Day 10 - Hydraulic/Pneumatic Systems Flashcards

1
Q

The T-1 hydraulic system controls

A

Flaps, landing gear, speed brakes, and normal braking

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2
Q

What types of hydraulic pumps are utilized in the T-1

A

Variable displacement, rotary plunger type pumps

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3
Q

The hydraulic pumps delivery and pressure varies from __ gpm at __ psi to __ gpm at __ psi

A

0, 1500, 3.9, 1400

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4
Q

Hydraulic reservoir capacity is

A

1.2 gallons

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5
Q

The hydraulic reservoir is pressurized by what and at what psi

A

Engine bleed air, 15 psi

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6
Q

Why is the hydraulic reservoir pressurized

A

To prevent frothing

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7
Q

The hydraulic system normally stabilizes at __ psi

A

1500

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8
Q

The hydraulic pressure relief valve begins to open at __ psi

A

1650

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9
Q

The hydraulic pressure relief valve is fully open at __ psi

A

1850

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10
Q

Hydraulic pressures above 1850 can only be relieved by doing what

A

By activating the hydraulic pressure relief switch on the flightdeck

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11
Q

The HYD PUMP PRESS LO annunciator illuminates when pressure falls below

A

750 psi

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12
Q

The HYD LEVEL LO annunciator illuminates when

A

The fluid level in the reservoir falls below 0.6 gallons

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13
Q

When landing without normal hydraulic pressure, increase __ flap landing distance by __

A

30, 90%

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14
Q

The systems that require bleed air are

A

Engine anti-ice, wing anti-ice, hydraulic reservoir pressurization, entrance door seal inflation, cabin pressurization, and environmental system (ACU)

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15
Q

When does CABIN PRESSURE LO annunciator illuminate

A

Cabin altitude 9500 +/- 500 feet

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16
Q

When does CABIN PRESSURE HI annunciator illuminate

A

11 +/- 1 psi

17
Q

When does ENG ICE TEMP LO annunciator illuminate

A

Below 120 F

18
Q

When does AIR COND FAIL annunciator illuminate

A

400 F or 53 psi

19
Q

When does BL AIR DCT FAIL annunciator illuminate

A

350 F or 3.5 +/- 0.5 psi

20
Q

When does DEFOG AIR OV HT annunciator illuminate

A

200 F

21
Q

When does CABIN AIR OV HT annunciator illuminate

A

390 +- 15F