STALL PREVENTION & RECOVERY TRAINING

Question 1

EXCEED THE CRITICAL ANGLE OF ATTACK & THE SURFACE WILL STALL, AND

LIFT WILL DECREASE INSTEAD OF INCREASING

Answer 1

REGARDLESS OF THE AIRPLANE SPEED OR ATTITUDE

Question 2

WHICH OF THE FOLLOWING STATEMENTS IS TRUE

Answer 2

RECOVERY FROM APPROACH TO STALL WARNING IS THE SAME AS

RECOVERY FROM A STALL

Question 3

THE AIRPLANE ANGLE OF ATTACK IS THE ANGLE BETWEEN

WING CORD AND ONCOMING AIR OR RELATIVE WIND

Answer 3

TRUE

Question 4

AIRPLANE STALL SPEEDS ARE PUBLISHED IN APPROVED FLIGHT MANUAL

FOR EACH AIRPLANE MODEL. THEREFORE SPEEDS ARE PRESENTED AS A

FUNCTION OF AIRCRAFT WEIGHT.

THEREFORE, IF A PILOT MAINTAINS AIRSPEED ABOVE THE APPROPRIATE

LISTED AIRCRAFT WEIGHT, THE AIRCRAFT WILL NOT STALL

Answer 4

FALSE

Question 5

STALL SPEED OF AN AIRPLANE IS:

Answer 5

AFFECTED BY WEIGHT AND BANK ANGLE

Question 6

LARGE DOWNWARD AILERON DEFLECTIONS:

Answer 6

COULD INDUCE AIR SEPARATION OVER THAT PORTION OF THE WING

AT VERY HIGH ANGLES OF ATTACK

Question 7

STALL RECOVERY TEMPLATE IN CORRECT ORDER

DNAARR

Answer 7

DISCONNECT AUTOPILOT, AUTO-THROTTLE & AUTO-THRUST

NOSE DOWN PITCH CONTROL UNTIL IMPENDING STALL INDICATIONS ELIMINATED

ADJUST BANK ANGLE TO WINGS LEVEL

APPLY THRUST AS NEEDED

RETRACT SPEED BRAKES & SPOILERS

RETURN TO DESIRED FLIGHT PATH