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Silver > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Taxi Weight

A

29,300

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2
Q

Max TO Weight

A

29,000

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3
Q

Max Landing Weight

A

28,500

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4
Q

Max Zero Fuel Weight

A

26,500

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5
Q

Cargo 1

A

1125

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6
Q

Cargo 2

A

850

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7
Q

Cargo 1 and 2 Total

A

1725

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8
Q

Usable Fuel

A

5690

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9
Q

Max Fuel Imbalance

A

200

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10
Q

TO Power + APR or Go Around

TRQ% and ITT Deg C

A

TRQ 107

ITT Deg C 940

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11
Q

Max ITT Temp time at 940 Deg C

Max ITT Temp time at 950 Deg C

A

Time at 940 Deg C is 5 mins

Time at 950 Deg C is 2 mins

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12
Q

TO Power TRQ% and ITT Deg C

A

100

917 (927)

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13
Q

Max ITT time at 917 Deg C is

Max ITT time at 927 Deg C

A

5 mins

2 mins

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14
Q

When can normal TO ITT be exceeded

A

IAW Supplement 24

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15
Q

Max Continuous (OEI) TRQ% and ITT Deg C

A

100

940

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16
Q

Transient except TO TRQ% and ITT Deg C

A

112
965
Max 12 Secs

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17
Q

Max ITT time at 965 Deg C

A

12 sec

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18
Q

Engine Start Max ITT Deg C

A

965

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19
Q

Engine Anti-Icing will be turned on when

A

SAT or OAT +10 Degrees C or colder AND Visible moisture OR Standing water, slush, snow on ramps, taxiways or runways

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20
Q

After leaving Icing conditions, how long must Anti-Ice must be left on

A

At least 5 mins

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21
Q

Wing and Stab Deicing Boots are turned on when

A

SAT or OAT +5 Degs C or colder with visible moisture present OR the uncertainty of ice accumulation OR Any amount of ice observed on any part of the aircraft

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22
Q

Wing and Stab Boots may be used below ______ feet above TO field elevation only at the first sign of ice

A

400 feet

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23
Q

If SAT is below _____ Degs C only use _____ if ice is observed on aircraft

A

-40 Degs C

boots

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24
Q

Deicing boots can be turned off if

A

OAT or SAT of +5 Degs C and no ice on wipers and NO moisture with 3 cycles (9 mins) to be completed after leaving visible moisture. Time may be shortened to complete boot inflation before landing flare or if entering SAT below -40 Degs C

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25
Q

Prop Deicing is turned on when SAT or OAT Degs C is

A

-5 Deg C and below with visible ice accretion

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26
Q

Prop Deicing Norm Selection:

Temps

A

-5 to -12 Degs C

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27
Q

Prop Deice Max Selection:

Temps

A
  • 13 or colder unless vibration occur at warmer temps

* Use caution in MAX mode as runback ice may occur

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28
Q

Flap 7 or 15

A

175 KIAS

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29
Q

Flaps 20

A

165KIAS

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30
Q

Flaps 35

A

140 KIAS

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31
Q

Max Flap Altitude

A

14,000’

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32
Q

Max Landing Gear Retraction VLOR

A

150 KIAS

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33
Q

Max Landing Gear Extention VLOE

A

200 KIAS

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34
Q

Max Landing Gear extended VLE

A

200 KIAS

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35
Q

Max Landing Gear Emergency Extention VLOEE

A

200 KIAS

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36
Q

VMO to 16,000 feet

VMO at 25,000 feet

A

250 KIAS
210 KIAS
*May not be deliberately exceeded in flight

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37
Q

Max VA

A

180 KIAS

*Full deflection and maneuvers near critical angle of attack must be performed below VA

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38
Q

Define VMM (min maneuvering speed)

A

Min speed used for maneuvering portion of approach or departure, weight dependent speed required to maintain 1.3 Vs margin at 30 degs bank

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39
Q

Vmm Flaps 0 degree

A

Vref 20+30

Vref 35+35

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40
Q

Vmm Flaps 7

A

Vref 20+20

Vref 35+25

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41
Q

Vmm Flaps 15

A

Vref 20+15

Vref 35+20

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42
Q

Vmm Flaps 20

A

Vref 20+10

43
Q

Vmm Flaps 35

A

Vref 35+10

44
Q

Prior to reaching Vmm do not exceed___ degrees of bank

A

15 Degrees

45
Q

Max Rough Air Penetration Speed

A

190 KIAS up to 21,000 feet, ISA above this altitude, reduce speed as indicated by the VMO pointer by 30 KTS

46
Q

Flaps Retracted Load Factor

A

+2.75 to -1.0

47
Q

Flap Extended Load Factor

A

+2.0 to +/-0.0

48
Q

Wheel Braking cooling limits, abort/ Normal Braking

A

Contact dispatch and inform them of the abort with no need for MX
15 Mins since RTO

49
Q

Min Airspeed in Icing Climbing above MSA, Cruise, Descent, Holding and Approach (Flaps 0)

A

160 KIAS

50
Q

Airport Pressure Altitude

A

-1000 to 8000 feet

51
Q

Max TO and Landing Tailwind

A

10 KTS

52
Q

Max Operating Altitude

A

25,000 feet

53
Q

Use of Flight Director during TO

A

Is not authorized until gear handle is in the up position

54
Q

Autopilot not Authorized

A
  • Below 500 feet AGL or Acceleration Alt, whichever is lower
  • Below 500 feet on Visual Approach
  • Below 200 feet AGL on precision Approach
  • Below 200 feet on Go Around
  • Below MDA
55
Q

