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NetJets CE-680 systems Ch 1-17 (Supervisión of Fire Alarm System)Questions And Answers.
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NetJets CE-680 systems Ch 1-17 (Supervisión of Fire Alarm System)Questions And Answers.
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10/14/24, 12:35 PMNetJets CE-680 systems Ch 1-17
Jeremiah
Terms in this set (149)
1. C
Which statement regarding the hydraulic
system is true?
A. Loss of both hydraulic pumps illuminates
the HYDRAULIC PRESSURE LOW
amber CAS message.
B. The main hydraulic system powers the
ailerons/spoilers, landing gear and brakes,
nosewheel steering, and flaps.
C. The hydraulic systems main components
include: a reservoir and fluid, 2 engine-
driven pumps, an auxiliary pump, and
pressure/volume indicators.
D. Loss of both hydraulic pumps illuminates
the HYDRAULIC LOW FLOW amber CAS
message.
2. The CE-680 hydraulic system provides C
power
to:
A.
Flaps
B.
Horizontal stabilizer
C. Roll Spoilers/Speed brakes
D. Ailerons
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3. What subsystems are powered by the B
CE-080 hydraulic system?
A. Speedbrakes, roll spoilers, ailerons,
brakes, and flaps
B. Landing gear, brakes, speedbrakes, roll
spoilers, and nosewheel steering
C. Wheel brakes, landing gear, nosewheel
steering, and trim
D. Flaps, secondary horizontal stabilizer
trim, landing gear, wheel brakes, and
steering
4. While airborne, what signals the loss of D
both hydraulic pumps:
A. HYDRAULIC VOLUME LOW L-EICAS
cyan message
B. HYDRAULIC PRESSURE LOW L-R cyan
CAS message
C. HYDRAULIC FLOW LOW L-R amber CAS
message
D. HYDRAULIC PRESSURE LOW L-R amber
CAS message
5. C
In an emergency, standby hydraulic
pressure
may be obtained by:
A. Selecting the AUX HYDRAULIC pump
ON
B. By selecting crossflow to tap into the
APU hydraulic pump
C. There is no standby hydraulic pressure
available in flight
D. By deploying the wind driven hydraulic
pump if you are below FL250
6. The main hydraulic system preflight D
requires:
A. No external check
B. Aircraft batteries connected and battery
buttons on to check the reservoir recharge
pressure
C. AUX hydraulic pump on to determine the
reservoirs volume
D. Reference to a temperature/pressure
placard on the ground service panel to
determine the correct reservoir precharge
pressure
2/26
, 10/14/24, 12:35 PM
1. Which of the following is true regarding D
the anti-skid system?
A. The ANTISKID FAIL| CAS message
illuminates during self-test while the
landing gear is retracting.
B. Power brakes fail if anti-skid protection is
lost. Pneumatic braking must be used.
C. The ANTISKID FAIL CAS message
illuminates then extinguish during the
warning systems test.
D. The ANTISKID FAIL CAS message
illuminates if an anti-skid fault is detected
or the switch is turned OFF.
2. The proper method of checking brake C
wear during preflight is to set the parking
brake and assure that:
A. The brake wear indicators are flush and
show freedom of movement
B. A 0.20 mm feeler gauge fits snug
between the indicator pad and the face of
the carbon disc brake
C. The brake wear indicator pin is not
recessed into the caliper housing
D. The REPLACE BRAKES CAS message
is displayed on the EICAS
3. If the ANTISKID FAIL CAS message A
illuminates prior to landing and the
message cannot be extinguished:
A. Power braking is still available, but anti-
skid protection is lost. Landing distance
must be extended
B. Power brakes are still available but anti-
skid protection is lost. No change to the
landing distance.
C. Power braking and thrust-reversers are
lost. Pneumatic braking must be used
D. Power brakes are still available unless
the BRAKE PRESS LOW CAS message has
also illuminated
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