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Citation 650 > Limitations > Flashcards

Limitations Flashcards

1
Q

What is the Max Takeoff Wt

A

23,000 lbs.

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2
Q

Oper in HIGH (PAC FLOW) not approved for

A

TO and Landing Flight above 45,000 ft. Bleed air A/I sys on

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3
Q

Starter limits for start

A

3 starts per 30 minutes with one min rest period between cycles

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4
Q

Speed brakes with flaps prohibited

A

Below 500ft AGL

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5
Q

Max Ldg wt

A

20,000 lbs

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6
Q

Max number seats

Crew + PAX

A

15

2 Crew + 13 PAX

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7
Q

Time Limit to test Eng A/I On gnd above +10C

A

10 seconds

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8
Q

Max load factor Ldg

A

+3.5G at 20,000 lbs.

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9
Q

Altitude Speed brakes with flaps prohibited

A

Below 500ft AGL

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10
Q

APU Restriction on landing

A

TRs can only be used for 30 seconds

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11
Q

Spoiler Extend inflight Limit

A

Emergency descent only and on ground

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12
Q

Ground Idle Limit

A

Must be in HIGH for touch and Go landings

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13
Q

Maximum usable fuel quantity

A

Wings - 6484
Fuselage - 900
Max Usable- 7384

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14
Q

Min Spoiler Ext Speed

A

150 kts

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15
Q

Max Altitude

A

51,000 ft.

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16
Q

Radar Alt inop Limit

A

Must depart with flaps 20 land with full flaps

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17
Q

Max Alt TO and Ldg

A

14,000 ft

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18
Q

Operating in HP mode (PAC HP VLV Open) prohibited

A

During TO and LDG or with following sys:
WS bleed air
Wing AI
Eng AI

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19
Q

How many vortex gens can be missing for TO

A

One per wing

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20
Q

When does pressurization begin

A

TO roll above 75% N1

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21
Q

When must all A/I systems be on

A

Visible moisture TAT/RAT below +10c

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22
Q

PAC Bleed Air Switch (PAC HP VLV OPEN max Altitude

A

NORM or HP above 45,000ft

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23
Q 
Excessive climbing cabin altitude indications 
Light
Warn horn
EMR PRESS
Auto descent mode
A 
Cabin Alt 8500 ft light
Warning horn 10,000
EMR Press 13,500
Auto descent mode 13,500 and
Above 34,275 ft. FL350
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24
Q

Max Ramp wt

A

23,200 lbs

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25
Q

Max landing light ext Speed

A

250 kts

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26
Q

Rudder bias Limit

A

Rudder bias heater must be verified operational per preflight test

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27
Q

When can you select alternate Vmo

A

ZFW Less 15,350 lbs.

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28
Q

Max slush/water

A

0.75 inch

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29
Q

Max Altitude to start APU

A

20,000 ft

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30
Q

Max pressure Diff

Auto mode

Manual mode

A

Auto mode 9.3 paid

Manual mode 9.7

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31
Q

Radar Alt inop Limit

A

Must depart with flaps 20 land with full flaps

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32
Q

Spoiler Extend inflight Limit

A

EMR Descent Only

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33
Q

TR limits

A

Operationally checked first flight of day
Prohibited Touch and Go
Good only on paved runways

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34
Q

Max Turbulent sir penetration speed

A

200 KIAS or 0.75 Mach whichever is less

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35
Q

Emergency Pressurization Limit

A

Flight above 45,000ft. Both L and R Must be operational as per preflight test

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36
Q

Max tire Speed

A

165 kts

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37
Q

Oper in HIGH (PAC FLOW) not approved for

A

TO and Landing Flight above 45,000 ft. Bleed air A/I sys on

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38
Q

Cross gen start is how much of battery start

A

1/3 of a battery start

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39
Q

Maximum usable fuel quantity

A

Wings - 6484
Fuselage - 900
Max Usable- 7384

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40
Q

Ground Idle Limit

A

Must be in HIGH for touch and Go landings

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41
Q

Max altitude for takeoff and landing

A

14,000 ft.

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42
Q

Min Speed Brake Ext Speed

A

Vref+15

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43
Q

Min Alt for VNAV

A

500 Ft AGL

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44
Q

Fuselage fuel tank transfer must be started prior to

A

Wing fuel quantity 2,500lbs. ZFW CG aft of 327 or by 19,000 lbs.
Or
2,000 lbs. ZFW CG forward of 327 or by 19,000 lbs.

45
Q

Max Alt with Lo Hyd Temp

A

FL450

46
Q

BATT O’Temp

Steady temp?

Flashing temp?

A

Steady temp 60C BAT’O’TEMP Master Warn

Flashes 71C BAT’O’TEMP Master Warn

47
Q

Speed brakes with flaps prohibited

A

Below 500ft AGL

48
Q

Spoiler Extend inflight Limit

A

Emergency descent only and on ground

49
Q

Max load factor flaps 7 to full

A

-0.0 tp +2.0G at 22,000 lbs

50
Q

Max landing light ext Speed

A

250 kts

51
Q

Spoiler Extend inflight Limit

A

Emergency descent only and on ground

52
Q

When does pressurization begin

A

TO roll above 75% N1

53
Q

Vmca

A

103 kts.

54
Q

Max slush/water

A

0.75 inch

55
Q

Oper in HIGH (PAC FLOW) not approved for

A

TO and Landing Flight above 45,000 ft. Bleed air A/I sys on

56
Q

Pass Oxy Mask deploy Cabin Alt

A

13,500ft

57
Q

What is Max VMO below 8000

A

275 kts.

