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Citation CE-560XL > Excel (N560VS) Limitations > Flashcards

Excel (N560VS) Limitations Flashcards

1
Q

Maximum Design Ramp Weight

A

20,200

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2
Q

Maximum Design Takeoff Weight

A

20,000

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3
Q

Maximum Design Landing Weight

A

18,700

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4
Q

Maximum Design Zero Fuel Weight

A

15,000

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5
Q

Minimum Flight Weight

A

12,400

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6
Q

Maximum Tailcone Baggage Weight

A

700

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7
Q

Takeoff weight is limited by the most restrictive of…

A
  1. Maximum Certified Takeoff Weight
  2. Max Weight Permitted by Climb Requirements
  3. Takeoff Field Length
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8
Q

Landing weight is limited by the most restrictive of…

A
  1. Maximum Certified Landing Weight
  2. Max Landing Weight Permitted by Climb Requirements or Brake Energy Limit
  3. Landing Distance
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9
Q

Center of Gravity Limits Envelope

A

Refer to Figure 2-1

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10
Q

Max Takeoff Thrust Time Limit

A

5 minutes (10 minutes for OEI)

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11
Q

Max Takeoff ITT

A

720

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12
Q

Max Continuous ITT

A

720

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13
Q

Max Starting ITT

A

720** (Refer to Figure 2-3)

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14
Q

Max Transient ITT

A

760 - 20 seconds (Refer to Figure 2-3)

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15
Q

Max Takeoff N2

A

101.8%

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16
Q

Max Continous N2

A

101.8%

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17
Q

Min Ground Idle N2

A

47.0% MIN (EEC Mode Only)

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18
Q

Min Flight Idle N2

A

51.5% MIN (EEC or MANUAL Mode)

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19
Q

Max Transient N2

A

103.0% - 20 seconds (Refer to Figure 2-4)

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20
Q

Max Takeoff N1

A

100.0%

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21
Q

Max Continuous N1

A

100.0%

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22
Q

Max Transient N1

A

102.0% - 20 seconds (Refer to Figure 2-4)

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23
Q

Normal Oil Pressure - Takeoff and Max Continuous

A

45 - 140 (Above 60% N2)

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24
Q

Start Oil Pressure may exceed 140PSI…

A

(Not to exceed 250) for up to 300 seconds

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25
Q

Normal Oil Pressure - Ground Idle

A

25(MIN) - 140

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26
Q

Normal Oil Pressure - Flight Idle

A

25(MIN) - 140

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27
Q

Min Transient Oil Pressure - 20 Seconds

A

0

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28
Q

Transient Oil Pressure - 120 Seconds

A

20(MIN)

250(MAX)

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29
Q

Normal Oil Temp - Takeoff and Max Continuous

A

10 - 121.1

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30
Q

Min Oil Temp - Ground and Flight Idle

A

-40 - 121.1

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31
Q

Min Oil Temp - Starting

A

-40

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32
Q

Max Transient Oil Temp

A

135 - 120seconds

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33
Q

Starter Limitation

A

3 cycles per 30 minutes w/ 90 second rest

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34
Q

Battery Limitation

A

3 cycles per hour

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35
Q

Cross-Gen Start =

A

1/3 battery start

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36
Q

EPU Start

A

0 battery start

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37
Q

APU Start =

A

Same as Battery Start Limits per SB

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38
Q

EPU Requirement

A

28VDC and 800amp (MIN)

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39
Q

EPU Limits

A

> 28VDC or 1000amp may damage starter

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40
Q

Ground operation of pitot static heat is limited to…

A

2 min to preclude damage to pitot tubes and AOA vane

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41
Q

Max Generator Load for Ground Operations

A

200amp (w/ transients 250amp - 4 minutes)

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42
Q

Normal Avionics Gound Operating Limit

A

See Figure 2-5

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43
Q

N560VS Hydraulic Fluid

A

Skydrol

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44
Q

Approved Hydraulic Fluids

A

See List

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45
Q

Approved Engine Oils

A

See List

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46
Q

N560VS Engine Oil

A

Mobil Jet Oil II

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47
Q

Max Oil Consumption

A

1qt per 10hr

See maint. manual if more

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48
Q

Max mixing of approved oils

A

2qt per 400hr

>2qt - drain and flush

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49
Q

If non-approved oils mixed

A

Drain and Flush

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50
Q

Single Point Refueling Pressure

A

10-55 psi

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51
Q

Max De-Fueling Pressure

A

-10 psi

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52
Q

FUEL BOOST pumps ON when…

A

LO FUEL LEVEL annunciator or 400lb or less

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53
Q

FUEL BOOST pumps ON when…

A

LO FUEL LEVEL annunciator or 400lb or less

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54
Q

Approved Fuels

A

See Figure 2-6

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55
Q

Fuel ANTI-ICE Additive required?

