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SkyWest 2024 CQ > Limitations > Flashcards

Limitations Flashcards

(66 cards)

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1
Q

Max Ramp Weight

A

85,450 lb (LL)
85,870 lb (LR)

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2
Q

Max Takeoff Weight

A

85,098 lb (LL)
85,517 lb (LR)

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3
Q

Max Landing Weight

A

74,957 lb (LL/LR)

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4
Q

Max Zero Fuel Weight

A

69,467 lb (LL)
69,886 lb (LR)

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5
Q

Minimum Runway Width

A

100 ft

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6
Q

Minimum Taxiway Width

A

50 ft

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7
Q

Aircraft Wing Span

A

93’ 11”

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8
Q

Aircraft Length

A

103’ 11”

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9
Q

Aircraft Tail Height

A

32’ 4”

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10
Q

Max Operation Altitude

A

41,000 ft

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11
Q

Max Takeoff & Landing Altitude

A

10,000 ft

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12
Q

Max Temperature T/O & Landing

A

ISA +35C (52C)

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13
Q

Min Temperature T/O & Landing

A

-40C

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14
Q

Runway Slope

A

+/- 2%

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15
Q

Max Tailwind

A

15 kt

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16
Q

Max Single Pack Operations

A

31,000 ft

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17
Q

Vmo (Sea Level - 8,000’)

A

Velocity Maximum Operating Speed
300 kt

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18
Q

Vmo (10,000’ - Mach Transition)

A

Velocity Maximum Operating Speed
320 kt

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19
Q

Mmo

A

Mach Maximum Operating Speed
0.82

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20
Q

Va

A

Maneuvering Speed
240 kt

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21
Q

Vlo (ext)

A

Landing Gear Extension Speed
250 kt

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22
Q

Vle (ret)

A

Landing Gear Retraction Speed
250 kt

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23
Q

Vle

A

Max Speed Operable with L/G Extended
250 kt

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24
Q

Vtire

A

195 kt

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25
V(rat deploy max)
Vmo/Mmo
26
Vmin (to provide electrical power)
130 kt
27
Vb (below 10,000 ft)
250 kt
28
Vb (10,000 ft and above)
270/0.76M, whichever is lower
29
V(wiper ops max)
250 kt
30
V(window)
160 kt
31
Vfe 1
230 kt
32
Vfe 2
215 kt
33
Vfe 3
200 kt
34
Vfe 4/5
180 kt
35
Vfe FULL
165 kt
36
Maximum Crosswind Components
RCC 6 : 38 kt RCC 5 : 31 kt RCC 4 : 20 kt RCC 3 : 15 kt RCC 2 : 12 kt RCC 1 : 8 kt RCC 0 : PROHIBITED
37
Max Altitude Flaps Extended
20,000 ft
38
CAT II Approach Mandatory Flaps Setting
Flaps 5
39
Flaps Full - Go Around Flaps
Flaps 4
40
Flaps 5 - Go Around Flaps
Flaps 2
41
Minimum Battery Voltage
22.5 V
42
Maximum Engine Start ITT Temp Limit
815 C
43
Starter Cranking Limits (Ground)
Starts 1 & 2 90 seconds ON - 10 seconds OFF Starts 3 - 5 90 seconds ON - 5 minutes OFF
44
Starter Cranking Limits (In Flight)
Starts 1 & 2 120 seconds ON - 10 seconds OFF Starts 3 - 5 120 seconds ON - 5 minutes OFF
45
Dry Motoring Cycle Limits
#1 90 seconds ON - 5 minutes OFF #2-5 30 seconds ON - 5 minutes OFF
46
Max Fuel Capacity
20,935 lb
47
Max Fuel Imbalance
794 lb
48
Min Fuel Tank Temperature
-37C
49
Max Time Allowable Unattended with APU Running (SKW)
5 minutes
50
APU Starter Duty Cycle
Start Attempt 1 & 2 60 seconds OFF Third Attempt 5 minutes OFF
51
APU Start/Continuous Min Temp
-54C
52
APU Start/Continuous Max Temp
ISA +35C (52C)
53
APU Max Start Altitude
30,000 ft
54
APU Max Continuous Operation Altitude
33,000 ft
55
APU Max Altitude for Continuous Electrical Generator Use
33,000 ft
56
APU Max Altitude for Engine Start
21,000 ft
57
APU Max Altitude for Bleed Use
15,000 ft
58
Max Differential Pressure
8.4 PSI
59
Max Differential Overpressure
8.8 PSI
60
Max Differential Negative Pressure
-0.5 PSI
61
Max Differential Pressure for T/O and Landing
0.2 PSI
62
Min Hydraulic Reservoir Temp for Engine Start
-18C
63
ENG A/I OAT Temp from 5C - 10C Requirements
- When there is any possibility of encountering visible moisture up to 1,700 ft AFE - When operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engines, nacelles, or engine sensor probes.
64
ALL A/I OAT Temp Less than 5C Requirements
- When there is any possibility of encountering visible moisture up to 1,700 ft AFE - When operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engines, nacelles, or engine sensor probes.
65
Min AP Engagement Height
400 ft
66
Min AP Use Height on Approach
50 ft HAT

SkyWest 2024 CQ (3 decks)

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