Aircraft System Limitations Flashcards

(32 cards)

1
Q

Maximum liters of oxygen

A

25 L

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2
Q

Number of oxygen regulators

A

10

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3
Q

Static oxygen pressure range

A

270-455 PSI

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4
Q

Continous breathing range oxygen pressure range

A

270-340 PSI

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5
Q

LOX QTY Low Advisory

A

5 L

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6
Q

LOX QTY Low Caution

A

2,5 L

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7
Q

Auxiliary hydraulic system PSI

A

2.760-3.200 PSI
Approx. 3.000 PSI

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8
Q

Auxiliary hydraulic system operates the following

A

Ramp and door
Emergency brakes
Nose gear emergency extension

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9
Q

Auxiliary hydraulic system hydraulic fluid quantity

A

5,2 gal.

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10
Q

Utility hydraulic system PSI

A

2.900-3200 PSI
Approx. 3.000 PSI

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11
Q

Utility hydraulic system, which EDP (engine driven pump)

A

1 and 2

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12
Q

Utility hydraulic system operates the following

A

Flaps
Brakes
Gear
Nose-wheel steering
Portion of flight controls

(Fat boys get no punani)

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13
Q

Utility hydraulic system hydraulic fluid quantity

A

4,3 gal.

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14
Q

Booster hydraulic system PSI

A

2.900-3200 PSI
Approx. 3.000 PSI

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15
Q

Booster hydraulic system, which EDP (engine driven pump)

A

3 and 4

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16
Q

Booster hydraulic system operates the following

A

Half of flight controls

17
Q

Booster hydraulic system hydraulic fluid quantity

18
Q

Fuel tank 1 and 4 quantity

19
Q

Fuel tank 2 and 3 quantity

20
Q

Auxiliary fuel tanks quantity

21
Q

Fuel transfer pump pressure

22
Q

Fuel boost pump pressure

23
Q

Fuel tank limit (same side)

A

500-1.000 lbs

24
Q

Fuel tanks symmetrical limit

25
Fuel tanks wings limit
1.500 lbs
26
Primary fuel management
Nothing in the auxiliary tanks OR 7.060 lbs OB and 6.400 IB
27
APU start light extinguishes
50%
28
APU starter duty cycle
1 minute on, 4 minutes off
29
APU maximum continuous EGT
680
30
APU over temp ACAWS
710 EGT longer than 3 seconds
31
APU normal RPM range
98%-105%
32
APU door opens in flight/on ground
15 / 35 degrees