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

18
Q

Approved Takeoff Flap Settings

19
Q

Max altitude with the landing gear and/or flap extended

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

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)

25
Vlo - LG Operating
200 kt
26
Vle - LG Extended
215 kt
27
Rough Air Speed
210 kt
28
Alt. Gear Extension Speed
185 Kt
29
Max tire ground speed
182 kt
30
Starter Cranking Limits
70s on 2 min Off 70s on 2 min Off 70s on 30 min Off
31
Max Torque on Ground (%)
100%
32
Min NH on Ground (%)
64.2%
33
Min SAT for engine relight
-40C
34
Max load meter reading for takeoff
0.1
35
Minimum battery temp for takeoff
-20C
36
Max Usable Fuel
11724 lbs
37
Max Fuel Asymmetry
600 lbs
38
Normal Cabin Differential
5.46 PSI (+/- .1)
39
Max Cabin Differential
5.95 PSI
40
Max Cabin Differential for taxi, takeoff, landing
0.5 PSI
41
Max Cabin altitude pressurized
8000'
42
Wind Limits for Cat II/III ILS (Steady State)
Headwind - 25 kts Crosswind - 15 kts Tailwind - 10 kts