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Citation Latitude > Limitations - All Other > Flashcards

Limitations - All Other Flashcards

1
Q

Battery Limits

APU Starts Per Hour

A

9

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2
Q

Lav pocket doors must be latched open for:

A

Taxi, takeoff, and landing

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3
Q

When do we turn L and R WING ON?

A

+5 to -35° C in visible moisture.

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4
Q

Fuel

Total fuel quantity

A

11,390 lbs.

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5
Q

Do not taxi until attitude and heading alignment is complete. How long for AHRS?

A

90 seconds

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6
Q

Oil Limitations
Oil Pressure
Ground / Flight Idle

A

20 - 110 psi

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7
Q

EICAS Temperature Limitations:
If ambient temperature is at or above ISA + 26 degrees C, and avionics are operated continuously:

A

Provide conditioned air to the cockpit and close the cabin door.

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8
Q

Reverse Thrust Time Limit

A

5 minutes

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10
Q

Baggage Compartment
Weight Limits

A

Weight limits are placarded above each compartment.

1,000 lbs
150 lbs/ft2

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12
Q

Engine Limitations
Max ITT
Starting

A

950° C

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13
Q

Following any APU shutdown, do not attempt restart until ___ seconds after APU is at ___% RPM.

A

30 seconds

0%

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14
Q

Oil Limitations
Oil Temperature
TO, MCT, CRU, Reverse,
Ground / Flight Idle

A

16 - 135° C

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15
Q

Engine Limitations
N1 / N2 %
TO, MCT, CRU, Reverse

A

105%

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16
Q

Do not operate ___ ___ ___ while manually operating cockpit and cabin temp controls.

A

MAX COOL ON

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17
Q

The APU compartment must be inspected after an:

A

Automatic Shutdown

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18
Q

Fuel
Pressure refueling limits
PSI

A

10 - 55 psi

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19
Q

If bleed air anti-ice is selected ON for more than 30 seconds, operate both engines at or above ___ % N2.

A

65%

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20
Q

Passenger oxygen masks are not approved for sustained operation at a cabin altitude greater than _____ ft.

A

25,000’

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21
Q

EICAS Temperature Restrictions
If ambient temperatures is at or above ISA + 31 degrees C:

A

Limit ground operations of avionics to 30 minutes (45 minutes between flights) without conditioned air.

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22
Q

Do not depart if any Garmin Display Unit (GDU) is in ____ _____.

A

Reversion Mode

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23
Q

Oil Limitations
Oil Pressure
TO, MCT, CRU, Reverse

A

36 - 110 psi

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24
Q

Engine Limitations
N2
Ground Idle Minimum

A

57%

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25
Q

Fuel
Max Defueling pressure
PSI

A

-10 psi

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26
Q

Max continuous static ground operation at TO is limited to:

A

2 minutes

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27
Q

Max Tire Groundspeed

A

182 kts

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30
Q

Reverse thrust must be ____ during static operations.

A

IDLE

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32
Q

Min Airspeed

Speedbrake Extended

A

Vref + 15

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33
Q

Max Airspeed

Below 8,000’

A

270 kts

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34
Q

Minimum Dry Runway Length for release

A

4000’

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35
Q

When do we turn ENGINE/STAB ON?

A

+10 to -35° C in visible moisture.
RAT in flight
SAT on ground

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36
Q

Minimum Battery Temp

APU Start

A

-20° C

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37
Q

Can you use the autopilot when either AHRS has failed?

A

NO

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38
Q

Ops Review required for Wet / Contaminated runway less than _____.

A

5000’

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39
Q

Can you use the autopilot when any comparison monitor is activated?

A

NO

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40
Q

Flight in _____ _____ is prohibited.

A

Freezing Rain

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41
Q

Engine Starts

Pilot Initiates aborts for:

A 
1. No oil pressure w/i 20 sec. of
     ITT rise
2. No N1 by 40% N2
3. No stable idle w/i 90 sec of ITT
     rise
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42
Q

45 minute IFR Reserve fuel:

A

1464 lbs

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43
Q

Operate ENG/STAB ANTI-ICE at least ___ - ___ minutes prior to entering icing conditions.

A

3 - 5

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44
Q

Maximum GPU load

A

1500 amps

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45
Q

Can you back the aircraft with reverse thrust?

A

NO

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46
Q

Max Flap / Landing Gear

Extended Altitude

A

18,000’

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48
Q

Except for ground preflight check, max SAT for operation of bleed air anti-ice with thrust lever above IDLE is _____.

A

+20° C

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49
Q

Min Airspeed
S/E Enroute Climb

A

180 kts

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50
Q

Do not use reverse thrust when conducting:

A

Touch and Go landings

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51
Q

Max number of passengers:

A

8 plus 2 lap children

Due to total number of installed O2 masks

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52
Q

Do not manually override autopilot during:

A

Normal Flight

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53
Q

Electrical Power
Electrical Load Limitations
Max Engine Generator Load
On Ground

A

300 amps

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54
Q

Max oil consumption:

A

1 quart per 8 hour period

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55
Q

EICAS Temperature Restrictions:
If ambient temperature is ISA + 36 degrees C or higher:

A

Operations without conditioned air are prohibited. Electrical power cannot be selected ON for power up. Cool the cockpit.

56
Q

Oil Limitations
Oil Pressure
Starting

A

0 - 220 psi

57
Q

Minimum speed in RVSM Airspace is _____ kts.

A

160 kts

58
Q

Takeoff is limited to Flaps ___ when Type II, III, or IV de/anti-ice fluid has been applied.

A

1

59
Q

Reverse thrust must be idle by ___ knots on landing rollout.

A

65 kts

60
Q

Emergency Fuel

A

1100 lbs

61
Q

Hot Spare Fuel

A

4800 lbs

62
Q

Minimum Battery Temp

Engine Start

A

-10° C

63
Q

Can you operate the APU during de/anti-icing procedures?

A

NO

64
Q

Initiate a missed approach if the FMS annunciator is not displayed or any of the following annunciators are displayed:

A

GPS NOT USED

DR

65
Q

When APU is operating, do not use reverse thrust longer than ___ seconds.

A

30

66
Q

After ___ minutes of APU operation in ambient temperatures of ___ degrees C or greater, keep ___ ___ ___ closed except for boarding or deplaning of crew or passengers.

A

45 minutes
30 degrees C
Main Cabin Door

67
Q

Max Airspeed

8,000’ - 29,833’

A

305 kts

68
Q

Max Zero Fuel Weight

A

21,430 lbs

70
Q

Battery Limits
Start Cycle
1 GPU Start < 1000 amps

A

1 Battery Start

71
Q

To use autothrottle during approach, set airspeed at _____ or greater.

A

Vref + 3

72
Q

Oil pressure less than ___ PSI but greater than or equal to ___ PSI is acceptable when the throttles are set to less than _____.

A

36
20
82% N1

73
Q

Minimum oxygen pressure for dispatch allows for O2 consumed by crew and number of passengers indicated during a ___ minute emergency descent from FL___ to _____ ft.

A

10 minute

FL450 - 10,000’

74
Q

Engine Limitations
Max ITT
TO, MCT, CRU, Reverse

A

920° C

75
Q

In icing conditions, maintain Flaps ___ configuration, except during approach and landing.

A

UP

76
Q

How many APU start attempts are allowed following a dual Gen failure?

A

1

77
Q

When do you arm the autothrottle?

A

When cleared for takeoff

78
Q

Minimum release fuel

A

2564 lbs

79
Q

Electrical Power
Electrical Load Limitations
Max Engine Generator Load
In Air
Above 35,000’

A

275 amps

80
Q

Do not use the autopilot or yaw damper for:

A

Takeoff or landing

81
Q

Battery Limits
Battery Power Only
Engine Starts Per Hour

A

3

82
Q

Can you use the autopilot when either PFD is in ATT or HDG reversion?

A

NO

83
Q

Ops review required for dry runway less than _____ ft.

A

4500’

84
Q 
Battery Limits
Start Cycle
1 GPU Start > 1000 amps
1 Gen Assisted Start
1 APU Start
A

1/3 Battery Start

85
Q

Max Airspeed

Mmo above 29,833’

A

.80 M

86
Q

Minimum runway width

A

70’

87
Q

Crewmember oxygen masks are not approved for sustained use above ______ ft cabin altitude.

A

40,000’

88
Q

Do not use WING ANTI-ICE above:

A

FL410

89
Q

What kind of approaches must be retrieved for CURRENT database?

A

GPS Approaches

90
Q

Electrical Power
Electrical Load Limitations
Max APU Generator Load
Ground or Inflight

A

275 amps

91
Q

Do not transmit on HF when NAV is based on ___.

A

ADF

92
Q

Ops Review required if DAAP runway length is less than _____ ft.

A

4500’

93
Q

Pressurization

Normal Differential Pressure

A

0 - 10.2 psi

94
Q

Minimum runway length distance is for release only. Upon arrival, use _____ computed distance for landing distance assessments.

