 15.20.9). A.- An engine exceedance. B.- Failure of one EICAS CRT. C.- Rotating the SEI selector to on.

Which of the following can appear on the EICAS status display? (FCOM, 15.10.5). A.- Fuel temperature and quantity indications. B.- Hydraulic fluid temperature and quantity indications. C.- Flight control positions and status messages.

Which aurals are associated with caution? (FCOM, 15.20.5). A.- Voice and siren. B.- Voice and beeper. C.- Beeper and chime.

When is status information displayed? (FCOM; 15.10.6). A.- Anytime a new status message occurs. B.- Anytime both engines are shut down. C.- Only when the status display switch is pushed.

When does the takeoff inhibiting of the master warning/caution lights end?(FCOM, 15.20.6). A.- After climbing above 1,500 feet radio altitude. B.- Twenty seconds after rotation or 400 feet AGL. C.- When the flaps are fully retracted.

When can status information be displayed, if one EICAS CRT has failed? (FCOM, 15.20.9). A.- Only in flight. B.- Only on the ground. C.- Anytime.

What is indicated by the EICAS status cue? (FCOM, 15.10.1). A.- New status message exists. B.- Status display switch was pushed. C.- Status display switch is inoperative.

What is displayed if the upper EICAS CRT fails? (FCOM, 15.20.9). A.- Engine indications appear on the lower EICAS CRT. B.- Engine indications appear on the standby engine indicator. C.- A display inoperative message appears on the upper EICAS CRT.

What indications are inhibited during a takeoff, beginning at rotation? (FCOM, 15.20.6). A.- Fire bell and master warning lights,. B.- Beeper and master caution lights. C.- Master warning/caution lights and display messages.

What happens to the crew alerting messages when the cancel switch is pushed? (FCOM, 15.10.7). A.- All warning, caution and advisory messages disappear. B.- Only caution and advisory messages disappear. C.- Only the most recent message disappears.

What happens if the left EICAS computer fails? (FCOM, 15.20.9). A.- Left engine indications are blanked. B.- The right computer controls both CRTs. C.- The upper CRT is blanked.

What happens if an EICAS status page is displayed and you push the engine diplay switch? (FCOM, 15.10.2). A.- Engine related status messages appear. B.- Secondary engine indications replace the status page. C.- Secondary engine indications compact on the upper CRT.

What does the GPWS "sink rate" aural indicate? (FCOM, 15.20.17). A.- An excessive descent rate. B.- An altitude loss during a go-around. C.- An altitude loss just after take off.

What action is required to display the second page of EICAS alert messages? (FCOM, 15.10.7). A.- Push the next page switch. B.- Push the recall switch. C.- Push the cancel switch.

What action is required to display the second EICAS status page? (FCOM, 15.10.6). A.- Push the next page switch. B.- Push the status display switch. C.- Push the cancel switch.

How do you display additional pages of status messages? (FCOM, 15.10.6). A.- Push the cancel switch. B.- Push the next page switch. C.- Push the status display switch.

How do you cancel the EICAS test? (FCOM, 15.10.7). A.- Push the indicator light test switch. B.- Push the engine display switch. C.- Push the EICAS test switch in the accesory panel.

How can you silence the GPWS "glide slope" aural? (FCOM, 15.20.17). A.- Push the glide slope inhibit switch. B.- Push the master warnin/caution reset switch. C.- Push the cancel switch.

How can you remove the status cue from the EICAS CRT? (FCOM, 15.10.6). A.- Push the status display switch. B.- Push the cancel switch. C.- Push the engine display switch.

Wing anti-ice can be operated in flight only. It is inhibited on the ground. (FCOM, 3.20.1). A.- NO. B.- YES.

Which windows are anti-fogged by continuous flow of conditioned air? (FCOM, 3.20.3). A.- Captain\'s and first officer\'s windshields. B.- Left and right side windows. C.- All cockpit windows.

When the engine anti-ice switches are off and both VALVE lights out, what is the position of the engine anti-ice valves? (FCOM, 3.10.1). A.- Closed. B.- Open. C.- In transit.

When does probe heat operate? (FCOM, 3.20.3). A.- When the switch is on and both engines are running. B.- Automatically when any engine is running. C.- Only when airborne.

What protects the wings from icing? (FCOM, 3.20.1). A.- Electric heating elements in the three outboard LE slats. B.- Engine bleed air heating the inboard LF slats. C.- Engine bleed air heating three outboard LE slats.

What is true about Probe Heat? (FCOM, 3.20.3). A.- Operation of the probe heat system is fully automatic. B.- Power to the electrically heated probes is applied any time an engine is running. C.- Both.

The engine anti-ice switches are ON with both VALVE lights illuminated, what is the position of the engine anti-ice valves? (FCOM, 3.10.1). A.- .All valves are on. B.- All valves are open. C.- All valves are closed.

Overheat detection systems are installed for both engines, struts, and pneumatic ducts in the wing and body areas. (FCOM, 8.20.1). A.- True. B.- False.

On the ground or in flight, pushing the ENGINE ANTI-ICE switches ON commands the engine anti-ice valves: (FCOM, 3.20.1). A.- To open. B.- To open, and allows engine bleed air to anti-ice the engine cowl inlets. C.- To close, and allows engine bleed air to anti-ice the engine cowl inlets.

One INOP light illuminates and the EICAS advisory message L or R FWD WINDOW or L or R SIDE WINDOW displays to indicate: a window is not being heated. (FCOM, 3.20.3). A.- A window is not being heated. B.- The system in not turned ON. C.- The valve not agrees with commanded position.

If the left engine anti ice switch is blank and its VALVE light (amber) is illuminated, what is the condition of the left engine anti ice valve? (FCOM, 3.10.1). A.- Signaled open, and not open. B.- Signaled closed, and not closed. C.- Signaled open, and is in transit.

If both engine anti-ice switches are ON and both valve lights extinguished, what is the position of the engine anti-ice valves? (FCOM, 3.10.1). A.- Closed. B.- Open. C.- In transit.

ICE AND RAIN GRAPHIC: 7 Which windows have a fault or overheat condition? (FCOM, 3.10.2). A.- L & R FWD. B.- R FWD. C.- L FWD.

ICE AND RAIN GRAPHIC: 6 Which windows are being heated? (FCOM, 3.10.2). A.- Side windows. B.- Forward windows. C.- The left forward and side windows.

ICE AND RAIN GRAPHIC: 5 ¿What is the position of the right wing anti-ice valve? (FCOM, 3.10.1). A.- Signaled open and not open. B.- Singnaled closed and not closed. C.- Signaled closed but in transit.

ICE AND RAIN GRAPHIC: 4 What is the position of the wing anti ice valves with these indications? (FCOM, 3.10.1). A.- Open. B.- Closed. C.- Valve position can not be determined.

ICE AND RAIN GRAPHIC: 4 What is the position of the engine anti ice valves? (FCOM, 3.10.1). A.- Closed. B.- Open. C.- Intransit.

ICE AND RAIN GRAPHIC 4: Is this panel configuration normal to flight without icing conditions?. A.- Yes. B.- No.

ICE AND RAIN GRAPHIC 1: Total Air Temperature (TAT) Probe Light Illuminated (amber) – when probe is not being heated in flight or neither engine is running on the ground. (FCOM, 3.10.49. A.- YES. B.- NO.

How are the wing anti-Ice valves controlled? (FCOM, 3.10.1). A.- By Hydraulics power. B.- By switches in the manual Anti-Ice Panel (Overhead). C.- By Pneumatics power.