GLEIM UNIT 3

A) RUNWAY HOLDING POSITION SIGN B) HOLDING POSITION SIGN FOR A RUNWAY APPROACH AREA C) HOLDING POSITION FOR ILS CRITICAL AREA D) SIGN PROHIBITING AIRCRAFT ENTRY INTO AN AREA E) TAXIWAY LOCATION SIGN F) RUNWAY LOCATION SIGN G) RUNWAY BOUNDARY SIGN H) ILS CRITICAL AREA BOUNDARY SIGN I) DIRECTION SIGN TERMINAL J) DIRECTION SIGN FOR COMMON TAXIING ROUTE TO RUNWAY K) DIRECTION SIGN FOR RUNWAY EXIT L) RUNWAY DISTANCE REMAINING SIGN M) HOLD SHOR-1 N) TAXIWAY ENDING SIGN.

A) HOLDING POSITION MARKINGS ATG BEGINNING OF TAKE OFF RUNWAY 19 B) ILS CRITICAL AREA BOUNDARY MARKING C) ROADWAY EDGE STRIPES D) RUNWAY HOLDING POSITION MARKING E) TAXIWAY HOLDING POSITION MARKER F) TAXIWAY BOUNDARY.

WHAT IS ONE PURPOSE OF WING FLAPS?.

ONE OF THE MAIN FUNCTIONS OF FLAPS DURING APPROACH AND LANDING IS TO:

WHAT IS THE PURPOSE OF THE RUDDER ON AN AIRPLANE?.

WHICH IS NOT A PRIMARY CONTROL FLIGHT CONTROL SURFACE?.

THE ELEVATOR CONTROLS MOVEMENT AROUND WHICH AXIS?.

WHICH STATEMENT IS TRUE CONCERNING PRIMARY FLIGHT CONTROLS?.

WHICH OF THE FOLLOWING IS TRUE CONCERNING FLAPS?.

WHICH DEVICE IS A SECONDARY FLIGHT CONTROL?.

TRIM SYSTEMS ARE DESIGNED TO DO WHAT?.

WHAT IS THE RELATIONSHIP OF LIFT, DRAG THRUST AND WEIGHT WHEN THE AIRPLANE IS IN STRAIGHT AND LEVEL FLIGHT?.

WHICH STATEMENT RELATES TO BERNOULLI'S PRINCIPLE.

THE TERM ANGLE OF ATTACK IS DEFINED AS THE ANGLE BETWEEN THE?.

THE ANGLE BETWEEN THE CHORD LINE OF AN AIRFOIL AND THE RELATIVE WIND IS KNOWN AS THE ANGLE OF?.

THE ANGLE OF ATTACK AT WHICH AN AIRPLANE WING STALLS WILL:

AS THE ALTITUDE INCREASES, THE INDICATED AIRSPEED AT WHICH A GIVEN AIRPLANE STALLS IN A PARTICULAR CONFIGURATION WILL?.

IN WHAT FLIGHT CONDITIONS MUST AN AIRCRAFT BE PLACED IN ORDER TO SPIN?.

DURING A SPIN TO THE LEFT, WHICH WING(S) IS/ARE STALLED?.

WHAT IS GROUND EFFECT?.

FLOATING CAUSED THE PHENOMENON OF GROUND EFFECT WILL BE MOST REALIZED DURING AN APPROACH TO LAND WHEN AT:

WHAT MUST A PILOT BE AWARE OF AS A RESULT OF GROUND EFFECT?.

AN AIRCRAFT LEAVING GROUND EFFECT DURING TAKE OFF WILL:

GROUND EFFECT IS MOST LIKELY TO RESULT IN WHICH PROBLEM?.

WHAT FORCE MAKES AN AIRPLANE TURN?.

WHAT DETERMINES THE LONGITUDINAL STABILITY OF AN AIRPLANE.

AN AIRPLANE SAID TO BE INHERENTLY STABLE WILL.

CHANGES TO THE CENTER OF PRESSURE OF A WING AFFECT THE AIRCRAFT'S:

AN AIRPLANE HAS BEEN LOADED IN SUCH A MANNER THAT THE CG IS LOCATED AFT OF THE AFT CG LIMIT. ONE UNDESIRABLE FLIGHT CHARACTERISTIC A PILOT MIGHT EXPERIENCE WITH THE AIRPLANE MIGHT BE:

WHAT CAUSES AN AIRPLANE (EXCEPT A T-TAIL) TO PITCH NOSE DOWN WHEN POWER IS REDUCED AND CONTROLS ARE NOT ADJUSTED?.

WHAT IS THE EFFECT OF ADVANCING THE THROTTLE IN FLIGHT?.

LOADING AN AIRPLANE TO THE MOST AFT CG WILL CAUSE THE AIRPLANE TO BE:

AN AIRPLANE LOADED WITH CENTER OF GRAVITY (CG) REAR OF THE AFT CG LIMIT COULD:

IN WHAT FLIGHT CONDITION ARE TORQUE EFFECTS MORE PRONOUNCED IN A SINGLE ENGINE AIRPLANE?.

THE LEFT TURNING TENDENCY OF AN AIRPLANE CAUSED BY P FACTOR IS THE RESULT OF THE:

WHEN DOES P FACTOR CAUSE THE AIRPLANE TO YAW TO THE LEFT?.

WHICH BASIC FLIGH MANEUVER INCREASES THE LAD FACTOR ON AN AIRPLANE AS COMPARED TO STRAIGHT AND LEVEL FLIGHT?.

THE AMOUNT OF EXCESS LOAD THAT CAN BE IMPOSED ON THE WING OF AN AIRPLANE DEPENDS UPON THE?.

DURING AN APPROACH TO A STALL, AN INCREASED LOAD FACTOR WILL CAUSE THE AIRCRAFT TO:

STRUCTURAL DAMAGE OR FAILURE IS MORE LIKELY TO OCCUR IN SMOOTH AIR AT SPEEDS ABOVE:

LIMIT LOAD FACTOR IS THE RATIO OF: