SYS5 Test Review () Flashcards

(45 cards)

1
Q

For the ACU to function, BLEED AIR switch must be in which position?

A

NORM
L ENG/R ENG
HIGH

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2
Q

For most training flights, the MODE switch will be in the ____ position

A

AUTO FLDK

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3
Q

A passenger in the rear of the A/C complains it’s too hot, how can you increase the amount of cool air to the aft cabin?

A

Press the CABIN OUTLET button

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4
Q

Pressurization is provided by _______

A

bleed air through the air cycle unit

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5
Q

Cabin pressure is maintained by regulating the amount of _____

A

air leaving the cabin

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6
Q

The cabin rate-of-climb knob is usually set in which position?

A

10 o’clock

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7
Q

The CABIN PRESSURE LO annunciator illuminates when the cabin altitude reaches

A

9,500 ft (+/-500ft)

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8
Q

When operating properly, the outflow valves will keep cabin pressure differential from exceeding ___ psi

A

9.1

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9
Q

Prolonged operation with the bleed air in EMER can result in __

A

Melted trim panels in the rear portion of the cabin

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10
Q

The VCCS provides

A

the primary cooling prior to engine start and the auxiliary cooling in the air

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11
Q

ELECT HEAT 1&2 activates

A

3 heaters

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12
Q

When does Ground air provide fresh air to the cabin?

A

on the ground only

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13
Q

What action should the crew take in the event of AV BLO FAIL?

A

press the AV STBY BLO switch

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14
Q

The T-1A is pressurized by

A

engine bleed air

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15
Q

The temperature in the cabin during normal inflight operations is controlled by

A

mixing hot bleed air and cooled bleed air

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16
Q

When planning to cruise at FL330 the cabin controller should be set to ___

A

34,000 ft

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17
Q

The use of the EMER position on the bleed air knob is

A

an emergency and should not be prolonged any longer than necessary

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18
Q

The avionics standby blower

A

provides an additional source of cooling for the avionics rack in the back of the cabin

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19
Q

Which of the following systems is capable of cooling the aircraft cabin prior to engine start?

A

VCCS

Vapor Cycle Cooling Subsystem

20
Q

Selection ELEC HEAT 1&2 on the aux control switch

A

activated 3 heaters

21
Q

The ice detect probe triggers an annunciator

A

if it accumulates 0.02 inches of ice

22
Q

For engine anti-ice, where is the bleed air inlet valve with or without power?

A

OPEN WITHOUT power

CLOSED WITH power

23
Q

T/F: While airborne, do not operate engine anti-ice at a static air temp above 10*C

24
Q

The red WING OV HT annunciator illuminates when

A

any one of the over-temp switches senses a temp in excess of either 212* or 350*F

25
Wing anti-ice uses a combination of ___ and ____
bleed air and ram air
26
Max speed for wipers
200 KIAS
27
Impact of using HIGH windshield heat?
Distorts vision also causes erratic and unreliable mag compass headings
28
what do you do if the horizontal stab. anti ice system fails in flight?
use the backup system
29
When can you use anti/de-ice systems on the ground?
Testing and LDG roll only
30
The backup de-ice system is operated by placing the switch in the
MANUAL position momentarily
31
Placing the H STAB ANTI ICE switch in the test position
simulates an overheat condition
32
The PLT STATIC rocker switch on the overhead panel controls power to which heating elements?
one static port on each side of the A/C
33
The PITOT HT OFF annunciator will illuminate when
- either heater fails | - either is turned off
34
The wing anti-ice system contains
piccolo tubes and an ejector
35
Fresh ambient air is introduced into the wing leading edge by
ram air scoops located at the root of each wing and near the wing tip
36
the horizontal stabilizer heating mats maintain temp of ____ when using the anti-ice system
between 260* and 280*F
37
For horizontal stab, is the de-ice or the anti-ice primary? secondary?
neither is primary, both must be on
38
horizontal stab backup deice used when
either of the horizontal stab systems fails
39
the HIGH setting on the windshield heat causes heating where?
lower section of the windshield
40
T-1 defog systems routes air where
windshield and/or floor
41
oxygen is not available to anyone unless which knob is pulled?
SYS READY
42
Passenger oxygen sys is charged when
SYS READY and PASS OXYGEN knobs are pulled
43
The green overboard discharge indicator will be missing
if the pressure has exceeded 2700 psi
44
The flow of oxygen to passenger masks is activated how?
Must pull down on the mask/lanyard
45
Redline pressure on oxygen gauge?
2000 psi