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Citation Excel > CE-560XL > Flashcards

CE-560XL Flashcards

1
Q

Aircraft Length?

A

51.8 feet

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2
Q

Aircraft Wing Span?

A

55.7 feet

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3
Q

Aircraft Tail Height?

A

17.2 feet

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4
Q

Wheelbase?

A

21.9 feet

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5
Q

Maximum Ramp Weight?

A

20,200 pounds

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6
Q

Maximum Takeoff Weight?

A

20,000 pounds

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7
Q

Maximum Landing Weight?

A

18,700 pounds

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8
Q

Maximum Zero Fuel Weight?

A

15,000 pounds

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9
Q

Minimum Flight Weight?

A

12,400 pounds

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10
Q

Maximum Tailcone Baggage Weight?

A

700 pounds

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11
Q

Maximum Aft Cabin Weight?

A

600 pounds (limit of 120 lbs/sq ft)

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12
Q

Maximum Airspeed (Vmo) 0 to 8000 feet?

A

260 KIAS

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13
Q

Maximum Airspeed (Vmo) 8000 to 26,515 feet?

A

305 KIAS

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14
Q

Maximum Airspeed (Vmo) 26,515 to 45,000 feet?

A

.75 Mach Indicated

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15
Q

Minimum Control Speed, Ground (Vmcg)?

A

81 KIAS

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16
Q

Minimum Control Speed, Air (Vmca)?

A

90 KIAS

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17
Q

Maximum Speed Brake Operation Speed (Vsb)?

A

No Limit

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18
Q

Maximum Flap Extended Speed (Vfe) 7° or 15° ?

A

200 KIAS

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19
Q

Maximum Flap Extended Speed (Vfe) 35° ?

A

175 KIAS

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20
Q

Maximum Landing Gear Extended Speed (Vlo)?

A

250 KIAS

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21
Q

Maximum Landing Gear Retraction Speed (Vlr)?

A

200 KIAS

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22
Q

Maximum Landing Gear Extending Speed (Vle)?

A

250 KIAS

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23
Q

Maximum Operating Altitude?

A

45,000 feet

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24
Q

Maximum Operating Altitude with 1 to 3 Vortex Generators Missing?

A

41,000 feet

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25
Q

Maximum Altitude for Takeoff and Landing?

A

14,000 feet

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26
Q

Maximum Operating Temperature?

A

ISA +39° C

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27
Q

Minimum Operating Temperature?

A

-54° C

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28
Q

Maximum Demonstrated Cross Wind?

A

24 knots

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29
Q

Maximum Tailwind for Takeoff and Landing?

A

10 knots

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30
Q

Minimum Speed in Icing?

A

160 knots

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31
Q

Maximum Recommended Turbulence Airspeed?

A

180 knots

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32
Q

Maximum Tire Speed?

A

165 knots

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33
Q

What is the Tire Pressure for the Main Landing Gear Tires?

A

218 +2/-5 psi (loaded)

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34
Q

What is the Tire Pressure for the Nose Gear Tire?

A

135 +5/-5 psi (loaded)

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35
Q

What is the Engine Manufacturer and Model?

A

Pratt and Whitney PW-545A Turbofan Engines

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36
Q

What is the Engines Thrust Output at Sea Level (each)?

A

3804 pounds

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37
Q

What are the Engines Maximum ITT at Takeoff?

A

720° C

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38
Q

What is the Engines Maximum ITT on Start?

A

720° C

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39
Q

What is the Engines Maximum Continuous ITT?

A

720°C

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40
Q

What is the Engines Maximum ITT in Transient?

A

760° C

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41
Q

Maximum Altitude to Start the APU?

A

20,000 feet

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42
Q

Maximum Altitude to Operate the APU?

A

30,000 feet

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43
Q

Maximum Generator Load of the APU?

A

200 Amps (230 Amps Transient)

44
Q

What is the Maximum Fuel Capacity?

A

6790 pounds (1006 gallons)

45
Q

What is the Maximum Fuel Capacity Per Tank?

A

3395 pounds (503 gallons)

46
Q

What is the Maximum Normal Operations Fuel Imbalance?

A

400 pounds

47
Q

What is the Maximum Emergency Operations Fuel Imbalance?

A

800 pounds

48
Q

How many Fuel Drain Valves are in each Wing?

A

5

49
Q

What are the approved fuels for use in the aircraft?

A

Jet A, Jet-A1, Jet 3, JP-5 and JP-8.

Consult the AFM for use of Jet B and JP-4

50
Q

Is Anti-Ice additive approved for use in the fuel?

A

Yes, but it’s not required.

51
Q

What components uses Hydraulic Pressure to operate?

A

Landing Gear, Flaps, Speedbrakes, Two-Position Stabilizer and Thrust Reversers.

52
Q

What are the only approved hydraulic fluids?

A

Skydrol (Solutia,Inc.) and Hyjet (Exxon/Mobile)

53
Q

What is the Maximum Oil Consumption per Engine?

A

1 quart per 10 hour period.

54
Q

23 PSI Service Air is used to provide pressurized air for?

A

Elevator De-Ice Boots
Primary Cabin Door Seal
Outflow Valve Control
Throttle Detents

55
Q

Name the Emergency Equipment in the Cockpit?

A 
Fire Extinguisher 
Oxygen Mask
Life Vests 
Smoke Goggles 
Flashlights
56
Q

Name the Emergency Equipment in the Cabin?

A 
Fire Extinguisher 
Oxygen Masks 
Life Vests 
First Aid Kit
Water Barrier
57
Q

What are the power requirements for a Ground Power Unit (GPU) ?

A

28 VDC

800 to 1000 Amps

58
Q

Describe the Main Aircraft Battery?

A

24 volt, 44 amp/hour, Lead Acid or NiCad Battery.

59
Q

How long can the Main Aircraft Battery supply power in an emergency?

A

Up to 30-minutes for components on the Emergency Battery Bus.

60
Q

What is the 1 Engine Service Ceiling at Maximum Takeoff Weight?

A

28,600 feet

61
Q

What is the Cabin Height?

A

5 feet 8 inches

62
Q

What is the Cabin Width?

A

5 feet 7 inches

63
Q

What is the Recommended Maximum Rate of Climb Speed?

A

230 knots to 25,000 feet

64
Q

What is the Recommended Cruise Climb Speed?

A

250 knots to 25,000 feet

65
Q

What is the Minimum Enroute Altitude to use the Autopilot?

A

1000 feet agl

66
Q

What is the Minimum Altitude to use the Autopilot on a Precision Approach?

A

180 feet agl

67
Q

What is the Minimum Altitude to use the Autopilot on a Non-precision Approach?

A

300 feet agl

68
Q

What is the Maximum Air Speed to use the Autopilot?

A

Vmo/Mmo

69
Q

Autopilot Limitations?

A

Must be OFF for takeoff and landing.

One pilot must be at his/her station with seatbelt on while using the autopilot.

70
Q

What is the Maximum Cabin Differential PSI ?

A

9.7 psid

71
Q

The Thrust Reversers must be reduced to Idle Power by what groundspeed?

A

60 KIAS

72
Q

What is the Maximum Deployed Time of the Thrust Reversers?

A

3 minutes in any 10 minute period. (30 seconds with the APU running)

73
Q

Minimum Temperature to use the Tail De-Ice System below 150 KIAS?

A

-40° C (-40° F)

74
Q

Minimum Temperature to use the Tail De-Ice System at or Above 150 KIAS?

A

-35° C (-31° F)

75
Q

What items are on the Live Battery Bus (available whenever the battery or GCU are connected) ?

A

Entry Way lights, Cabin Lights, Baggage Compartment Lights, Tailcone Compartment Light

External Lavatory Service

APU Oil Check Light

76
Q

ENGINE FAILURE OR ANY OTHER EMERGENCY DURING TAKEOFF?

A

SPEED BELOW V1:
1. TAKEOFF……..ABORT

SPEED AT OR ABOVE V1:

  1. CLIMB TO A SAFE ALTITUDE
  2. WING XFLOW (if wing anti-ice is ON)…….ON
77
Q

LH OR RH ENGINE FIRE (ENGINE FIRE WARNING)?

A
  1. THROTTLE (affected engine)……..IDLE
    * IF SWITCH LIGHT REMAINS ILLUMINATED
  2. ENGINE FIRE SWITCHLIGHT (affected side)…..LIFT COVER and PUSH
  3. EITHER ILLUMINATED BOTTLE ARMED SWITCHLIGHT…..PUSH
78
Q

EMERGENCY RESTART - TWO ENGINES?

A
  1. IGNITION SWITCHES……..BOTH ON
  2. FUEL BOOST PUMP SWITCHES…….BOTH ON
  3. THROTTLES……..IDLE
79
Q

EMERGENCY EVACUATION?

A
  1. PARK BRAKE……..SET
  2. THROTTLES………BOTH CUT OFF
  3. LH ENGINE FIRE SWITCHES……..PRESS
  4. LH BOTTLE ARMED SWITCHLIGHTS……PRESS (if fire suspected)
  5. RH ENGINE FIRE SWITCHES……..PRESS
  6. RH BOTTLE ARMED SWITCHLIGHTS……PRESS (if fire suspected)
  7. APU MASTER SWITCH……..OFF
  8. BATT SWITCH………OFF
80
Q

APU FIRE (FIRE WARNING ILLUMINATED)?

A

APU FIRE WARNING SWITCH……..LIFT cover and PUSH

81
Q

ELECTRICAL FIRE OR SMOKE?

A
  1. OXYGEN MASKS……..DON and EMER

2. MICROPHONE SWITCHES……..MIC OXY MASK

82
Q

BATT O’ TEMP (BATTERY OVERTEMPERATURE)?

A
  1. AMPERAGE……..NOTE
  2. BATT SWITCH……..EMER
  3. AMPERAGE……..NOTE DECREASE
83
Q

CAB ALT (CABIN DECOMPRESSION)?

