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CAE Ground School > K350 Flight Profiles And Maneuvers > Flashcards

K350 Flight Profiles And Maneuvers Flashcards

1
Q

When must you turn engine anti ice off for takeoff operations

A

When ambient temperature is above 10 degrees Celsius

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2
Q

How much nosewheel travel do rudder pedals provide

A

14 degrees left and 12 degrees right

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3
Q

What does braking and differential power increase steering authority too

A

48 degrees left or right for low speed taxi

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4
Q

What is N1 for ground operations and why

A

70% N1 on condition lever to avoid excessive ITT during ground ops at high temp, high elevation, high generator load

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5
Q

What RPM do engines spool up to and stabilize at before advancing engines to static torque

A

1700

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6
Q

What RPM is considered governing speed

A

1700 RPM

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7
Q

How long after brake release should you reach static torque

A

No later than Ten seconds

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8
Q

What is takeoff pitch attitude

A

10 degrees

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9
Q

What is air minimum control speed

A

Minimum flight speed at which plane is directionally controllable. This includes one engine out,auto-feather armed ,5 degree bank toward good engine , takeoff power on good engine , rudder boost on , gear up, flaps in takeoff, and most rearward CG

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10
Q

What is Vr (rotation speed)

A

Speed of rotation which ensures if engine fails at V1 plane should pass through 35 ft at V2

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11
Q

What is takeoff safety speed (V2)

A

Desired speed at 35 feet AGL if engine fails at V1

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12
Q

What is climb gradient that V2 gives you at takeoff

A

2% at 400 feet and 1.2% at 1500 feet

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13
Q

What is minimum V2 as compared to VMCA and VS1

A

V2 can’t be less than 1.1 times VMCA and 1.2 times VS1

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14
Q

What is all engine takeoff speed (V35)

A

Takeoff safety speed at 35 feet above ground level with both engines

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15
Q

What is minimum runway length required for departure

A

Longest of :

  1. Distance to accelerate and recognize engine failure at V1 , accelerate and rotate at Vr, then climb and accelerate to achieve V2 at 35 feet above runway
  2. Distance to accelerate and notice engine failure at V1 and stop
  3. All engine operating distance to accelerate to and rotate at Vr, then climb and accelerate IOT achieve V35 at 35 feet above runway increased by 15%
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16
Q

What are you checking prior to raising the gear

A

VSI and altimeter show positive rate of climb

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17
Q

What are you looking for prior to retracting the flaps

A

Airspeed increases to a minimum of VYSE

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18
Q

When should you set climb power

A

At 400 feet and clear of obstacles

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19
Q

What is altitude restriction for VFR operations over noise sensitive areas

A

2000 feet

20
Q

What speed should you climb at

A

170 knots indicated through 10k feet

21
Q

What should you do after setting climb power and when clear of airport traffic

A

Complete the climb checklist

22
Q

What should you do if you encounter a temperature inversion during the climb

A

Monitor climb torque and ITT to stay within limits

23
Q

What is max airspeed below 21k feet

A

263 knots indicated

24
Q

What is max airspeed from 21k to 35k feet

A

194 to 263 knots indicated and/or .58 Mach

25
Q

Maximum cruise ITT limit

A

820 degrees Celsius

26
Q

Transient ITT limit

A

850 degrees for no longer than 20 seconds

27
Q

Normal torque

A

100%

28
Q

Transient torque

A

102 % for seven minutes or 20 seconds where indication could reach 156 %

29
Q

What is speed for Severe turbulence

A

170 knots indicated with auto ignition on

30
Q

What can you do in severe turbulence to reduce yaw and roll oscillations

A

Ensure yaw damper is engaged

31
Q

What should you do if penetrating severe turbulence with autopilot on

A

Engage soft ride mode

32
Q

When should you activate surface de ice system

A

After observation of half to one inch of ice accumulation

33
Q

When must you use engine anti ice

A

All ground operations and while airborne in visible moisture when OAT is 5 degrees Celsius or colder

34
Q

What does rudder boost system do

A

Compensates for loss of engine power on one side . Make sure it is on prior to flight

35
Q

Main thing to know about yaw damper

A

Must be disengaged before touchdown

36
Q

What is speed for steep turns

A

180 knots indicated

37
Q

Minimum altitude for stall practice

A

5000 feet above terrain

38
Q

First two steps before beginning stall training

A

Clear cockpit of loose articles and clear practice area

39
Q

Power lever and prop setting to initiate stall

A

Power lever to 5% and propellers to maximum RPM

40
Q

Stall recovery procedure (clean/cruise configuration- flaps and gear up)

A
  1. Autopilot on
  2. Pitch reduce AOA and trim as necessary
  3. Bank level the wings
  4. Propellers high RPM full forward
  5. Throttles increase power to max allowable
  6. Recover to Vref
  7. Establish normal climb attitude
  8. Resume original flight path
  9. Don’t exceed limitations
41
Q

Setup for stall in takeoff/departure configuration (flaps approach and gear up)

A 
Level turn 15-30 degrees AOB 
Power levers 5% torque 
Propellers maximum RPM 
At 125 KIAS power to 50% and climb 
Airspeed should decrease 1 knot per second until stall
42
Q

What is airspeed , torque , props, gear, and flaps for terminal area

A

180 KIAS, 30% torque , 1500 RPM , gear up , flaps up

43
Q

What is airspeed , torque , props, gear, and flaps for 3 degree glide slope ( ILS RNAV to DA)

A

130 KIAS, 25% torque , 1700 RPM , gear down , flaps approach

44
Q

What is airspeed , torque , props, gear, and flaps for descent to MDA at approximately 900 FPM

A

130 KIAS, 15% torque , 1700 RPM , gear down, flaps approach

45
Q

What is airspeed , torque , props, gear, and flaps for level flight configured (circle to land / MDA)

A

130 KIAS, 43% torque , 1700 RPM , gear down, flaps approach

46
Q

What is airspeed , torque , props, gear, and flaps for steep turns

A

180 KIAS, 43% torque , 1500 RPM , gear up, flaps up

CAE Ground School (5 decks)

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