A

LPA

95
Q

Idle speed is a function of ambient _____ and _____.

A

Temperature

Pressure

96
Q

Can the APU be operated unattended?

A

NO

97
Q

The APU Compartment must be inspected following an:

A

Automatic shutdown

98
Q

For gen cooling during ground ops, the engine must be operated at ____ with the gen load less than ___ amps for ___ minutes prior to shutdown. Otherwise, a ___ minute cooling period is required prior to attempting a restart.

A

IDLE
75 amps
4 minutes
35 minute

99
Q

Maximum runway slope

A

+/- 2%

100
Q

Max Takeoff + Landing Altitude

A

14,000’

101
Q

Oil Limitations
Oil Temperature
Minimum Starting Temp

A

-40° C/F

102
Q

Engine Limitations
N2
Flight Idle Minimum

A

65%

103
Q

Pressurization

Max Differential Overpressure

A

10.3 psi

104
Q

What must be operational if baggage is carried in the baggage compartment?

A

Smoke detection &

Extinguishing system

105
Q

The cabin must be _______ prior to opening the cabin door.

A

Depressurized

106
Q

Autothrottle __________ modes are unavailable when the radio altimeter is inoperative.

A

RETARD

107
Q

Oil Limitations
Transient Temperature
90 seconds

A

135 - 143 degrees C

108
Q

Oil Limitations
Transient Pressure
90 seconds

A

110 - 220 psi

109
Q

Max Airspeed

Speedbrake Extended

A

No Limit

109
Q

Min Airspeed

In Icing

A

180 kts

109
Q

The 5 minute takeoff thrust time limit commences when the throttle is first increased to _____.

A

TO

109
Q

Electrical Power
Electrical Load Limitations
Max Engine Generator Load
In Air (35,000’ or below)

A

300 amps

109
Q

Ops Review if runway width is less then ____ ft.

A

75’

110
Q

APU

Following shutdown, wait ___ sec. after RPM reads ___% before attempting restart.

A

30 seconds
0%

111
Q

Inclement Weather / Overnight Fuel

A

6000 lbs

112
Q

Single engine repositioning is only authorized for the following 2 events:

A

Uneven ramp, to check engine oil

Upwind engine exposed to a tailwind greater than 10 knots.

113
Q

Do not use _____ with any comparison monitor message and appropriate reversion not selected.

A

Autothrottle

114
Q

Three generator assisted cross starts are equal to _____ engine battery start.

A

One

115
Q

Do not use auxiliary hydraulic pump ___ _____ or when SAT is ____ degrees C.

A

In flight
-40 degrees C

116
Q

Auxiliary hydraulic pump is limited to ___ minutes (cumulative) of operation in any ___ consecutive minutes. After ___ minutes allow a ___ minute cooling period.

A

2
15
2
15

117
Q

Red EICAS AT HOLD FAIL is displayed when autothrottle TO Mode is active BUT …

A

the autothrottle has not entered the HOLD mode.
• one or both throttles did not reach takeoff position or
• autothrottle servo still receiving electrical power.

118
Q

If Type 2, 3, or 4 Anti-Ice Fluid has been applied, do not select WING ANTI-ICE ON until just prior to _____ _____.

A

Takeoff Thrust

119
Q

WING ANTI-ICE operation requires _____ to be selected ON.

A

ENGINE / STAB ANTI-ICE

120
Q

RNAV and RNP Operations:
Authorized RNAV Approach Minima

A

LNAV
LNAV/VNAV
LPV
LP

121
Q

RNAV and RNP Operations:
Enroute Class 1 RNAV / LRNS (Q & T Routes) for RNP-2 / RNAV-2 navigation require a current Nav Database except …

A

for Q or Y Routes in the Gulf of Mexico or WAT (pervious WATRS) airspace.

122
Q

VNAV
VNAV guidance altitudes must be displayed on the ____ or ____ ____ ____ when using VNAV for flight guidance.

A

MFD
Flight plan page

123
Q

GPS / GNSS Approach
Applicable annunciator (FMS, LPV, LP, L/VNAV) must be displayed at the ____.

A

FAF

124
Q

Approach
Visual Approach
The crew must visually verify that the course and path are _______.

A

Acceptable

125
Q

Engine Limitations
Cruise
MCT must be reduced to CRU either by the FADEC or manually within how many minutes of leveling off at cruise?

A

10 minutes

Citation Latitude (16 decks)

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