C90B Flashcards

1
Q

Fuel flow (L) - IFR

A

250 l

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2
Q

Fuel flow (L) - IFR

A

70 L a mais (total)

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3
Q

Ops PEC Long range

A

230 FL
230 kt
230 L

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4
Q

VXSE (ângulo)

A

100 kt

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5
Q

VYSE (razão)

A

108 kt

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6
Q

VMCA

A

80 kt

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7
Q

One engine inoperative enroute climb (blue line)

A

108 kt

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8
Q

VX

A

101 kt

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9
Q

VY

A

112

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10
Q

Emergency descent

A

182

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11
Q

VSSE

A

97 kt

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12
Q

Balked landing climb

A

101

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13
Q

Flaps down final approach

A

101 kt

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14
Q

Flaps down final approach Single

A

101 kt

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15
Q

VYSE

A

108 kt

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16
Q

Max demonstrated crosswind

A

25 kt

17
Q

MTOW

A

10,100 lb

18
Q

MLW

A

9,600 lb

19
Q

V Rotate

A

97 kt

20
Q

Maneuvering speed

A

169

21
Q

COMPRESSOR: N1 MAX

A

101,5% (38,100RPM)

22
Q

Propeller Max RPM

A

2200 RPM

23
Q

Max RPM Reverso

A

1100 RPM

24
Q

Limitações de overspeed e causas

A

2420 RPM (5 s)

  • ACIMA DE 2200RPM INDICA FALHA NO GOVERNADOR PRIMARIO
  • ACIMA DE 2288RPM INDICA FALHA EM AMBOS GOVERNADORES
25
Q

Velocidade max para abaixamento de trem de pouso

A

182 kt

26
Q

Velocidade de penetração de turbulência

A

161 kt

27
Q

A partir de qual altitude pode-se ligar o piloto automático

A

500 pés ou MDA ou DA

28
Q

Após falha da transfer pump todo o combustível do tanque será transferido para o tanque principal, exceto:

A

28 us gal

29
Q

Após ser teclado uma queda de pressão na linha de bomba de transferência, a luz no transfer se acende em:

A

30 seg

30
Q

Antes da decolagem, previsto como warning com relação às bombas de combustível devem:

A

Ambas operar normalmente

31
Q

Após a falha da transfer pump e o nível do tanque principal ter caído a aproximadamente …, o combustível do tanque da asa começará a ser transferido para o tanque principal?

A

3/8

32
Q

Regra de nível de voo king air

A

Até 30 min - 130

Até 40 min - 140

33
Q

Nível de voo maximo VFR

A

F145