Yaw Damper not Authorized for

A

Takeoff
Go-around
Landing

56
Q

Windshield Wiper Speeds Low and High

A

Low Mode 130 KIAS
High Mode 160 KIAS Max
*Never Operate on Dry Windshields

57
Q

Main Battery Temp

No Battery Start

A

57 Degs C

58
Q

Main Battery Temp

No Cross Gen Start

A

61 Degs C

59
Q

Main Battery Temp

Max for TO

A

64 Degs C

60
Q

Main Battery Temp

Battery Hot Light

A

71 Degs C

61
Q

High Energy Abort

A
  • Make an entry in the logbook
  • Contact Dispatch
  • MX will determine the need for Inspection
62
Q

Climb (no maneuvering)

A

VCLEAN +15

63
Q

Climb (maneuvering) below Minimum Safe Altitude (MSA)

A

VMM+10

64
Q

Climb above MSA, cruise,descent, holding, and Approach (Flaps 0)

A

160 KIAS

65
Q

Corrected VREF

A

VREF+10

66
Q

Final Approach (Maneuvering)

A

VMM+10

67
Q

Missed Approach/Go Around below MSA

A

VREF+20

68
Q

Starter Duty Cycle:(s)

A

Two start attempts with 3 minutes cooling between, then 25 minutes cooling before subsequent starts.

69
Q

Motoring:

A

Three 30-second ventilations with 3 minutes cooling between each, then a one-hour cooling period before subsequent starts or motoring.

70
Q

Time to light-off (from initial Ng rotation to ITT rise),

A

20 seconds maximum (for direct start operations only), and 10 seconds from introducing fuel to light off (for motoring start only).

71
Q

Maximum time with engaged starter is ___ seconds of which max___seconds plain motoring.

A

70 sec

30 sec

72
Q

BAT start is not allowed if the battery temperature is below

A

-20°C

73
Q

Minimum voltage for any battery start is ___ volts.

A

24 volts

74
Q

Minimum time between engine starts when starting subsequent engines is___minute. This applies to all start types. The___minute wait begins when the associated GEN light extinguishes following engine start and the subsequent engine start flow.

A

one min

one min

75
Q

Minimum oil temperature for engine start with type II oil is______. Mixing of Type I and II oils is allowed but not recommended.

A

-40ºC (-40ºF)

76
Q

_____ and _____ switches shall be OFF and CLOSED during takeoff and landing in normal operation.

A

XFEED

CONN VALVE

77
Q

The FUEL TEMP LOW light must be____for takeoff

A

off

78
Q

Fuel Temp, (°C) Operating Limits

A

min-40°C
max+43°C
max pressure altitude 31,000

79
Q

Ice Speed function of Stall Warning System will activate when

A

Either Engine Anti-Ice switch is turned ON.

80
Q

Runway Slope, Landing

A

-2% to +2%

81
Q

Runway Slope, Takeoff

A
  • 2% to +1.5%
82
Q

Maximum Differential Pressure

A

7.5 psi

83
Q

CABIN PRESSURIZATION

Auto Mode Schedule

A

7.1 psi

84
Q

Crosswind Takeoff and Landing

A

35 KTS

85
Q

During initialization on ground the aircraft must not be moved. Takeoff is not permitted if:

A
  1. If attitude difference between the attitude displayed on both EFIS EADls and the standby attitude indicator is three (3) degrees or more (bank and pitch).
  2. If the heading on the compass card is slewing away from the aircraft heading.
86
Q

Reverse taxi operations or power-backs are

A

STRICTLY PROHIBITED

87
Q

Prop Normal operating range RPM is

A

1150-1396 RPM

88
Q

Minimum Emergency Battery Temp for TO

A

-18 Degs C

89
Q

Captain ONLY TO and Landing with less than 100 Hrs as FO

CRAMVX

A 
Contaminated RWY
RWY less than 5000 feet
Airports (Special)
MEL specifies
Vis less than 4000 RVR or 3/4 SM
Xwind exceeding 15kts
90
Q

Captain ONLY TO and Landings

WFBL

A

Winshear reported in vicinity
Flaps in 0 position
Breaking action less than good
Lower than standard TO mins

91
Q

Max tire speed

A

165 kts

92
Q

Icing conditions exist whenever:

The outside air temperature (OAT) or static air temperature (SAT) is ___C or colder and:

A

+10°

  1. There is any type of visible moisture present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet, ice crystals), or
  2. When on the ground, there is standing water, slush, or snow (hard packed snow excluded) on the ramps, taxiways, or runways
93
Q

Minimum oil temp. for ground operations, and after Takeoff for maximum 5 minutes

A

25°C

94
Q

Minimum Emergency Lighting Battery Temperature for takeoff

A

-18°C

95
Q

Derivative Takeoff Power takeoffs are prohibited if any of the following conditions exist: (Reduced Power)

A
  1. The Anti-Skid system is inoperative
  2. CTOT inoperative
  3. Wind shear
  4. Tailwind
  5. Contaminated RWY
  6. De-icing fluid applied
96
Q

In instrument conditions final configuration must be accomplished prior to reaching _________with the exception of circling approaches, single engine operations, or in order to comply with ATC speed restrictions.

A

the final approach fix

97
Q

In visual conditions, final configuration must be accomplished no later than_____.

A

In visual conditions, final configuration must be accomplished no later than 500ft. AGL.

98
Q

For single engine Nonprecision Approaches, final flaps will be delayed until

A

landing is assured

99
Q

For circling approaches, final flaps will be selected when

A

leaving the MDA.

100
Q

TO with Auto Coarsen INOP is

A

Not authorized on contaminated RWY

101
Q

Reverse thrust is prohibited below

A

60kts

102
Q

Standby pitot must be on______mins before TO

A

5 mins

103
Q

Windshield heat must be on_____mins before TO

A

6mins

Silver (4 decks)

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