A
  1. OXYGEN MASKS……..DON and 100% OXYGEN
  2. MICROPHONE SWITCHES……..MIC OXY MASK
  3. EMERGENCY DESCENT……..AS REQUIRED
84
Q

ELECTRIC ELEVATOR RUNAWAY TRIP?

A

AP TRIM DISC BUTTON……..PRESS and RELEASE

85
Q

EMERGENCY DESCENT?

A
  1. AP TRIM DISC BUTTON……..PRESS and RELEASE
  2. IGNITION SWITCHES……..ON
  3. THROTTLES……..IDLE
  4. SPEED BRAKES……..EXTEND
  5. AIRPLANE PITCH ATTITUDE……INITIALLY TARGET 20° NOSE DOWN
86
Q

ENVIRONMENTAL SYSTEM SMOKE OR ODOR?

A
  1. OXYGEM MASKS……..DON and EMER

2. MICROPHONE SWITCHES……..MIC OXY MASK

87
Q

SMOKE REMOVAL?

A
  1. OXYGEM MASKS……..DON and EMER

2. MICROPHONE SWITCHES……..MIC OXY MASK

88
Q

THRUST REVERSER INADVERTENT DEPLOYMENT DURING TAKEOFF?

A

SPEED BELOW V1:
1. TAKEOFF……..ABORT

SPEED AT OR ABOVE V1:

  1. EMERGENCY STOW SWITCH (affected engine)……..EMER
  2. THROTTLE (affected engine)……..CHECK IDLE
  3. CLIMB TO A SAFE ALTITUDE
89
Q

THRUST REVERSER INADVERTENT IN-FLIGHT DEPLOYMENT?

A
  1. CONTROL WHEEL AP/TRIM DISC BUTTON……..GRIP/PRESS AND RELEASE
  2. EMERGENCY STOW SWITCH (affected engine)……..EMER
  3. THROTTLE (affected engine)……..CHECK IDLE
  4. AIRSPEED……..REDUCE TO 140 KIAS OR LESS
90
Q

THRUST REVERSER UNLOCK ANNUNCIATOR ILLUMINATED IN-FLIGHT?

A
  1. EMERGENCY STOW SWITCH (affected engine)……..EMER

2. THRUST REVERSER LEVERS……..CHECK THRUST REVERSER AT STOWED (FULL FORWARD) POSITION

91
Q

WHEEL BRAKE FAILURE?

A
  1. BRAKE PEDALS REMOVE FEET FROM BRAKE PEDALS

2. EMER BRAKE HANDLE PULL as required

92
Q

AUTOPILOT MALFUNCTION?

A

AP/TRIM DISC BUTTON……..PRESS and RELEASE

93
Q

INADVERTENT STALL (BUFFET/ROLL-OFF)?

A
  1. AP/TRIM DISC BUTTON……..PRESS and RELEASE
  2. PITCH ATTITUDE……..REDUCE
  3. ROLL ATTITUDE……..LEVEL
  4. THROTTLES……..MAXIMUM THRUST
94
Q

Engine Anti-Ice Must Be ON a Minimum of ____ Seconds Out of Every ____ Minutes?

A

15

4

95
Q

What Items does the Right Squat Switch Control?

A

Stick Shaker and Test
Thrust Reversers
Anti-Skid

96
Q

What Items does the Left Squat Switch Control?

A 
Ground Idle
Radar Forced Standby 
Cabin Outflow Valves
EMER Press Valve (Inop on the ground)
Cross-Generator a Start Disabled in Flight
Hour Meter and Digital Clocks
Landing Gear Handle Solenoid and Anti-Skid
Stick Shaker and Test
Thrust Reversers
97
Q

With the PASS OXY Control Switch in the AUTO Position the Passenger Oxygen Mask will Automatically drop when the Cabin Altitude exceeds?

A

14,500 +/- 500 ft.

98
Q

Activation of the Emergency Dump Switch will cause the cabin altitude to rise quickly to a maximum of?

A

14,500 ft.

99
Q

High Altitude Airport Mode is automatically selected when a landing field elevation above ________ feet MSL is set into the Cabin Pressurization Controller?

A

8000

100
Q

Normal Oil Pressure range at N2 speeds above 60% ?

A

45 to 140 PSI

101
Q

Oil Pressure at takeoff and maximum thrust may exceed 140 PSI up to ____ seconds?

A

120

102
Q

Oil Temperature range?

A

-40 to 121.1° C

103
Q

What is the minimum oil temperature for starting?

A

-40° C

104
Q

What is the maximum EGT for the APU?

A

690° C

105
Q

A Speed-Sensing Switch prohibits the Stabilizer from moving at air speeds above approximately?

A

215 KIAS

106
Q

Nose-Wheel steering with the Rudder Pedals produces a maximum ______° deflection either side of center?

A

20°

107
Q

Low bank angle is limited to ____° ?

A

14°

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