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Q400 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Ramp Weight

A

65,400 lbs

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2
Q

Max Takeoff Weight

A

65,200 lbs

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3
Q

Max Landing Weight

A

62,000 lbs

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4
Q

Max ZFW

A

58,000 lbs

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5
Q

Max Weight Cargo Comp. 1

A

3800 lbs

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6
Q

Max Weight Cargo Comp. 2

A

1000 lbs

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7
Q

Max Weight Fwd Cargo Comp. 3

A

910 lbs

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8
Q

Max Weight Wardrobe

A

160 lbs

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9
Q

Max Weight Cargo Comp 1 + 2

A

3800 lbs

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10
Q

Max Operating Altitude

A

FL250

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11
Q

Max Altitude Takeoff and Landing

A

10,000’

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12
Q

Max Runway slope Takeoff and Landing

A

2% up or down

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13
Q

Max Tailwind for Takeoff or Landing

A

20 kt

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14
Q

Max Cross-Wind Component

A

32 kts

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15
Q

Max Ambient Air Temp Limit (ground and air)

A

50C or ISA +35C Whichever is lower (hits first)

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16
Q

Min Ambient Air Temp Limit (ground and air)

A

-54C

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17
Q

With the engine intake bypass doors open, take-off, landing, and setting MTOP and MCP are limited to a maximum ambient air temp of

A

ISA +25C

18
Q

Approved Takeoff Flap Settings

A

5, 10, 15

19
Q

Max altitude with the landing gear and/or flap extended

A

15,000’

20
Q

Takeoff power setting limitation (wind)

A

Setting TO power prior to brake release, with the nose of the aircraft more than 45 degrees out of wind is prohibited for wind speeds greater than 8kt

21
Q

Max Airstart Altitude

A

20,000’

22
Q

Vmo

A 
0-8000' - 245 kt
10,000' - 282 kt
18,000' - 286 kt
20,000' - 275 kt
25,000' - 248 kt
23
Q

Vfe

A

Flap 5 - 200 kt
Flap 10 - 181 kt
Flap 15 - 172 kt
Flap 35- 158 kt

24
Q

Va (maneuvering)

A

204 kt

25
Q

Vlo - LG Operating

A

200 kt

26
Q

Vle - LG Extended

A

215 kt

27
Q

Rough Air Speed

A

210 kt

28
Q

Alt. Gear Extension Speed

A

185 Kt

29
Q

Max tire ground speed

A

182 kt

30
Q

Starter Cranking Limits

A

70s on 2 min Off
70s on 2 min Off
70s on 30 min Off

31
Q

Max Torque on Ground (%)

A

100%

32
Q

Min NH on Ground (%)

A

64.2%

33
Q

Min SAT for engine relight

A

-40C

34
Q

Max load meter reading for takeoff

A

0.1

35
Q

Minimum battery temp for takeoff

A

-20C

36
Q

Max Usable Fuel

A

11724 lbs

37
Q

Max Fuel Asymmetry

A

600 lbs

38
Q

Normal Cabin Differential

A

5.46 PSI (+/- .1)

39
Q

Max Cabin Differential

A

5.95 PSI

40
Q

Max Cabin Differential for taxi, takeoff, landing

A

0.5 PSI

41
Q

Max Cabin altitude pressurized

A

8000’

42
Q

Wind Limits for Cat II/III ILS (Steady State)

A

Headwind - 25 kts
Crosswind - 15 kts
Tailwind - 10 kts

Q400 (3 decks)

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