Performance Flashcards

1
Q

What is the purpose of % MAC figure after W/B is completed?

A

To set pitch trim.

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2
Q

What is the zero fuel weight on the challenger 350 aircraft?

A

28,200lbs

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3
Q

What is the minimum flight wait on the challenger 350 aircraft?

A

24,800 lbs

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4
Q

What is the Vmcg speed for Flaps 10?

A

115 KIAS

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5
Q

Where is the anti-ice control panel located?

A

Centre pedestal

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6
Q

When should the anti-ice systems be turned on?

A

In contaminated surfaces, prior to flight into visible moisture and TAT of 10 C or less

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7
Q

When is the wing Anti-ice system not needed flight?

A

Speed above 210KIAS with the ICE DETECT message not illuminated

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8
Q

What is used for anti icing of the wing leading edge and engine intake cowls?

A

HP BLEED AIR

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9
Q

Is operation of APU during fluid deicing / anti icing allowed?

A

No

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10
Q

How many and how much time master lapse between APU start attempts?

A

One minute between first 3 starts. After third start 20 min cool down
Then max 2 more starts with one minute in between

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11
Q

What is the maximum operating altitude for the APU?

A

37,000 ft in air

14,000 ft on ground

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12
Q

What is the engine designation for the challenger 350 aircraft?

A

HTF 7350

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13
Q

HTF7350 is flat rated at______

A

7323 lbs of thrust up to ISA +15C

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14
Q

Automatic power reserve APR provides 7323 pounds of thrust up to_____

A

ISA +20C

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15
Q

At what maximum altitude does the engine start envelope begin?

A

30,000 ft

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16
Q

When does automatic APR activate?

A

APR switch to ON
Thrust Levers in T/O detente
And N2 differs by 15% or the engine FADECS lose communication with each other

17
Q

The permanent magnet alternator PMA supplies power to the FADEC at and above______

A

N2 45%

18
Q

From where does the FADEC obtain powered during startup and shutdown?

A

AIRCRAFT 28 VDC

19
Q

During a normal Engine start, when does the DC fuel pump supply fuel to the engine driven pump?

A

When the DC pump switch is in AUTO and

When the RUN switch is selected ON

20
Q

In-flight, when does the DC fuel pump come on automatically?

A

When the motive flow pressure is lost from the main ejector

21
Q

For how long can the engine be motored (cranked)?

A

5 min

22
Q

What is the cooling period After three consecutive engine start cycles?

A

15 min

23
Q

For takeoff, A fuel system inhibitor FSI I must be used when bulk fuel temperatures are below ______

A

-20C

Unless cold weather procedures are followed

24
Q

What are the Thrust Reverser limitations?

A
No backing up 
Idle only by 40 kts
Do not deploy in flight 
Do not deploy during a touch and go 
Only on paved surfaces
25
Q

At what bulk fuel temperature is takeoff prohibited?

A

50 C

26
Q

For JET A, at what bulk fuel temperature is takeoff prohibited?

A

-30 C

27
Q

APR power initiated by the AUTO system is it in limited to_____

A

10 min

28
Q

Normal takeoff power is limited to____

A

5 min

29
Q

What is the minimum oil temperature required to operate the engines above ground idle?

A

5 C

30
Q

At what oil temperature range me engines be operated from idle up to but not including CLB power?

A

5 to 14 C

31
Q

With air temperatures below -30°C, what is the minimum oil temperature limit for takeoff?

A

15 C provided an icing inhibitor is used and cold weather operations are followed

32
Q

With thrust levers in CRZ or CLB, the engines will sync to N1 or N2 when they are within____

A

5% of each other

33
Q

When will MACH HOLD adjust N1 within a plus or -3% of thrust lever position?

A

When engines are in sync
Autopilot is engaged
And level flight with ALT or ALTS

34
Q

Where is oil filter and cooled?

A

FHOC

FUEL HEATER AND OIL COOLER