Landing Emergencies Flashcards
During an EGPWS warning, (PULL UP!) do not change ___ or ___ until the plane is out of the warning condition and stabilized
Flaps or gear configuration
Adequate rudder is available to maintain directional control during patter, approach and landing if what 3 conditions for directional control are satisfied?
Speed, thrust setting and control inputs
For 3 engine operation, if the charted go-around N1 setting for the asymmetric/outboard engine is not exceeded, Vmca will be ____ than touchdown speed
Less than or equal to
At high gross weights consider flying a ___ final approach
Extended
To minimize trim changes with thrust adjustments use ____ to the max extent possible
Symmetric throttles
in a 3 engine approach, if the decision is made to go around advance __ engines to ____ then ___ if needed
Symmetric, charged go-around setting, asymmetric not to exceed max asymmetric thrust setting
If landing with one engine and powered rudder inoperative fly downwind and base legs with ___ flaps at minimum at a speed of ___
20 degrees, Vref+30
Remove __ trim prior to landing
Rudder
Time permitting, a gross weight that achieves a climb gradient of ___ % or greater is recommended
28%
Avoid excessive sideslip by maximum use of ___
Rudder
If landing with 2 engines out on the same side, once airspeed is below ____ go-around capability cannot be assured.
Approach speed
With 2 engines and powered rudder inoperative, ____ should be primary consideration of landing base with ___ conditions preferred
Weather conditions, VMC
With 2 engines and powered rudder inoperative, reduce gross weight to ____. Don’t lower flaps beyond ____
Minimum practical, 20 degrees
If full rudder will be required, ensure seat is ___
Full vertical
For two engine operation, if thrust setting doesn’t exceed charted go-around N1, Vmca should be ___ to approach speed
Less than or equal to