Boeing 737 Systems-Flight Warning System (CDW) 100% Correct Answers
1. Immediate attention warning red
lights are .
2. Red warning lights may indicate -engine, wheel well, and APU fires
. -A/P, A/T disconnects
-landing gear unsafe conditions
(all of the above)
3. Informational alerts such as elec- blue
trical power availability, valve
position, equipment status, and
flight attendant or ground com-
munications are indicated by
lights that are in color.
4. Some lights have a bright blue moving to its selected position/in the se-
and a dim blue setting. The bright lected position
blue indicates a valve and
the dim blue indicates a valve
.
5. Green lights indicate an extended both landing gear and leading edge de-
configuration of . vices
6. The GPWS Inoperative (INOP) -GPWS malfunction
Light illuminates amber for . -a power loss
-invalid inputs
(all of the above)
7. Generally, aural warnings will si- automatically when the associated
lence . non-normal condition no longer exists
8. The Proximity Switch Electronic -takeoff and landing configuration warn-
Unit (PSEU) monitors . ings
-air/ground sensing
- landing gear
(All of the above)
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, Boeing 737 Systems-Flight Warning System (CDW) 100% Correct Answers
9. Two independent Mach/airspeed airspeed is reduced below VMO/MMO
warning systems sound a clack-
er when maximum speed is ex-
ceeded. The clacker will only be
silenced when .
10. The PSEU light is inhibited . in flight
11. The stick shakers are designed to just before a stall develops
alert the pilots .
12. On the fire test panel, we can test -APU, engines, and wheel well fire
for . -engine overheat
-operational fire bottle squibs
(all of the above)
13. will activate the takeoff SPEED BRAKE lever is not in the DOWN
warning system. position
14. The flaps are set at 10 degrees, The horn will not sound
the landing gear is up, and you
are above 800 feet RA. Which of
the following statements is true
about the landing gear horn?
15. A momentary altitude alert tone approaching 900 feet of the altitude se-
will activate . lected on the mode control panel
16. A flashing amber box around the an altitude deviation of 200 feet or more
current altitude signifies .
17. Maximum engine limits are dis- red
played in .
18. A start valve failed to close on en- Blinking start valve open alert for 10 sec-
gine start. Which of the following onds
will alert the crew?
2/6
1. Immediate attention warning red
lights are .
2. Red warning lights may indicate -engine, wheel well, and APU fires
. -A/P, A/T disconnects
-landing gear unsafe conditions
(all of the above)
3. Informational alerts such as elec- blue
trical power availability, valve
position, equipment status, and
flight attendant or ground com-
munications are indicated by
lights that are in color.
4. Some lights have a bright blue moving to its selected position/in the se-
and a dim blue setting. The bright lected position
blue indicates a valve and
the dim blue indicates a valve
.
5. Green lights indicate an extended both landing gear and leading edge de-
configuration of . vices
6. The GPWS Inoperative (INOP) -GPWS malfunction
Light illuminates amber for . -a power loss
-invalid inputs
(all of the above)
7. Generally, aural warnings will si- automatically when the associated
lence . non-normal condition no longer exists
8. The Proximity Switch Electronic -takeoff and landing configuration warn-
Unit (PSEU) monitors . ings
-air/ground sensing
- landing gear
(All of the above)
1/6
, Boeing 737 Systems-Flight Warning System (CDW) 100% Correct Answers
9. Two independent Mach/airspeed airspeed is reduced below VMO/MMO
warning systems sound a clack-
er when maximum speed is ex-
ceeded. The clacker will only be
silenced when .
10. The PSEU light is inhibited . in flight
11. The stick shakers are designed to just before a stall develops
alert the pilots .
12. On the fire test panel, we can test -APU, engines, and wheel well fire
for . -engine overheat
-operational fire bottle squibs
(all of the above)
13. will activate the takeoff SPEED BRAKE lever is not in the DOWN
warning system. position
14. The flaps are set at 10 degrees, The horn will not sound
the landing gear is up, and you
are above 800 feet RA. Which of
the following statements is true
about the landing gear horn?
15. A momentary altitude alert tone approaching 900 feet of the altitude se-
will activate . lected on the mode control panel
16. A flashing amber box around the an altitude deviation of 200 feet or more
current altitude signifies .
17. Maximum engine limits are dis- red
played in .
18. A start valve failed to close on en- Blinking start valve open alert for 10 sec-
gine start. Which of the following onds
will alert the crew?
2/6
