RQ-4A Limits Flashcards

1
Q

PROPULSION

  1. Engine Designation?
A

F137-RR-100

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2
Q

PROPULSION

  1. Engine Type?
A

2 spool, axial flow turbofan

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3
Q

PROPULSION

  1. Engine rated?
A

8500 lbs (sea level)

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4
Q

PROPULSION

  1. Bypass Air Thrust at Sea Level?
A

82%

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5
Q

PROPULSION

  1. Bypass Air Thrust at 60K’?
A

83%

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6
Q

PROPULSION

  1. Number of Compressor Stages?
A

14 (1-5 are variable)

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7
Q

PROPULSION

  1. Turbine Section Stages?
A

2 stage - high pressure

3 stage - low pressure

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8
Q

PROPULSION

  1. Accessory Gearbox (ACG) components
A
H - 
O - 
O - 
F - 
S - 
A - 
G -
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9
Q

PROPULSION

  1. Hydraulic pump supplies?
A

B - Brakes
A - AC Generator
N - Nose Gear
G - Gear

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10
Q

PROPULSION

  1. Must stay below ___ for a known oil aux scavenge pump failure.
A

57,000’

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11
Q

PROPULSION

  1. When above ____, ensure the ISS is shut down before descending.
A

60,000’

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12
Q

PROPULSION

  1. Type of combustor and number of fuel nozzles?
A

Annular, 16 nozzles

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13
Q

PROPULSION

  1. Oil Reservoir Capacity?
A

3.25 gal

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14
Q

PROPULSION

  1. Oil Level Indications?
A

1 - 3 gal, 2.8 gal typical at start

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15
Q

PROPULSION

  1. Oil bypass condition hour limit?
A

20 Engine hours

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16
Q

PROPULSION

  1. 8th Stage air provides pressure to?
A

Avionics
ERU
Fuel Tanks

17
Q

PROPULSION

  1. PMA powers the FADECs at what N2?
A

Above 50% N2

18
Q

PROPULSION

  1. Rapid Relight is unable to restart the engine after ___ due to rpm decay.
A

Approx. 8 sec

19
Q

PROPULSION

  1. N2 Ignition starts at?
A

14% N2

20
Q

PROPULSION

  1. N2 Fuel Flow starts at?
A

31.5% N2 or 12 sec after ignition