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Citation Latitude > General > Flashcards

General Flashcards

1
Q

Pilot aborts starts for:

A

1) No Oil Pressure within 20 seconds of ITT rise.
2) No N1 by 40% N2.
3) No stable GRD idle within 90 seconds of ITT rise.

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2
Q

FADEC aborts starts for:

A

1) Insufficient ITT rise within 20 seconds after fuel flow.
2) ITT limit exceeded.

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3
Q

TRU max current Limit?

A

100 Amps.

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4
Q

Minimum battery temperature for APU Start?

A

-20C

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5
Q

Minimum battery temperature for engine start?

A

-10C

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6
Q

Flap setting for anti-ice Type 2, 3, or 4.

A

Flaps 1.

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7
Q

Tail height.

A

21 feet.

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8
Q

Aircraft width?

A

73 feet.

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9
Q

Aircraft length?

A

63 feet.

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10
Q

Monitored doors?

A

1) L and R Nose.
2) Passenger door.
3) Emergency exit door.
4) Baggage door.
5) Tail come access door.
6) Lav doors.

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11
Q

Which electrical bus is the Cabin Door on?

A

Left Battery.

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12
Q

Cabin entry door holds at closed for how many seconds?

A

10 seconds, +- 2.

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13
Q

Cabin entry door “Pressure Warning” LED light means what?

A

Cabin is pressurized.

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14
Q

Baggage compartment heated? Pressurized?

A

No. No.

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15
Q

Battery type and amps?

A

44 amp/hr Ni-CAD.

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16
Q

Engine Generator Amps?

A

300 Amps, Above FL350 275 Amps.

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17
Q

APU Amps?

A

275 Amps.

18
Q

Fuel boost pumps turns on for:

A

SLAC

1) Starting engines.
2) Low Pressure sensed.
3) APU running without R engine running.
4) Crossfeed operation.

19
Q

Accessory Gearbox driven systems.

A

SOAPFH

1) Starter/Generator.
2) Oil Pump.
3) Alternator.
4) PMA (Permanent Magnet Alternator)
5) Fuel Pump.
6) Hydraulic Pump.

20
Q

Latitude Engines.

A

PW306D1, 5907 pounds of thrust.

21
Q

Service Air:

A

*Available anytime Bleed-Air source in on.

1) Cabin Recirculation Valve.
2) Enables ACM (Air Cycle Machine) low temp limit valve.

22
Q

PITOT/STATIC Heat:

A

1) Pitot
2) Static
3) Angle of Attack.

23
Q

ENG/STAB heat:

A

HIRES

1) Horizontal Stabilizer.
2) Inboard wing, (1/3).
3) RAT probes.
4) Engine Inlets.
5) Stator Vanes.

24
Q

What is powered by the hydraulic system:

A

BLTSSN

1) Brakes.
2) Landing Gear.
3) Thrust Reversers.
4) Speed Brakes.
5) Spoilers.
6) Nose wheel steering.

25
Q

Bootstrap Accumulator ensures:

A

Hydraulic pump lubrication during engine start.

26
Q

Elevator trim tabs:

A

1) Aerodynamically fairs elevator in position with the stabilizer.
2) Above Mach 0.77 helps prevent Mach tuck.

27
Q

What is a RED CAS message and it’s indicators?

A

Warning message:

  • Flashing Master Warning Light.
  • Audio Alert: Aural or (2) Chimes.
  • CAS message remains until resolved.
28
Q

What is a AMBER CAS message and it’s indicators?

A

Caution message:

  • Master Caution light.
  • (1) Chime.
  • CAS message remains until resolved.
29
Q

What is a WHITE CAS message and it’s indicators?

A

Advisory message.
- CAS message flashes for 5 seconds, then steady.

30
Q

Engine Ground Idle?

A

57% N2.

31
Q

Engine Flight Idle?

A

65% N2.

32
Q

CDFA Requirements:

A

Continuous Descent Final Approach:

VAST (Vertical decent, Altimeter, Straight, Temp)

  • Straight in Approach Minimums.
  • Published descent angle.
  • Cold correction if needed.
  • Local altimeter setting.
33
Q

Emergency Descent Mode Requirements:

A
  • Aircraft Above 30,000 Feet.
  • Autopilot Engaged.
  • Cabin Altitude exceeds 14,500 feet.
34
Q

Flight Abort Mode Requirements:

A
  • Descent is initiated.
  • Flight never reaches 6000 feet above takeoff field elevation.
  • Flight time less than 10 minutes.
35
Q

TOGA button actions when pressed:

A
  • Cancels Autopilot.
  • Flight Director rolls wings level.
  • Flight Director pitches for 7.5 degrees in the air, 10.0 degrees on the ground.
  • Sequences the FMS for missed Approach.
36
Q

Generator cooling requirements:

A

Engine Idle with Generator load of <75 amps for 4 minutes prior to shutdown or wait 35 minutes after shutdown to start.

37
Q

Oxygen bottle size and location:

A

77 cubic feet, left nose compartment.

38
Q

Minimum Flap Maneuvering Speed

A

UP - 150 kts
1 - 145 kts
2 - 140 kts
FULL - VREF+10

39
Q

RVSM Requirements

A

1 Autopilot
1 Altitude Alerting Device
1 ATC Altitude Reporting Transponder
2 Air Data Computers
2 Pitot Probe Heaters linked to ADC in use
160 kt Minimum Airspeed in RVSM Airspace

40
Q

Zero Fuel Weight

A

21,430 pounds

Citation Latitude (24 decks)

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