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Limitations (box items) Flashcards

1
Q

Max depth standing water takeoff/landing

A

.5”/.75”

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2
Q

APU start attempt 3.

A

15 seconds GPU. 30 seconds battery. 2 min off

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3
Q

N2 ground limitations

A

N2 split between engines at idle shouldn’t be greater than 2%
Don’t accelerate above idle if N2 is 57% or less when OAT is -20C or more.

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6
Q

DC power ground limitation

A

To protect Flight compartment CRT displays, max time for ground ops with DC power is 5 min

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7
Q

Max flaps altitude

A

15000

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8
Q

Pressurization

A

Aircraft must be completely de pressurized prior to opening any door. Failure to comply could result in an accident, injury or death.

When low pressure air to ground connection is used, the main cabin door or avionics bay door must be open. AWA uses main cabin door to meet this requirement.

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11
Q

Center fuel tank

A

Takeoff with less than 500 lbs isn’t permitted unless each main wing has above 4400 pounds

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12
Q

Starter temp limits

A

ITT 120C or less for ground start

ITT 90C or less for air starts

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15
Q

Pitch trim

A

Failure to set the pitch trim to the appropriate CG may result in excessive rotation rate at takeoff

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16
Q

Bleed Air system

A

Bleed air 10th stage valve must be closed for takeoff and landing if engine cowl or wing anti ice systems are on.

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17
Q

Turbulence penetration speed

A

280 or .75 Mach

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18
Q

Max depth dry snow takeoff/landing

A

3”/3.75”

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20
Q

Max operating altitude/speed for APU

A

37000/ .85

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23
Q

APU bleed air limitations ground

A

No bleed air extraction limitation
Each engine can be started with APU bleed air
If both engines started, N2 cannot exceed 70%

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24
Q

Flight spoilers

A

Cannot be extended below 1000 AFE.

Cannot be extended below approach speed (VREF+5) or maneuvering speed (VREF+10) plus 17 knots

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25
Q

Stall protection system

A

Must be tested first flight of the day.

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26
Q

Non GPS Approaches with FMS

A

ILS, LOC, LOC BC, LDA, SDF, MLS approaches using FMS is prohibited. Does not provide automatic transition to the ILS.

