Additional Limitations Flashcards

1
Q

When must the engine ignition be on?

A
Moderate rain
Moderate turbulence
Vulcanic dust
Contaminated runway
Entering icing conditions
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2
Q

RNP limitaitons

A

En route 1nm
Terminal area .5nm
Approach .3nm

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3
Q

Fuel capacity

A

Center 14200
Wing Tanks 27500
Total 42000

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4
Q

Max fuel imbalance outer tanks

A

1521
815 at take off

-Max fuel imbalance is allowed if the inner and outer tanks on one side are the same as the other side.

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5
Q

Avionics ventilation limitation

A

OAT less than 49 deg C.-No limits

OAT between 49C-55C- 2 hours

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6
Q

Ram Air Inlet max diff pressure

A

Opens only if below 1.0 PSI

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7
Q

Max positive and negative cabin pressure

A

9 psi/-1 psi

safety relief valve set to 8.6 psi

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8
Q

Max Load per gen

Max continuous load per TR

A
  • 90 Kva

- 200 Amps

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9
Q

Oxygen

A

If less than 1339 psi refer to FCOM chart

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10
Q

RAT max speed

A

250 KIAS (for flight test of the RAT)

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11
Q

Structural Icing Conditions

A

Exists when the OAT (on the ground) or TAT (in flight) is at or below 10 C and visible moisture is present in any form.
Engine anti-ice can be off during climb and cruise when SAT is below -40C

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12
Q

Max altitude for battery restart in Emergency Electrical Configuration

A

FL 250

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13
Q

Max APU rpm speed

A

107% will shut down

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14
Q

Max APU EGT

A

Ground…675
Below FL350…1090
Above FL350…1120

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15
Q

Can you use APU air for wing A/ice

A

No

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16
Q

Nose wheel steering angles

A

Hand wheel 75
Towing 95 (85 towbarless)
rudder 6

17
Q

Cannot take-off in the following conditions

A
  • Wet ice
  • Snow over ice
  • Water over compacted snow
18
Q

Max runway altitude

A

9200 feet

19
Q

Vmo/Mmo

Turbulent air penetration

A

350/.82M
-Below FL100 250Kts
Above FL100 275/.76Kts