Section 2 Flashcards
Main Gear Strut Extension
4 to 4 3/4 Inches (4 3/8 +- 3/8)
Nose Gear Strut Extension
5 3/4 to 6 1/8 Inches
Oxygen Hose Disconnection Tension
12 - 20lbs
When Battery is Less Than ___ Volts, EED Defaults to Max Day Mode Brightness
22 Volts
Ignition Should Occur Before ___ Fuel Flow
360lbs/hr
If Ignition Does Not Occur Wait How Long Before Attempting Second Start
2 Minutes with Air
EGT Should Rise Within __ Seconds of Fuel Flow, If Not Abort Start
12 Seconds
With Normal Movement, Hydraulic Pressure Should Not Drop Below ___ PSI
1500 PSI
MDP Must be On For ___ Seconds Before Testing Lights
45 Seconds
The EED fuel flow should show no higher than _____
60 lbs per hour, could indicate EED failure/ fuel transmitter if higher
Oxygen Quantity Light Illuminates at ___ Liters
1 Liter
Nosewheel Tires are Severly Damaged When Max Deflection Turns are Attempted in Excess of ___ kts
10kts
Main Nosewheel is Rated to ___kts But Has Been Tested Up to ___% of That
174 and 120%
Delay ___ Minutes for Large Aircraft and ___ Minutes for Heavy Aircraft
2 Minutes/4 Minutes
Wake Turbulence Time Limits May be Reduced if Crosswind Is More Than ___ kt
5 KTS
Abort Takeoff if AB Fails to Light After ___ Seconds
5 Seconds
Nosewheel Should Lift Off Runway at ___kts and The Aircraft Should Lift Off at ___kts
150kts and 165kts
Aerobraking Until Loss of Elevator Authority, Then Applying Brakes Increases Chart Landing Distance By ___ %
50%
Extreme Caution Must be Used When Apply Wheel Brakes Above ___kts
120kts
If external power isn’t accepted and power unit checks good do what
Cycle battery switch