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Q-400 Study > Q-400 Limitations > Flashcards

Q-400 Limitations Flashcards

Aircraft Limitations

1
Q

Kinds of Operation

A
  1. Day and Night VFR
  2. IFR
  3. Icing Conditions
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2
Q

Minimum Flight Crew

A

One Pilot and One Copilot

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3
Q

Maximum Ramp Weight

A

65,400 lbs

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4
Q

Maximum Take-Off Weight

A

65,200 lbs

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5
Q

Maximum Landing Weight

A

62,000 lbs

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6
Q

Maximum Zero Fuel Weight

A

58,000 lbs

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7
Q 
Center of Gravity Limits
Forward Limit (up to 53,000 lbs)
A

13.8% MAC

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8
Q 
Center of Gravity Limits
Forward Limit (53,000 to 65,200 lbs)
A

13.8% to 17.7% MAC

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9
Q

Center of Gravity Limits

Aft Limit

A

36.0% MAC

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10
Q

Maneuvering Limit Load Factors

Flaps Retracted

A

+2.5g to -1.0g

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11
Q

Maneuvering Limit Load Factors

Flaps Extended

A

+2.0g to -0.0g

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12
Q

Maximum Fuel Imbalance

A

600 lbs

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13
Q

Max Operation Speed (Vmo)

Up to 8,000 ft

A

245 KIAS

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14
Q

Max Operation Speed (Vmo)

10,000 ft

A

282 KIAS

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15
Q

Max Operation Speed (Vmo)

18,000 ft

A

286 KIAS

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16
Q

Max Operation Speed (Vmo)

20,000 ft

A

275 KIAS

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17
Q

Max Operation Speed (Vmo)

25,000 ft

A

248 KIAS

18
Q

Flaps Extended Speeds

Flaps 5

A

200 KIAS

19
Q

Flaps Extended Speeds

Flaps 10

A

181 KIAS

20
Q

Flaps Extended Speeds

Flaps 15

A

172 KIAS

21
Q

Flaps Extended Speeds

Flaps 35

A

158 KIAS

22
Q

Maneuvering Speed (Va)

A

204 KIAS

23
Q

Landing Gear Operating Speed (Vlo)

A

200 KIAS

24
Q

Landing Gear Extended Speed (Vle)

A

215 KIAS

25
Q

Rough Air Speed

A

210 KIAS

26
Q

Alternate Gear Extension Speed

A

185 KIAS

27
Q

Maximum Operating Altitude

A

25,000 ft

28
Q

Maximum Oerating Altitude for T/O and Landing

A

10,000 ft

29
Q

Aircraft Approach Category

A

Category C, CAT 1

30
Q

Maximum Runway Slopes

A

+/- 2%

31
Q

Maximum Tailwind Component

Takeoff Flaps 10 or 15, landing Flaps 35

A

20 kts

32
Q

Maximum Tailwind Component

Takeoff Flaps 5, landing Flaps 10 or 15

A

10 kts

33
Q

Minimum Runway Width

A

100 ft

34
Q

Maximum Crosswind Component Dry or Wet

A

32 kts

35
Q

Maximum Crosswind Component Dry Loose Snow

A

18 kts

36
Q

Maximum Crosswind Component Standing Water, Slush, Wet Snow

A

24 kts

37
Q

Ambient Temperature Limits Maximum

A

50 C or ISA +35 C, whichever is lower

38
Q

Ambient Temperature Limit Minimum

A

-54 C

39
Q

Take-off Power Setting Limitations

A

Setting take-off power to brake release, with the nose of the airplane more than 45 degrees out of wind, is prohibited for wind speeds greater than 8 knots.

40
Q

Single Engine Taxi

A

Not Authorized

41
Q

Reverse Taxi

A

Not Authorized

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