Cannot continue past FAF if a “NO APPR” message displayed on PFD

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30
Q

Fuel CrossFlow restrictions

A

Powered and gravity cross flow must be off for takeoff

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32
Q

TCAS-RA

A

Only vertical guidance should be used when responding to an RA

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33
Q

Max takeoff and landing altitude

A

10,000 ft

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34
Q

Minimum fuel for go around

A

450 pounds per wing and 10 degrees max nose up

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35
Q

Thrust reversers restrictions

A

To prevent damage due to FOD. Thrust reversers must not be used below 60 knots

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37
Q

Tire speed limits

A

182

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38
Q

MTOW

A

53,000

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39
RCAM value 1
10 Knots
40
Manufacturer max operating altitude
41,000 ft
41
Max APU start altitude/speed
30000 ft and 315 knots
42
Engine indications
Red-maximum and minimum limitations Amber-caution range Green-normal operating range
44
Rotation rate
Excessive rotation rates exceeding 3 degrees per second while aircraft is ne’er ground can reduce stall margins significantly resulting in stickshaker or pusher and potentially loss of control
45
Single engine taxi limitations. SET not authorized:
When damage or injury may result to equipment or personnel on ramp. For first outbound taxi of the day, when airport surfaces contaminated with snow or ice. Left engine shuts down for SET into the gate
48
Flex thrust operation
Flex thrust can’t be used: Normal takeoff fan speed is less than 85% N1 Wing or cowl anti ice bleeds are ON Contaminated runways or windshear warnings
49
Flaps 30 Max operating speed Max extended speed
185 | 185
51
Starter cranking limitations (ground and air)
Start 1- 1 minute on 10 seconds off. Start 2- 1 minute on 10 seconds off Start 3- 1 minute on 5 minutes off. Start 4+- 1 minute on 5 minutes off.
52
Horizontal stabilizer trim
Check must be accomplished first flight of the day.
54
Dry motoring cycle
Start 1- 90 seconds on. 5 minutes off | Start 2-30 seconds on. 5 minutes off
56
APU start attempt 1
15 seconds GPU. 30 seconds battery. 2 min off
60
Engine warmup and cool down
Engines should warm up at idle for 2 minutes before takeoff thrust is set. 5 minutes for first flight of the day. Engines should run at idle for 2 min to cool down. Time starts when aircraft leaves runway to taxi to gate
61
Cold weather operations
Takeoff prohibited with frost ice snow slush to any critical surface. Takeoff permitted with front underside of wing caused by cold soaked fuel. Tactile check of wing needed when: OAT is 5C or less Wing fuel temp is 0C or less Atmospheric conditions are conducive to frost formation
62
Max altitude/speed for using APU bleed air
15000 ft/335 knots
63
Max fuel imbalance.
800 lbs.
67
Max landing gear extension speed
250
68
Cat 2 operation. Max crosswind/max tailwind
15 knots/10 knots
70
Carrying cargo
Flight must be within 45 min of a suitable airport
71
Engine fuel temperature limit
Takeoff with engine fuel below 5* is prohibited
72
Max landing gear retraction
200
73
Cold soaked aircraft operation
If plane is cold soaked in ambient temp of -30 below for more than 8 hours: N1 fan rotation must be verified prior to introducing fuel. Thrust reversers must be actuated until deploy and stow cycles are less than 5 seconds
74
Air Wisconsin max operating altitude
37,000 ft
77
``` Takeoff minimum temp. Takeoff max temp. (-1000 to sea level) Takeoff max temp (sea level to 10000) Enroute max temp ( sea level to 1000) Enroute max temp (above 10k to 41000) ```
``` -40 C +50 C ISA +35 C ISA +35 C ISA +30 C ```
78
MZFW (max zero fuel weight)
44000
79
APU start attempt 2
15 Seconds GPU. 30 seconds Battery. 20 min off
80
Max depth slush takeoff/landing
.5”/.88”
82
APU start attempts 4.
15 seconds GPU. 30 seconds battery. No start attempts for 40 min.
87
APU bleed air limitations-flight
During single engine operations, APU bleed air for engine start not permitted. For double engine failure, bleed air permitted below 13000
89
Ramp weight
53,250
90
Max altitude/speed for engine start using APU bleed air
13000ft/335 knots | 330 knots below 8000ft
91
MLW (max landing weight)
47000
93
RCAM Value 5
27 knots
95
RCAM value 2
10 knots
96
Passenger capacity flotation devices
50 flotation devices as seat cushions. Plus 3 separate child life preservers
97
Flaps 45 Max operating speed Max extended speed
170 | 170
102
RCAM value 4
20 knots
104
Minimum Flight weight
30000
105
Max depth wet snow takeoff/landing
1”/1.50”
106
Minimum takeoff and landing altitude
-1000 ft
112
Max tailwind component for takeoff and landing
10 knots
113
RCAM value 3
15 knots
114
RCAM value 6
27 knots
125
Flaps 8 Max operating speed Max extended speed
200 | 230
126
Flaps 20 Max operating speed Max extended speed
200 | 230
127
How to respond to a TCAS RA
Vertical guidance.
128
Minimum oil pressure for takeoff
45 PSI
129
Max pressurization taxi, takeoff, landing
.1 PSI
130
Max pressurization differences
8. 7 positive | - .5 negative
131
Flight icing definition
TAT 10*C or below and visible moisture. Except when SAT is -40 or below
132
Ground icing conditions definition
OAT is 5*C or less and visible moisture present below 400AGL. or runway is wet or contaminated. Or precipitation.
133
When must wing anti ice be on.
When ice annunciated by ice detector system. When in icing conditions and airspeed less than 230 kts When in icing conditions in a descent. Prior to extending flaps when TAT is 10 or below 2 min prior to takeoff if OAT 5 or below and type 1 only
134
Max engine start altitude
21000

Systems (5 decks)

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