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T-1 18-12 > SYS5 Test Review () > Flashcards

SYS5 Test Review () Flashcards

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

A

False

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
Q

Wing anti-ice uses a combination of ___ and ____

A

bleed air and ram air

26
Q

Max speed for wipers

A

200 KIAS

27
Q

Impact of using HIGH windshield heat?

A

Distorts vision

also causes erratic and unreliable mag compass headings

28
Q

what do you do if the horizontal stab. anti ice system fails in flight?

A

use the backup system

29
Q

When can you use anti/de-ice systems on the ground?

A

Testing and LDG roll only

30
Q

The backup de-ice system is operated by placing the switch in the

A

MANUAL position momentarily

31
Q

Placing the H STAB ANTI ICE switch in the test position

A

simulates an overheat condition

32
Q

The PLT STATIC rocker switch on the overhead panel controls power to which heating elements?

A

one static port on each side of the A/C

33
Q

The PITOT HT OFF annunciator will illuminate when

A
  • either heater fails

- either is turned off

34
Q

The wing anti-ice system contains

A

piccolo tubes and an ejector

35
Q

Fresh ambient air is introduced into the wing leading edge by

A

ram air scoops located at the root of each wing and near the wing tip

36
Q

the horizontal stabilizer heating mats maintain temp of ____ when using the anti-ice system

A

between 260* and 280*F

37
Q

For horizontal stab, is the de-ice or the anti-ice primary? secondary?

A

neither is primary, both must be on

38
Q

horizontal stab backup deice used when

A

either of the horizontal stab systems fails

39
Q

the HIGH setting on the windshield heat causes heating where?

A

lower section of the windshield

40
Q

T-1 defog systems routes air where

A

windshield and/or floor

41
Q

oxygen is not available to anyone unless which knob is pulled?

A

SYS READY

42
Q

Passenger oxygen sys is charged when

A

SYS READY and PASS OXYGEN knobs are pulled

43
Q

The green overboard discharge indicator will be missing

A

if the pressure has exceeded 2700 psi

44
Q

The flow of oxygen to passenger masks is activated how?

A

Must pull down on the mask/lanyard

45
Q

Redline pressure on oxygen gauge?

A

2000 psi

T-1 18-12 (23 decks)

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