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Citation Encore (N430AM) > N430AM Limitations > Flashcards

N430AM Limitations Flashcards

1
Q

Max Design Ramp Wt.

A

16,830

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2
Q

Max Design Takeoff Wt.

A

16,630

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3
Q

Takeoff weight is limited by the most restrictive of…

A
  1. Max Certified Takeoff Weight
  2. Max TO Wt. Permitted by Climb Requirements
  3. Takeoff Field Length (TOFL)
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4
Q

Max Design Landing Wt.

A

15,200

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5
Q

Landing weight is limited by the most restrictive of…

A
  1. Max Certified Landing Weight
  2. Max Landing Wt. Permitted by Climb Requirements or Brake Engergy
  3. Landing Distance
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6
Q

Max Design Zero Fuel Wt.

A

12,600

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7
Q

Max Nose Baggage Wt.

A

310

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8
Q

Max Tail Baggage Compartment Wt.

A

Fwd: 300
Aft: 200

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9
Q

Center of Gravity Limits

A

Refer to Figure 2-1

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10
Q

Engine Type

A

Pratt and Whitney Canada Inc.
PW535A
3400lb Thrust

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11
Q

Max Takeoff ITT

A

700 (5min)

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12
Q

Takeoff Thrust Time Limit

A

5min (10min OEI)

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13
Q

Max Continuous ITT

A

700

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14
Q

Max Starting ITT

A

740 (5sec)

Refer to Figure 2-3

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15
Q

Max Transient ITT

A

740 (20sec)

Refer to Figure 2-4

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16
Q

Max Takeoff N2

A

100%

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17
Q

Max Continuous N2

A

100%

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18
Q

Min Ground Idle N2

A

49.1% MIN

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19
Q

Min Flight Idle N2

A

52.9% MIN

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20
Q

Max Transient N2

A

102% (20sec)

Refer to Figure 2-3

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21
Q

Max Takeoff N1

A

100%

Limited by TO Charts, Section IV

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22
Q

Max Continuous N1

A

100%

Limited by Climb/Cruise Charts, Section IV

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23
Q

Max Transient N1

A

102% (20sec)

Refer to Figure 2-3

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24
Q

Normal Takeoff Oil Pressure

A

45 TO 140

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25
Q

Normal Continuous Oil Pressure

A

45 TO 140

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26
Q

Transient Oil Pressure (20 Seconds)

A

0 MIN

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27
Q

Transient Oil Pressure (400 Seconds)

A

20 TO 270

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28
Q

Normal Oil Pressure - Ground Idle

A

25 TO 140

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29
Q

Normal Oil Pressure - Flight Idle

A

25 To 140

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30
Q

Takeoff Oil Temp

A

10 TO 132.2

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31
Q

Continuous Oil Temp

A

10 TO 132.2

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32
Q

Ground Idle Oil Temp

A

-40 TO 132.2

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33
Q

Flight Idle Oil Temp

A

-40 TO 132.2

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34
Q

Min Starting Oil Temp

A

-40

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35
Q

Max Transient Oil Temp

A

140.5 MAX

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36
Q

Starter Limitations

A

3 per 30 Min (90 Seconds Rest)

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37
Q

Battery Limitations

A

3 per hour

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38
Q

Generator assisted cross-start =

A

1/3 Battery Start

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39
Q

EPU start =

A

No battery cycle

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40
Q

EPU Requirements

A

28V

800-1000 amps

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41
Q

Continuous Engine Ground Operation Limit

A

5 Min

Temp Range - Figure 2-8

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42
Q

Pitot/Static Ground Operation Time Limit

A

2 min ON - 2 min OFF

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43
Q

Max Generator Load - Ground Idle

A

125 amp

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44
Q

Max Generator Load - Flight Idle

A

225 amp

45
Q

Max Transient Generator Load - Ground Ops

A

300 amp up to 4 min

46
Q

Avionics time limit begins…

A

when avionics are powered on (Figure 2-5)