58
Q

Max Ramp wt

A

23,200 lbs

59
Q

Cross gen start is how much of battery start

A

1/3 of a battery start

60
Q

What is Vlo

What is Vle

A

Vlo and Vle 210 kts

61
Q

Vfe full flaps

A

Full flaps 170

62
Q

Max Turbulent air penetration speed

A

200 KIAS or 0.75 Mach whichever is less

63
Q

Reverse thrust to idle by

A

65 kts.

64
Q

Which wing feeds APU

A

Right Wing

65
Q

Max Altitude operation of stab anti-ice prohibited

A

FL410

66
Q

Max Altitude operation of stab anti-ice prohibited

A

FL410

67
Q

Max zero fuel wt

A

16,500 lbs

68
Q

Restrictions Ail Boost INOP

A

Basic Autopilot (Pitch & Roll

69
Q

Max asymmetric fuel imbalance

A

Normal 200 lbs.

Emergency 800 lbs.

70
Q

APU Restriction on landing

A

TRs can only be used for 30 seconds

71
Q

GPU Min amps for starting

A

1,000 Amps

72
Q

Max Speed Brake Ext Speed

A

No limit

73
Q

Time limit on gnd with EFIS FAN light illuminated

A

10 min and must maintain VFR

74
Q

Operating in HP mode (PAC HP VLV Open) prohibited

A

During TO and LDG or with following sys:
WS bleed air
Wing AI
Eng AI

75
Q

Vfe Full Flaps

A

170 kts

76
Q

Max pressure Diff

Auto mode

Manual mode

A

Auto mode 9.3 paid

Manual mode 9.7

77
Q

No Takeoff Warning Items

6 Items

A
  1. Cabin door light
  2. Trim out of Takeoff Range
  3. flaps up or full
  4. Gust lock
  5. Speed Brakes not down
  6. Spoiler hold on
78
Q

Battery Limit for Eng/APU

A

3 Eng/APU per hour

79
Q 
Gen Amp Limit 
Takeoff
Gnd ops 
Up to FL 410
Up to FL 470
Above FL 470
Single gen
A 
Gen Amp Limit 
Takeoff 365 amps
Gnd ops 300 amps
Up to FL 410 300 amps
410 to FL 470 200 amps
Above FL 470 200 amps
Single gen 365 amps up to FL 250
80
Q

When can you select alternate Vmo

A

ZFW Less 15,350 lbs.

81
Q

Radio Alt limits for takeoff and Ldg

A

Must be on, operative and Tested to TO flaps 7 or land flaps 20

82
Q

Radar Alt inop Limit

A

Must depart with flaps 20 land with full flaps

83
Q

Authorized operations

5 Items

A 
Day
Night
VFR
IFR
Known icing conditions
84
Q

Operating in HP mode (PAC HP VLV Open) prohibited

A

During TO and LDG or with following sys:
WS bleed air
Wing AI
Eng AI

85
Q

Max Loaf Factor Flaps Up

A

-1 to +3 Gs at 23,000 lbs.

86
Q

Time Limit to test Eng A/I On gnd above +10C

A

10 seconds

87
Q

Vmcg 23,000 lbs

A

116 kts

88
Q

Max Alt to operate both PACs on one bleed source (Isolation valve open) in HI flow

A

Above 25,000 ft.

89
Q

When must all A/I systems be on

A

Visible moisture TAT/RAT below +10c

90
Q

Anti skid required for TO

A

Must be on unless using supplement 11

91
Q

Min alt autopilot use

A

200ft AGL

autopilot and Yaw damper must be off for TO and Ldg

92
Q

Reverse thrust to idle by

A

65 kts.

93
Q

Approved Hydraulic fluid

Color

A

Braco

Red

94
Q

Rudder bias Limit

A

Rudder bias heater must be verified operational per preflight test

95
Q

Max Reverse Limit

A

90% TO thrust

96
Q

Max Ldg wt

A

20,000 lbs

97
Q

Max altitude to operate APU

A

30,000 ft.

98
Q

Crosswind limitations?

Without T/R deploy

With T/R deploy

Ailerons or roll Spoilers inop

A

Without T/R deploy 25 kts.

With T/R deploy limiting 25 kts.

Ailerons or roll Spoilers inop 10 kts

99
Q

Max Tailwind component

A

10 kts.

100
Q

Max Air Temp TO and LDG

A

ISA +37C

101
Q

Max VMo below 8,000 ft.

A

275 kts.

102
Q

What type engine and max thrust

A

Garrett TFE.731-4R/2S

4080 lbs.

103
Q

What Items are on The hydraulic system
6 items
Aux system
3 items

A 
1 Landing gear
2 NW steering 
3 Spoilers
4 Speed brakes 
5 Aileron boost
6 Thrust Reversers
7 Spoiler Holddown - Aux system 
8 Brakes - Aux system
9 Roll spoilers - Aux System
104
Q

Max altitude with Hyd Press Low or Fluid Loss

A

45,000 ft.

105
Q

Charge batteries from GPU 4

A

No battery less than 23VDC
Batteries must be charged together
No longer than 4 hours
Ambient air temperature less than 100°F

106
Q

Autopilot limitation

A

One pilot must remain in his seat with seatbelt and shoulder harness fastened during all autopilot operations.

107
Q

Manual engagement of altitude hold mode is prohibited when the airplane descent rate is greater than _______ ft. per minute.

A

5,500

108
Q

Maximum dual generator loads?

A

Up to 41,000 ft. 300 amps
Above 41,000 ft. 250 amps
Above 47,009 ft. 200 amps

109
Q

Flap extension or landing gear is prohibited above ______ altitude.

A

20,000 ft.

Citation 650 (2 decks)

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