cl300 limitations Flashcards

(38 cards)

1
Q

max ramp weight

A

39000

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2
Q

max takeoff weight

A

38850

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3
Q

max zero fuel weight

A

27200

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4
Q

max landing weight

A

33750

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5
Q

minimum flight weight

A

23100

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6
Q

Vmo up to 8000 feet

A

300 kias

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7
Q

Vmo 8,001-29,475

A

320 kias

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8
Q

Mmo above 29,475

A

.83M

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9
Q

Rough air penetration speed

A

265 kias / .75M

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10
Q

Max landing gear operating speed extension

A

250 kts

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11
Q

max landing gear operating speed retraction

A

200 kts

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12
Q

max tire speed

A

182 kts

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13
Q

max takeoff and landing PA

A

10,000’

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14
Q

max tailwind component

A

10 kts

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15
Q

load factors flaps up

A

+2.6g to -1.0 G

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16
Q

load factor flaps extended

17
Q

max differential pressure on the ground

18
Q

max differential pressure during landing

19
Q

max positive differential pressure

20
Q

autopilot minimum engage height

21
Q

autopilot minimum height on glide path 3.5 degrees or less

22
Q

autopilot minimum height on glide path between 3.5 and 4.5 degrees

23
Q

visual and non precision autopilot minimum altitude height

24
Q

max altitude for yaw damper off

25
maximum fuel load
14,150
26
fuel per tank maximum
7,075
27
maximum fuel if gravity fed fuel
13,000 (6500 per tank)
28
minimum fuel for go around
500 pounds
29
takeoff with bulk fuel temp above ___C is prohibited
50C
30
with bulk fuel temp at 45C+, min fuel load is
2800 lbs
31
On the ground, APU starts limited to ___ start attempts, followed by a ___ minutes cooling period
3 starts, 1 minute
32
After a third start attempt of the APU on the ground, there must be a ___ minute cooling period. ___ more starts may then be made.
20 minutes. | 2
33
maximum negative pressure differential
-0.5 psi
34
minimum battery temperature
-20C
35
prohibited to extend flaps above what altitude
18000
36
prohibited to extend gear above what altitude
18000
37
flight spoilers must not be used below
500 agl
38
single point pressure refueling is limited to
55 psi and -8 psi defueling