47
Q

Approved Hydraulic Fluid

A

See Limitations

We use Skdrol

48
Q

Approved Engine Oil

A

See Limitations

We use 2380

49
Q

Mixing Approved Oil Brands

A

2qt per 400hr

>2qt requires complete system flush

50
Q

Max Oil Consumption

A

0.2qt/hr over 10hr period

51
Q

Min Start Oil Temp

A

-33

52
Q

Single Point Refueling

A

Fueling: 10 to 50 PSI
Defueling: -10

53
Q

Approved Fuels

A

See Limitations

54
Q

FUEL BOOST Pumps - ON when…

A

LOW FUEL lights or >180+/-20

55
Q

Max Fuel Imbalance

A

Normal: 200
Emergency: 600

56
Q

Fuel Temperature Limitations

A

See Figure 2-7

57
Q

Vmo/Mmo

A

BELOW 8000: 262
8000-28907: 292
ABOVE 28907: 0.755

58
Q

Max Maneuvering Speed

A

Refer to Figure 2-9

59
Q

Vfe

A

0-15deg: 200

35deg: 173

60
Q

Vle

A

250

61
Q

Vlo

A

Extend: 250
Retract: 200

62
Q

Vsb

A

No Limit

63
Q

Vmca

A

86

64
Q

Vmcg

A

Flaps 7: 96

Flaps 15 92

65
Q

Vmcl

A

88

66
Q

Max Autopilot Operation

A

292/0.755

67
Q

Min Icing Speed - Sustained Flight

Except Takeoff, Approach, and Landing

A

160

68
Q

Max Takeoff and Landing Altitude

A

14,000

69
Q

Max Tailwind

A

10

70
Q

Max Takeoff and Landing Temperature

A

Refer to Figure 2-8

71
Q

Min Takeoff and Landing Temperature

A

-54C

72
Q

Max Water/Slush on Runway

A

0.5 inches

73
Q

Max Tire Ground Speed

A

165

74
Q

Nose Tire Inflation

A

125 +/-5

75
Q

Autopilot and yaw damper must be…

A

…OFF for takeoff and landing

76
Q

ENGINE SYNC must be…

A

…OFF for takeoff and landing

77
Q

VNAV must be…

A

off below 500AGL

78
Q

Takeoff and Landings are limited to…

A

…paved runway surfaces

79
Q

Takeoff with antiskid inoperative…

A

…is prohibited

80
Q

Nosewheel must be…

A

…in firm contact with ground prior to deploying thrust reversers

81
Q

Takeoff is prohibited with the following forms of contamination:

A

See Limitations (Clean Aircraft Concept)

82
Q

Visual and Tactile inspection required…

A

<10C or Fuel Temp <0C and

a. Visible moisture
b. Water present on wing upper surface
c. < 3C temp/dew point spread
d. Conditions conducive to frost formation

83
Q

WING/ENGINE Anti Ice - ON

A

<10C RAT and visible moisture

84
Q

TAIL DEICE switches ON

A

+10C to -35C at >150Kts

+10C to -40C at <150Kts

85
Q

Pitot/Static Heat Ground Operation Limit

A

2 min

86
Q

Anti-ice systems must not be used to…

A

…deice surfaces prior to takeoff.

87
Q

Max Operating Altitude

A

45,000

88
Q

Max Ambient Temperature

A

Refer to Figure 2-8

89
Q

Min Ambient Temperature

A

Refer to Figure 2-8

90
Q

Max Generator Load (Above Idle)

A

300 amp in Flight

91
Q

Max Generator Load (Idle)

A

225 amp in Flight

92
Q

Boundary Layer

A

16 per wing

All must be present for dispatch

93
Q

Min Flight Crew for All Operations

A

1 Pilot and 1 Copilot

94
Q

Load Factor Limits - In Flight

A

Flaps UP: -1.44 to =3.6G at 16,630
Flaps 7-35: 0.0 to =2.0G at 16,630
Limits bank angle and pull-up/push-over maneuvers

95
Q

Max Load Factor - Landing (Flaps 35)

A

+3.46 at 15,200

Limits sink rate to 600 fpm

96
Q

Cabin Pressure Limits

A

0.0 to 9.0 PSI

97
Q

Autopilot Min Altitudes

A

Enroute: 1000AGL
Non-Precision: 300AGL
ILS (CAT I): 180AGL

98
Q

Crew and Pax Oxygen Mask max approved altitude

A

40,000 cabin altitude

99
Q

Passenger Oxygen Mask prolonged operations

A

25,000

100
Q

Min Cabin Temp After Cold Soak

2hr at -10C or colder

A

0C for 15min prior to flight above FL250

Oxygen Mask Deployment

101
Q

Reverse thrust must be reduced to IDLE by…

A

60

102
Q

Max Reverse Thrust

A

=/>-18C: 71.4%

<18C: 68.3%

103
Q

Max Allowable Thrust Reverser Deployment Time

A

3min in any 10min period

104
Q

Engine static ground operation is limited to…

A

idle power if thrust reversers deployed

105
Q

Use of Thrust Reversers is prohibited…

A

…for Touch and Go Landings.

106
Q

Use of Thrust Reversers is prohibited…

A

…to back the airplane.

107
Q

Thrust Reversers must be checked prior to…

A
  1. …first flight of the day

2. …after any maintenance.

108
Q

Elevator trim system preflight test…

A

…must be accomplished prior to takeoff

109
Q

Ground Idle Switch must be in HIGH…

A

…when conducting touch and go landings

Citation Encore (N430AM) (2 decks)

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