Lmitations Flashcards

1
Q

Maximum Maneuvering Speed Va

A

180 KIAS

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2
Q

Maximum Rough Air Penetration Speed, Vra

A

190 KIAS

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3
Q

Maximum Flaps Extended Speeds, Vfe

Flaps 7 or 15

A

175 KIAS

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4
Q

Maximum Flaps Extended Speeds, Vfe

Flaps 20

A

165 KIAS

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5
Q

Maximum Flaps Extended Speeds, Vfe

Flaps 35

A

140 KIAS

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6
Q

Maximum Landing Gear (Vlor - retraction)

A

150 KIAS

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7
Q

Maximum Landing Gear (Vloe - extension)

A

200 KIAS

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8
Q

Maximum Landing Gear (Vle - extended)

A

200 KIAS

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9
Q

Maximum Landing Gear (Vloee - extended)

A

200 KIAS (150 KIAS without mod 1150)

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10
Q

Maximum Operating Speed Vmo

A

250 KIAS (up to FL160 - then decrese up to 210 KIAS at FL250)

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11
Q

Operating limits - aviation kerosene

A

Min -40 deg C up to +43 deg C

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12
Q

Power Setting:

Take−off Power (max 5 min) - TRQ %

A

TRQ = 108%

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13
Q

Power Setting:

Take−off Power (max 5 min) - ITT °C

A

ITT = 930 °C

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14
Q

Power Setting:

Take−off Power (max 5 min) - ENG rpm %

A

ENG rpm = 100.6 %

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15
Q

Power Setting:

Take−off Power (max 5 min) - PROP rpm

A

RPM = 1396

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16
Q

Power Setting:

Transient except Take−off (max 12 sec) - TRQ %

A

TRQ = 118%

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17
Q

Power Setting:

Transient except Take−off (max 12 sec) - ITT °C

A

ITT = 960 °C

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18
Q

Power Setting:

Transient except Take−off (max 12 sec) - ENG rpm %

A

ENG rpm = 105%

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19
Q

Power Setting:

Transient except Take−off (max 12 sec) - PROP rpm

A

RPM = 1572

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20
Q

Power Setting:

Max Continuous - TRQ %

A

TRQ = 100%

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21
Q

Power Setting:

Max Continuous - ITT °C

A

ITT = 917 °C

22
Q

Power Setting:

Max Continuous - ENG rpm %

A

ENG rpm = 100%

23
Q

Power Setting:

Max Continuous - PROP rpm

A

RPM = 1396

24
Q

Power Setting:

Engine Start - ITT °C

A

ITT = 960 °C

25
Q

Maximum Taxi Weight (MTW)

A

12840 kg

26
Q

Maximum Take−Off Weight (MTOW)

A

12700 kg (MRB: 12930kg)

27
Q

Maximum Landing Weight (MLW)

A

12340 kg

28
Q

Maximum Zero Fuel Weights (MZFW)

A

11660 kg

29
Q

Maneuvering load factor (flaps retracted)

A

+2.75 to -1.0

30
Q

Maneuvering load factor (flaps extended)

A

+2.00 to 0

31
Q

Operational limits:

Airport Pressure Altitude

A

-1000 to +8000 ft

32
Q

Operational limits:

Maximum Take−off and Landing Tailwind Component

A

10 kts

33
Q

Operational limits:

Runway Slope, Landing

A

-2% to +2%

34
Q

Operational limits:

Runway Slope, Take-off

A

-2% to +1.5%

35
Q

Operational limits:

Maximum Operating Altitude

A

25000 ft

36
Q

Operational limits:

Minimum Environmental Temperature for take-off

A

-30 °C

37
Q

Operational limits:

Minimum Main Battery Temperature for take−off

A

-20 °C

38
Q

Operational limits:

Minimum Emergency Lighting Battery Temperature

A

-18 °C

39
Q

Engine Starting Limits - Starter Duty Cycle

A

Two start attempts with 3 minutes cooling between, then 25 minutes cooling before subsequent starts.

Motoring: Three 30−second ventilations with 3 minutes cooling between each, then a one−hour cooling
period before subsequent starts or motoring.

40
Q

Engine Starting Limits - Time to light off (from initial Ng rotation to ITT rise):

A

20 seconds maximum

41
Q

Engine Starting Limits:

Maximum time with engaged starter

A

70 seconds, of which max 30 seconds plain motoring

42
Q

Minimum airspeeds for icing conditions

A

Flaps 0 . . . . . . . . . . . . . 160 KIAS
Flaps 7 . . . . . . . . . . . . . 150 KIAS
Flaps 15 . . . . . . . . . . . . 145 KIAS
Flaps 20 . . . . . . . . . . . . 140 KIAS
Flaps 35 . . . . . . . . . . . . 130 KIAS

43
Q

Cabin Pressurization:

Maximum Differential Pressure

A

7.5 psi

44
Q

Cabin Pressurization:

Auto Mode Schedule

A

7.1 psi

45
Q

Autopilot:

Minimum Use Heights (MUH) during take-off or go-around:

A

200 ft AGL

46
Q

Autopilot:

Minimum Use Heights (MUH) during cruise

A

500 ft AGL

47
Q

Autopilot:

Minimum Use Heights (MUH) during coupled approach:

A

50 ft AGL

48
Q

Autopilot:

Minimum Use Heights (MUH) during non−coupled approach:

A

100 ft AGL

49
Q

Yaw Damper Operation is not authorised for:

A
  • Take-off
  • Go around
  • Landing.
50
Q

Flaps may only be extended on ground and during take off, low altitude holding, approach and landing,
up to a maximum altitude of

A

14000 ft