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Systems > Limitations (box items) > Flashcards

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
Q

RCAM value 1

A

10 Knots

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40
Q

Manufacturer max operating altitude

A

41,000 ft

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41
Q

Max APU start altitude/speed

A

30000 ft and 315 knots

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42
Q

Engine indications

A

Red-maximum and minimum limitations
Amber-caution range
Green-normal operating range

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44
Q

Rotation rate

A

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

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45
Q

Single engine taxi limitations. SET not authorized:

A

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

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48
Q

Flex thrust operation

A

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
Q

Flaps 30
Max operating speed
Max extended speed

A

185

185

51
Q

Starter cranking limitations (ground and air)

A

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
Q

Horizontal stabilizer trim

A

Check must be accomplished first flight of the day.

54
Q

Dry motoring cycle

A

Start 1- 90 seconds on. 5 minutes off

Start 2-30 seconds on. 5 minutes off

56
Q

APU start attempt 1

A

15 seconds GPU. 30 seconds battery. 2 min off

60
Q

Engine warmup and cool down

A

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
Q

Cold weather operations

A

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
Q

Max altitude/speed for using APU bleed air

A

15000 ft/335 knots

63
Q

Max fuel imbalance.

A

800 lbs.

67
Q

Max landing gear extension speed

A

250

68
Q

Cat 2 operation. Max crosswind/max tailwind

A

15 knots/10 knots

70
Q

Carrying cargo

A

Flight must be within 45 min of a suitable airport

71
Q

Engine fuel temperature limit

A

Takeoff with engine fuel below 5* is prohibited

72
Q

Max landing gear retraction

A

200

73
Q

Cold soaked aircraft operation

A

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
Q

Air Wisconsin max operating altitude

A

37,000 ft

77
Q 
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)
A 
-40 C
\+50 C
ISA +35 C
ISA +35 C
ISA +30 C
78
Q

MZFW (max zero fuel weight)

A

44000

79
Q

APU start attempt 2

A

15 Seconds GPU. 30 seconds Battery. 20 min off

80
Q

Max depth slush takeoff/landing

A

.5”/.88”

82
Q

APU start attempts 4.

A

15 seconds GPU. 30 seconds battery. No start attempts for 40 min.

87
Q

APU bleed air limitations-flight

A

During single engine operations, APU bleed air for engine start not permitted.
For double engine failure, bleed air permitted below 13000

89
Q

Ramp weight

A

53,250

90
Q

Max altitude/speed for engine start using APU bleed air

A

13000ft/335 knots

330 knots below 8000ft

91
Q

MLW (max landing weight)

A

47000

93
Q

RCAM Value 5

A

27 knots

95
Q

RCAM value 2

A

10 knots

96
Q

Passenger capacity flotation devices

A

50 flotation devices as seat cushions. Plus 3 separate child life preservers

97
Q

Flaps 45
Max operating speed
Max extended speed

A

170

170

102
Q

RCAM value 4

A

20 knots

104
Q

Minimum Flight weight

A

30000

105
Q

Max depth wet snow takeoff/landing

A

1”/1.50”

106
Q

Minimum takeoff and landing altitude

A

-1000 ft

112
Q

Max tailwind component for takeoff and landing

A

10 knots

113
Q

RCAM value 3

A

15 knots

114
Q

RCAM value 6

A

27 knots

125
Q

Flaps 8
Max operating speed
Max extended speed

A

200

230

126
Q

Flaps 20
Max operating speed
Max extended speed

A

200

230

127
Q

How to respond to a TCAS RA

A

Vertical guidance.

128
Q

Minimum oil pressure for takeoff

A

45 PSI

129
Q

Max pressurization taxi, takeoff, landing

A

.1 PSI

130
Q

Max pressurization differences

A
  1. 7 positive

- .5 negative

131
Q

Flight icing definition

A

TAT 10*C or below and visible moisture. Except when SAT is -40 or below

132
Q

Ground icing conditions definition

A

OAT is 5*C or less and visible moisture present below 400AGL. or runway is wet or contaminated. Or precipitation.

133
Q

When must wing anti ice be on.

A

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
Q

Max engine start altitude

A

21000

Systems (5 decks)

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