A

NO

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56
Q

Jet A Min Fuel Temp

A

-40C

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57
Q

Jet A Max Fuel Temp

A

+57C

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58
Q

Jet A Max Altitude

A

45000

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59
Q

Max Fuel Imbalance - Normal Operation

A

400lb

60
Q

Max Fuel Imbalance - Emergency Return

A

800lb

61
Q

Mmo

A

.75 (above 26,515)

62
Q

Vmo 8000-26,515

A

305

63
Q

Vmo <8000

A

260

64
Q

Va

A

See Figure 2-9

65
Q

Vfe (7-15 deg)

A

200

66
Q

Vfe ( 35 deg)

A

175

67
Q

Vle

A

250

68
Q

Vlo

A

Extend - 250

Retract - 200

69
Q

Vsb

A

No Limit

70
Q

Vmca

A

90

71
Q

Vmcg

A

81

72
Q

Vmcl

A

92

73
Q

Max Autopilot Speed

A

305 / .75

74
Q

Max Takeoff and Landing Altitude

A

14,000

75
Q

Max Tailwind

A

10

76
Q

Max Takeoff and Landing Ambient Temp

A

ISA+39 (Figure 2-8)

77
Q

Min Takeoff and Landing Ambient Temp

A

-54C (See Figure 2-8)

78
Q

The autopilot and yaw damper must be…

A

OFF for takeoff and landing

79
Q

Max Tire Ground Speed

A

165

80
Q

Lavatory doors…

A

must be latched open for takeoff and landing.

Emergency Exit

81
Q

Engine sync must be…

A

OFF for takeoff and landing

82
Q

Takeoffs and landings are limited to…

A

paved runway surfaces.

83
Q

Takeoffs and landings are limited to…

A

paved runway surfaces.

84
Q

Takeoff from a wet runway when using thrust reversers for for performance credit is limited to…

A

75ft MIN

85
Q

Antiskid must…

A

be operational for takeoff and landing

86
Q

Rudder Bias Requirements for Takeoff

A
  1. Bias - Operational
  2. Rudder Bias Heat - Operational
  3. Satisfactory Preflight Test - Section III, Normal Proc.
87
Q

Takeoff prohibited with frost adhering to…

A
  1. Wing Leading Edge
  2. Upper Wing Surface
  3. Windshield
88
Q

Takeoff prohibited with ice, snow or slush adhering to…

A
  1. Wing Leading Edge and Upper Surface
  2. Flight Control Surfaces Including All Hinge Gaps
  3. Horizontal Stabilizer
  4. Vertical Stabilizer
  5. Engine Inlets
  6. Top of Engine Pylons
  7. Top of Fuselage
  8. Windshield
  9. All Static Ports
  10. Angle of Attack Vane
  11. Upper Surface of Nose Forward of Windshield
89
Q

Takeoff prohibited with ice, snow or slush adhering to…

A
  1. Wing Leading Edge and Upper Surface
  2. Flight Control Surfaces Including All Hinge Gaps
  3. Horizontal Stabilizer
  4. Vertical Stabilizer
  5. Engine Inlets
  6. Top of Engine Pylons
  7. Top of Fuselage
  8. Windshield
  9. All Static Ports
  10. Angle of Attack Vane
  11. Upper Surface of Nose Forward of Windshield
90
Q

Refer to … for information on Ground Deicing

A

Section VII, Advisory Information

91
Q

A visual and tactile inspection of wing leading edge and upper surface must be performed when…

A

< +6C or Unknown Fuel Temp >0C when

  1. Visible moisture, or
  2. Water on upper wing surface, or
  3. <3C temp/dew point spread
  4. Conditions conducive to frost
92
Q

Takeoff with Red Annunciator?

A

NO

93
Q

Takeoff with Amber Annunciator?

A

Only if Deferred per MEL

94
Q

Min Icing Airspeed (Except TO and Ldg)

A

160

95
Q

Max Operating Altitude

A

45,000

96
Q

Max VGs Missing

A

3

97
Q

Max Altitude w/ 1-3 VGs Missing

A

41,000

98
Q

Max Enroute Ambient Temp

A

See Fig 2-8

99
Q

Min Enroute Ambient Temp

A

See Figure 2-8

100
Q

Max Generator Load

A

300amp

101
Q

When the airplane has been exposed to prolonged (>2hr) at temps < -7C cabin must be warmed to at least…

A

+13C prior to flight above FL250 to verify proper deployment of passenger oxygen masks.

