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NETJETS CITATION LATITUDE STUDY 1 > 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

FADEC automatically aborts start for:

A
  1. Insufficient ITT rise in 15 sec.

2. ITT limit is exceeded

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6
Q

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

A

90 seconds

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7
Q

Oil Pressure

Ground / Flight Idle

A

20 - 110 psi

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8
Q

If OAT is at or above 26 degrees C, and avionics are operated continuously:

A

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

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9
Q

Reverse Thrust Time Limit

A

5 minutes

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11
Q

Max Tailcone Baggage

A

1,000 lbs

150 lbs/ft2

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13
Q

Max ITT

Starting

A

950° C

5 sec. linear, 1000° 3 sec.

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14
Q

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

A

30 seconds

0%

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15
Q

Can you use the autopilot when in flight engine start is attempted with starter assistance?

A

NO

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16
Q

Oil Temp
Takeoff - Continuous
Ground / Flight Idle

A

16 - 135° C

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17
Q

N1 / N2

Takeoff - Continuous

A

105%

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18
Q

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

A

MAX COOL ON

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19
Q

The APU compartment must be inspected after an:

A

Automatic Shutdown

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20
Q

Fuel
Pressure refueling limits
PSI

A

10 - 55 psi

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21
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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22
Q

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

A

25,000’

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23
Q

Cockpit temperatures of 31 - 35 degrees C:

A

Limit ground operations of avionics to 30 minutes.

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24
Q

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

A

Reversion Mode

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25
Q

Oil Pressure

Takeoff - Continuous

A

36 - 110 psi

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26
Q

N2

Ground Idle Minimum

A

57%

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27
Q

Fuel
Max Defueling pressure
PSI

A

-10 psi

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28
Q

Max continuous static ground operation at TO is limited to:

A

2 minutes

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29
Q

Max Tire Groundspeed

A

182 kts

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32
Q

Reverse thrust must be ____ during static operations.

A

IDLE

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34
Q

Min Airspeed

Speedbrake Extended

A

Vref + 15

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35
Q

Max Airspeed

Below 8,000’

A

270 kts

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36
Q

Minimum Dry Runway Length for release

A

4000’

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37
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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38
Q

Engine Type

A

Pratt and Whitney

P306D1

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39
Q

Minimum Battery Temp

APU Start

A

-20° C

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40
Q

Engine Thrust

A

5907 lbs. @ Sea Level

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41
Q

Can you use the autopilot when either AHRS has failed?

A

NO

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42
Q

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

A

5000’

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43
Q

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

A

NO

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44
Q

Flight in _____ _____ is prohibited.

A

Freezing Rain

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45
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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46
Q

45 minute IFR Reserve fuel:

A

1464 lbs

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47
Q

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

A

3 - 5

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48
Q

Maximum GPU load

A

1500 amps

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49
Q

Can you back the aircraft with reverse thrust?

A

NO

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50
Q

Max Flap / Landing Gear

Extended Altitude

A

18,000’

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52
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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53
Q

Min Airspeed

S/E Enroute Climb

A

180 kts

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54
Q

Do not use reverse thrust when conducting:

A

Touch and Go landings

55
Q

Max number of passengers:

A

8 plus 2 lap children

Due to total number of installed O2 masks

56
Q

Do not manually override autopilot during:

A

Normal Flight

57
Q

Electrical Power
Max Amps
Engine - on Ground

A

300 amps

58
Q

Max oil consumption:

A

1 quart per 8 hour period

59
Q

Cockpit temperatures of 36 degrees C or higher:

A

Cool the cockpit before operating avionics.

60
Q

Oil Pressure

Starting

A

0 - 220 psi

61
Q

Minimum speed in RVSM Airspace is _____ kts.

A

160 kts

62
Q

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

A

1

63
Q

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

A

65 kts

64
Q

Emergency Fuel

A

1100 lbs

65
Q

Hot Spare Fuel

A

4800 lbs

66
Q

Minimum Battery Temp

Engine Start

A

-10° C

67
Q

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

A

NO

68
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

69
Q

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

A

30

70
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

71
Q

Max Airspeed

8,000’ - 29,833’

A

305 kts

72
Q

Max Zero Fuel Weight

A

21,430 lbs

74
Q

Battery Limits
Start Cycle
1 GPU Start < 1000 amps

A

1 Battery Start

75
Q

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

A

Vref + 3

76
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

77
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’

78
Q

Max Continuous / Takeoff

ITT

A

920° C

79
Q

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

A

UP

80
Q

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

A

1

81
Q

When do you arm the autothrottle?

A

When cleared for takeoff

82
Q

Minimum release fuel

A

2564 lbs

83
Q

Electrical Power
Max Amps
Engine - in Air
Above 35,000’

A

275 amps

84
Q

Do not use the autopilot or yaw damper for:

A

Takeoff or landing

85
Q

Battery Limits
Battery Power Only
Engine Starts Per Hour

A

3

86
Q

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

A

NO

87
Q

Ops review required for dry runway less than _____ ft.

A

4500’

88
Q 
Battery Limits
Start Cycle
1 GPU Start > 1000 amps
1 Gen Assisted Start
1 APU Start
A

1/3 Battery Start

89
Q

Max Airspeed

Mmo above 29,833’

A

.80 M

90
Q

Minimum runway width

A

70’

91
Q

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

A

40,000’

92
Q

Do not use WING ANTI-ICE above:

A

FL410

93
Q

What kind of approaches must be retrieved for CURRENT database?

A

GPS Approaches

94
Q

Electrical Power
Max Amps
APU - Ground or Inflight

A

275 amps

95
Q

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

A

ADF

96
Q

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

A

4500’

97
Q

Pressurization

Normal Differential Pressure

A

0 - 10.2 psi

98
Q

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

A

LPA

99
Q

Idle speed is a function of ambient _____ and _____.

A

Temperature

Pressure

100
Q

Can the APU be operated unattended?

A

NO

101
Q

The APU Compartment must be inspected following an:

A

Automatic shutdown

102
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

103
Q

Maximum runway slope

A

+/- 2%

104
Q

Max Takeoff + Landing Altitude

A

14,000’

105
Q

Oil Temperature

Minimum Starting Temp

A

-40° C/F

106
Q

N2

Flight Idle Minimum

A

65%

107
Q

Can you land with the autothrottles with other than flaps FULL?

A

NO

108
Q

Pressurization

Max Differential Overpressure

A

10.3 psi

109
Q

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

A

Smoke detection &

Extinguishing system

110
Q

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

A

Depressurized

111
Q

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

A

RETARD

112
Q

Oil Temp
Transient
90 seconds

A

135 - 143 degrees C

113
Q

Oil Pressure
Transient
90 seconds

A

110 - 220 psi

114
Q

Ops Review if runway width is less then ____ ft.

A

75’

115
Q

APU

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

A

30 seconds
0%

116
Q

Inclement Weather / Overnight Fuel

A

5000 lbs

117
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.

118
Q

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

A

Autothrottle

119
Q

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

A

One

120
Q

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

A

In flight
-40 degrees C

121
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

122
Q

Electrical Power
Max Amps
Engine - in Air

A

300 amps

123
Q

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

A

TO

124
Q

Min Airspeed

In Icing

A

180 kts

125
Q

Max Airspeed

Speedbrake Extended

A

No Limit

NETJETS CITATION LATITUDE STUDY 1 (15 decks)

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