THATS A STALL YA'LL
STILL STALLIN'
NO SPIN ZONE
NOW THAT YOU SPUN
POT POURI
100

A STALL WILL ALWAYS OCCUR WHEN THE MAXIMUM LIFT, ALSO KNOWN AS____IS EXCEEDED.

WHAT IS THE CRITICAL ANGLE OF ATTACK? (CLmax)

100

REDUCE ANGLE OF ATTACK.

WHAT IS THE FIRST STEP IN STALL RECOVERY?

100

THESE ARE PROHIBITED FROM INTENTIONAL SPINS.

WHAT ARE SINGLE ENGINE NORMAL CATEGORY AIRPLANES?

100

MOVE THE THROTTLE TO IDLE.

WHAT IS THE FIRST STEP IN SPIN RECOVERY?

100

THE FORCE OF GRAVITY THAT ACTS VERTICALLY THROUGH THE CENTER OF GRAVITY OF THE AIRPLANE TOWARD THE CENTER OF THE EARTH.

WHAT IS WEIGHT?

200

THINGS THAT EFFECT STALL SPEED.

WHAT ARE WEIGHT,ENVIRONMENTAL CONDITIONS, TURBULENCE, FLAPS (HIGH LIFT DEVICES)?

200

MOST LIKELY TO OCCUR WHEN TRYING TO COMPENSATE FOR OVERSHOOTING A RUNWAY ON LANDING APPROACH.

WHAT IS A CROSS CONTROLLED STALL?

200

A PREREQUISITE FOR A SPIN.

WHAT IS A STALLED AIRCRAFT?

200

NEUTRALIZE THE AILERONS.

WHAT IS THE SECOND STEP IN SPIN RECOVERY?

200

SPLIT, FOWLER, PLAIN, AND SLOTTED

ARE ARE DIFFERENT TYPES OF TRAILING EDGE FLAPS?

300

FOUR TYPES OF STALLS.

WHAT ARE POWER ON, POWER OFF, ACCELERATED, AND CROSSC CONTROLLED STALLS?

300

IF YOU ARE NOT ALREADY AT MAXIMUM POWER, INCREASE THE THROTTLE TO MINIMZE ALTITUDE LOSS AND GAIN AIRSPEED.

WHAT IS THE SECOND STEP IN STALL RECOVERY "SMOOTHLY APPLY MAXIMUM POWER"?

300

INVERTED, FLAT, ERECT.

WHAT ARE TYPES OF SPINS?

300

DETERMINE DIRECTION OF ROTATION AND APPLY FULL OPPOSITE RUDDER.

WHAT ARE THE 3RD AND 4TH STEPS  IN THE SEQUENCE OF SPIN RECOVERY?

300

DETERMINED BY WHERE THE PROPELLER IS MOUNTED AND THE GENRAL DIRECTION IN WHICH THE THRUST ACTS.

WHAT IS THE THRUSTLINE?

400

MUSHY FEELING IN THE FLIGHT CONTROLS AND LESS CONTROL EFFECTIVENESS.

WHAT ARE THE FIRST INDICATIONS OF A STALL?

400

NORMALLY ENCOUNTERED DURING TAKEOFF, CLIMBOUT, AND GO AROUNDS.

WHAT ARE POWER ON STALLS?

400

TO RECOVER FROM A SPIN, YOU MUST BE FAMILIAR WITH THE RECOVERY PROCEDURES FOR YOUR AIRPLANE. THEY ARE FOUND IN THE _____

WHAT IS THE POH?

400

SMALL AIRCRAFT AUTHORIZED FOR SPINS WILL LOSE APROX. 500' OF ALTITUDE PER EACH 3 SECOND TURN AND RECOVER IN 1/4-1/2 OF A TURN.

WHAT IS THE GENERAL RULE OF THUMB FOR SMALL AIRCRAFT SPIN RECOVERY?

400

THIS SHAPE IS DESIGNED TO TAKE ADVANTAGE OF NEWTONS LAWS AND BERNOULLI'S PRINCIPLE.

WHAT IS WING SHAPE?

500

THIS IS NORMALLY CAUSED BY POOR STALL RECOVERY TECHNIQUE SUCH AS ATTEMPTING TO FLIGHT PRIOR TO ATTAINING SUFFICIENT FLYING SPEED.

WAHT IS A SECONDARY STALL?

500

ADJUST POWER AS REQUIRED, MAINTAIN COORDINATED FLIGHTWHILE ADJUSTING THE POWER TO A NORMAL LEVEL.

WHAT IS THE LAST STEP IN STALL RECOVERY?

500

AN UNCOORDINATED MANEUVER WITH THE WINGS UNEQUALLY STALLED.

WHAT IS A SPIN?

500

THAT PORTION OF A SPIN FROM THE TIME THE AIRPLANE STALLS AND ROTATION STARTS UNTIL THE SPIN IS FULLY DEVELPOPED.

WHAT IS THE INCIPIENT SPIN?

500

WHEN THIS DECREASES, THIS MUST BE INCREASED, TO CREATE THE SAME AMOUNT OF LIFT.

WHAT IS ANGLE OF ATTACK?