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
Maximum Taxi Weight (MTW)
12840 kg
26
Maximum Take−Off Weight (MTOW)
12700 kg (MRB: 12930kg)
27
Maximum Landing Weight (MLW)
12340 kg
28
Maximum Zero Fuel Weights (MZFW)
11660 kg
29
Maneuvering load factor (flaps retracted)
+2.75 to -1.0
30
Maneuvering load factor (flaps extended)
+2.00 to 0
31
Operational limits: | Airport Pressure Altitude
-1000 to +8000 ft
32
Operational limits: | Maximum Take−off and Landing Tailwind Component
10 kts
33
Operational limits: | Runway Slope, Landing
-2% to +2%
34
Operational limits: | Runway Slope, Take-off
-2% to +1.5%
35
Operational limits: | Maximum Operating Altitude
25000 ft
36
Operational limits: | Minimum Environmental Temperature for take-off
-30 °C
37
Operational limits: | Minimum Main Battery Temperature for take−off
-20 °C
38
Operational limits: | Minimum Emergency Lighting Battery Temperature
-18 °C
39
Engine Starting Limits - Starter Duty Cycle
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
Engine Starting Limits - Time to light off (from initial Ng rotation to ITT rise):
20 seconds maximum
41
Engine Starting Limits: | Maximum time with engaged starter
70 seconds, of which max 30 seconds plain motoring
42
Minimum airspeeds for icing conditions
Flaps 0 . . . . . . . . . . . . . 160 KIAS Flaps 7 . . . . . . . . . . . . . 150 KIAS Flaps 15 . . . . . . . . . . . . 145 KIAS Flaps 20 . . . . . . . . . . . . 140 KIAS Flaps 35 . . . . . . . . . . . . 130 KIAS
43
Cabin Pressurization: | Maximum Differential Pressure
7.5 psi
44
Cabin Pressurization: | Auto Mode Schedule
7.1 psi
45
Autopilot: | Minimum Use Heights (MUH) during take-off or go-around:
200 ft AGL
46
Autopilot: | Minimum Use Heights (MUH) during cruise
500 ft AGL
47
Autopilot: | Minimum Use Heights (MUH) during coupled approach:
50 ft AGL
48
Autopilot: | Minimum Use Heights (MUH) during non−coupled approach:
100 ft AGL
49
Yaw Damper Operation is not authorised for:
- Take-off - Go around - Landing.
50
Flaps may only be extended on ground and during take off, low altitude holding, approach and landing, up to a maximum altitude of
14000 ft