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Citation Latitude > Limitations > Flashcards

Limitations Flashcards

1
Q

Min Reserve Fuel

A

1464

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2
Q

Min Fuel for Release

A

2564

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3
Q

Hot Spare Fuel Load

A

4800

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4
Q

Minimum Runway Dry

A

4000x70

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5
Q

Maximum Crosswind Dry/Wet

A

30 Knots

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6
Q

Max Crosswind Contaminated Runway

A

More than 150 wide- 15

Less than 150 wide- 10

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7
Q

Maximum Tailwind for Takeoff or Landing

A

10 Knots

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8
Q

Maximum Ramp/Taxi Weight

A

31,050

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9
Q

Max Takeoff Weight

A

30,800

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10
Q

Max Landing Weight

A

27,575

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11
Q

Max Zero Fuel Weight

A

21,430

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12
Q

Max Operating Altitude

A

45,000

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13
Q

Max Flap and Gear Extended Altitude

A

18,000

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14
Q

Max Altitude for Takeoff and Landing

A

14,000

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15
Q

Minimum Altitude for Speedbrake Extension

A

500 AGL

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16
Q

Vmo

A

Below 8,000-270

Above 8,000-305

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17
Q

Mmo

A

.80

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18
Q

Turbulent Air Penetration

A

225/.73

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19
Q

Vlo/Vle

A

210

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20
Q

Max Tire speed

A

182

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21
Q

Flaps 1 speed and auto throttle

A

Max-250

Auto Throttle- 190

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22
Q

Flaps 2 speed and auto throttle

A

Max-200

Auto Throttle- 160

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23
Q

Flaps Full speed and auto throttle

A

Max-175

Auto Throttle-120

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24
Q

Min holding speed in icing

A

180 knots

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25
Q

Minimum speed for speedbrake extension

A

Vref+15

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26
Q

Above FL410 Bleed Air

A

L & R ENG BLD AIR to NORM or HP and PRESS SOURCE to NORM

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27
Q

Normal DP

A

0-10.2

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28
Q

Max DP

A

10.3

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29
Q

Max Passengers

A

8 + 2 Lap children

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30
Q

Oxygen Masks Altitude Limit

A

Crewmember- FL400

PAX-FL250

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31
Q

APU Starter Limits

A

3 Starts with 90 Seconds in between in 30 min period

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32
Q

APU Max Airspeed start

A

305 Knots

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33
Q

APU Max Altitude Start

A

FL200

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34
Q

APU Do Not Operate

A

During ground De/Anti-icing

MAX Cool on while manually operating cockpit and cabin temps

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35
Q

Cabin door closed with APU running

A

After 45 mins of APU operation in temps greater than 30 C

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36
Q

APU Max Operating Altitude

A

FL300

37
Q

APU Max Speed

A

305/.80

38
Q

Autopilot min altitude En Route or descent

A

1000 AGL

39
Q

Autopilot min altitude ILS/ LPV

A

160

40
Q

Autopilot min altitude all other approach types

A

200

41
Q

Autopilot min altitude takeoff climb and missed

A

400

42
Q

Autothrottle on ground limits

A

Arm only when cleared for takeoff

Autothrottle HOLD must be displayed prior to 65 knotsq

43
Q

Autothrottle in air limits

A

do not engage above 65 on ground or below 400 feet

Disengage prior to landing with flaps other than full

44
Q

Battery starting limits

A

3 start attempts per hour

45
Q

GPU assisted start

A

3 starts more than 1000 amps- 1 battery start

1 start less than 1000 amps- 1 battery start

46
Q

Generator assisted cross start

A

3 generator assisted starts-1 battery start

47
Q

APU battery limits

A

9 APU starts per hour

48
Q

Voltage for battery start

A

Displayed green (23-32V)

49
Q

Max GPU voltage

A

30V

50
Q

Mas GPU Load

A

1500A

51
Q

Max Engine Gen load in flight or on ground

A

300A

52
Q

Max load for engine generator above FL350 and APU

A

275A

53
Q

Pressure refueling limits

A

10-55 PSI

54
Q

Max Defueling pressure

A

-10 PSI

55
Q

Total Fuel Quanity

A

11,390 pounds

56
Q

Max Fuel inbalance

A

400

57
Q

When to turn on anti icing

A

ENG/STAB 10 to -35C (3-5 mins prior to entering conditions)

Wing- 5 to -35C

58
Q

Max SAT for bleed air anti ice with thrust levers above idle

A

20C

59
Q

Pitot Static Anti Ice limit

A

2 mins on ground

60
Q

Anti Ice Fluid Limit

A

Limited to Flaps 1 take off

61
Q

Wing Anti Ice limit

A

Do not operate above FL410

62
Q

Temp Restrictions ISA +26

A

Provide conditioned air to cockpit and close cabin door

63
Q

Temp Restrictions ISA+31

A

Limit ground operation of avionics to 30 mins without conditioned air

64
Q

Temp Restrictions ISA +36 or higher

A

Prohibited

65
Q

Approach Category

A

Cat B if approach speed is faster than 120 use Cat C

66
Q

Max tailwind Component for Engine Start

A

10 Knots

67
Q

Max Continuous at cruise

A

10 mins

68
Q

Max Take off/MCT/CRU/Reverse Thrust N1

A

105

69
Q

Max Take off/MCT/CRU/Reverse Thrust N2

A

105

70
Q

Max Take off/MCT/CRU/Reverse ITT

A

920

71
Q

Take off thrust Time limit

A

AEO- 5 Mins

OEI- 10 Mins

72
Q

Reverse Thrust time Limit

A

5 Mins

73
Q

Ground Idle Min N2

A

57

74
Q

Flight Idle min N2

A

65

75
Q

Starting ITT limit

A

950 for 5 Seconds

76
Q

Transient N1 N2 and ITT

A

N1-106
N2-106
ITT-950
20 Seconds

77
Q

Oil Pressure above flight idle

A

36-110 PSI

78
Q

Oil Temp

A

16-135

79
Q

Ground and Flight Idle Oil Pressure

A

20-110

80
Q

Starting Oil pressure

A

0-220

81
Q

Min oil temp to start

A

-40

82
Q

Transient 20 sec oil pressure

A

0-20

83
Q

Transient 90 sec oil pressure

A

110-220

84
Q

Transient 90 sec oil Temp

A

135-143

85
Q

Engine Starter limits

A

Attempt Cooldown
1- 2 mins
2- 5 mins
3- 30 mins

86
Q

Motoring Limitations

A

Batteries only- 20 seconds
batteries with gen assist- 15 seconds
GPU 1000A- 15 seconds
GPU 1500A- 7 Seconds

87
Q

Thrust reverser limitations (4)

A

must be at idle at 65 knots
when APU in operation do not use reverse thrust for more than 30 seconds
do not use reverse thrust when conducting touch and gos
do not use to back the aircraft

88
Q

Aux hydraulic pump limit

A

do not use in flight or if SAT is -40

89
Q

Aux hydraulic pump ground limit

A

2 mins cumulative in any 15 min period. after 2 mins allow 15 min cooldown

Citation Latitude (4 decks)

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