Section 2 Flashcards

1
Q

Main Gear Strut Extension

A

4 to 4 3/4 Inches (4 3/8 +- 3/8)

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2
Q

Nose Gear Strut Extension

A

5 3/4 to 6 1/8 Inches

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3
Q

Oxygen Hose Disconnection Tension

A

12 - 20lbs

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4
Q

When Battery is Less Than ___ Volts, EED Defaults to Max Day Mode Brightness

A

22 Volts

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5
Q

Ignition Should Occur Before ___ Fuel Flow

A

360lbs/hr

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6
Q

If Ignition Does Not Occur Wait How Long Before Attempting Second Start

A

2 Minutes with Air

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7
Q

EGT Should Rise Within __ Seconds of Fuel Flow, If Not Abort Start

A

12 Seconds

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8
Q

With Normal Movement, Hydraulic Pressure Should Not Drop Below ___ PSI

A

1500 PSI

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9
Q

MDP Must be On For ___ Seconds Before Testing Lights

A

45 Seconds

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10
Q

Oxygen Quantity Light Illuminates at ___ Liters

A

1 Liter

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11
Q

Nosewheel Tires are Severly Damaged When Max Deflection Turns are Attempted in Excess of ___ kts

A

10kts

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12
Q

Main Nosewheel is Rated to ___kts But Has Been Tested Up to ___% of That

A

174 and 120%

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13
Q

Delay ___ Minutes for Large Aircraft and ___ Minutes for Heavy Aircraft

A

2 Minutes/4 Minutes

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14
Q

Wake Turbulence Time Limits May be Reduced if Crosswind Is More Than ___ kts

A

5kts

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15
Q

Abort Takeoff if AB Fails to Light After ___ Seconds

A

5 Seconds

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16
Q

Nosewheel Should Lift Off Runway at ___kts and The Aircraft Should Lift Off at ___kts

A

150kts and 165kts

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17
Q

Aerobraking Until Loss of Elevator Authority, Then Applying Brakes Increases Chart Landing Distance By ___ %

A

50%

18
Q

Extreme Caution Must be Used When Apply Wheel Brakes Above ___kts

A

120kts

19
Q

Use Caution When Braking at Speeds Above ___kts

A

100kts

20
Q

Aerobraking Using Full Back Stick Will Cause a Hard Nosewheel Impact at ___kts

A

100kts

21
Q

Closed Pattern Requires ___lbs of Fuel

A

150lbs

22
Q

Main Wheel Touchdown Should Occur at ___kts Below Final Approach Airspeed

A

25kts

23
Q

Minimize Landing Roll by Decreasing Final Approach Airspeed ___kts

A

10kts

24
Q

Charts Figure a Landing Attitude of ___ Degrees Nose High, Then Optimum Braking

A

12 Degrees

25
Q

Land on Upwind Side of Runway if Crosswind Exceeds ___kts

A

15kts

26
Q

Do Not Aerobrake if Crosswind Exceeds ___kts

A

15kts

27
Q

Landing Distance Without Aerobraking May be Increased ___ %

A

50%

28
Q

Chances for Optimum Braking are Greatly Increased Below ___kts

A

100kts

29
Q

Operate Engines Below ___% RPM For ___ Minutes Prior to Shutting Down

A

70%/ 1 Minute

30
Q

Landing/Taxi Light Requires ___ Seconds to Retract Prior to Engine Shutdown

A

10 Seconds

31
Q

Ram Dump Door May Require ___ Seconds to Close Prior to Engine Shutdown

A

10 Seconds

32
Q

Instrument Climb Minimum of ___fpm

A

1,000fpm

33
Q

Power Settings Between ___ and ___ Will Provide Comfortable Climb Rates For Intermediate Level-Offs

A

90% and 95%

34
Q

Maintain ___ Pitch Attitude For MAX Thrust Climb Once Reaching Desired Mach

A

20-25 Degrees

35
Q

Holding Airspeeds

A

250 - 265kts

36
Q

SE Holding at ___ ft or Above With More Than ___lbs of Fuel is Impossible

A

20,000ft and 1800lbs

37
Q

Recommended RPM For Anti-Ice Operation

A

80% RPM

38
Q

Circling Approach Minimum Airspeed and Configuration Prior to Final

A

180kts + Fuel and 60% Flaps

39
Q

Straight-In Approach Minimum Airspeed

A

160kts + Fuel

40
Q

Base Leg Minimum Airspeed

A

180kts + Fuel

41
Q

Radar Pattern Requires ___lbs of Fuel

A

400 lbs