102
Q

Severe Icing Limits

A

See AFM Limitations

103
Q

Number of VGs

A

52 (26 per wing)

104
Q

Number of Boundary Layer Energizers (BLE)

A

22 (11 per wing)

105
Q

Max Number of BLEs missing

A

0

106
Q

Min Flight Crew for All Operations

A

1 pilot and 1 copilot

107
Q

Max Load Factor

A

Flaps 0: -1.2G to +3.0G at 20,000lb
Flaps 7-35: 0.0G t0o +2.0G at 20,000lb
(Limits bank angle and pull-up maneuvers)

Landing: 0.0G to +2.0G at 18,700
(Limits rate of descent to 600fpm)

108
Q

Max Load Factor

A

Flaps 0: -1.2G to +3.0G at 20,000lb
Flaps 7-35: 0.0G t0o +2.0G at 20,000lb
(Limits bank angle and pull-up maneuvers)

Landing: 0.0G to +2.0G at 18,700
(Limits rate of descent to 600fpm)

109
Q

Normal Cabin Pressurization Limits

A

0.0 - 9.6 +/-0.1 PSI

110
Q

Pressure Relief Valve

A

9.5 +/-0.1 PSI

111
Q

Pressurization Gauge Redline

A

9.7 +/-0.1 PSI

112
Q

No acrobatic maneuvers, including spins above…

A

25,000

113
Q

For all takeoffs and landings, passenger seats must be…

A
  1. fully upright and outboard

2. seat belts and shoulder harnesses fastened

114
Q

Max number of passengers (per AFM, not configuration)

A

12

115
Q

If BATT O’TEMP illuminates during ground operation…

A

…do not takeoff.

116
Q

One pilot must be seated w/ seatbelt fastened for…

A

…all autopilot operations.

117
Q

Autopilot operation is prohibited if any … illuminates during flight.

A

Comparison Monitor Annunciator

118
Q

Minimum Autopilot Altitudes

A

Enroute - 1000AGL
Non-Precision Approach - 300AGL
Precision Approach - 180AGL

119
Q

Max Altitude for Continuous O2 Mask Use

A

Crew - 40,000

Passenger - 25,000

120
Q

Reverse thrust must be reduced to idle detent by…

A

…60kt

121
Q

Max Reverse Thrust

A

Approx 75% of Takeoff Thrust

122
Q

Engine static ground operation is limited to … with thrust reversers deployed

A

… idle power …

123
Q

Use of thrust reversers is prohibited for…

A

…touch and go landings

124
Q

Thrust reversers must be checked…

A
  1. First Flight of the Day
  2. Any Flight using TR for Performance Credit
  3. First Flight after ANY Maintenance
125
Q

The use of thrust reversers is prohibited to…

A

…back the airplane

126
Q

APU operation is prohibited until a…

A

…satisfactory test has been accomplished.

127
Q

Starting the APU is prohibited whenever…

A

APU FAIL illuminated

128
Q

APU start is prohibited…

A

after a dual generator failure

129
Q

Following shutdown for any reason, APU restart must not be attempted until…

A

…30 sec after RPM reads 0%

130
Q

Applying deice/anti-ice fluid is prohibited with…

A

APU operating

131
Q

Max Thrust Reverser Deployed Time w/ APU Operating

A

30 seconds

132
Q

APU is not approved for…

A

unattended operation

133
Q

APU is not approved for…

A

unattended operation

134
Q

Max APU Start Altitude

A

20,000

135
Q

Max APU Operating Altitude

A

30,000

136
Q

Max APU EGT

A

690 (will shut down automatically if EGT limit exceeded)

137
Q

Max APU RPM%

A

108%

138
Q

Max/Min APU Fuel Temp

A

Same as Engine Limitations

139
Q

Max APU Generator Load

A

Ground: 200amp
Flight: 230amp

140
Q

Max/Min APU Operating Temp

A

-54C/+54C

141
Q

APU Starter Limits

A

3 cycles per 30min w/ 90sec rest between cycles

142
Q

APU Battery Start Limits

A

9 per hour (0 if Ext Pwr used to start APU)

143
Q

APU … assist during main engine start.

A

DOES NOT

144
Q

Min Tail Deice Temp (RAT)

A

<150kt: -40C

>150kt: -35C

145
Q

If AHRS moved to DG mode, it must…

A

…remain in DG mode for remainder of flight.

Citation CE-560XL (3 decks)

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