Becoming Remote Pilot Flashcards

(61 cards)

1
Q

Stay BELOW

A

400 FT

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2
Q

WHAT AUTHORIZATION MUST YOU HAVE IN “CONTROLLED” AIRSPACE?

A

ATC AUTHORIZATION

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3
Q

VLOS

A

VUSUAL LINE OF SIGHT (MUST BE MAINTAINED)

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4
Q

REMAIN CLEAR OF

A

MANNED AIRCRAFTS

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5
Q

AVOID:

A

TRAFFIC PATTERNS
APPROACHES
RUNWAYS
TAXIWAYS

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6
Q

HOW MANY MILES OF VISIBILTY ARE REQUIRED?

A

3 TO FLY UNDER PART 107

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6
Q

HOW MANY MILES OF VISIBILTY ARE REQUIRED?

A

3 TO FLY UNDER PART 107

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7
Q

VFR

A

VISUAL FLIGHT RULES

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8
Q

IFR

A

INSTRUMENT FLIGHT RULES

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9
Q

VFR CONDITIONS

A

VMC VISUAL METEORLOGICAL CONDITIONS

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10
Q

IMC CONDITIONS

A

INSTRUMENT METEORLOGICAL CONDITIONS

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11
Q

AGL

A

ABOVE GROUND LEVEL

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12
Q

MSL

A

MEAN SEAL LEVEL

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13
Q

ALTITIUDE CLASSIFICATIONS

A

AGL & MSL

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14
Q

LIFT FACTOR

A

PULLS AIRCRAFT UP

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15
Q

WEIGHT FACTOR

A

PULLS AIRCRAFT DOWN

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16
Q

VECTOR

A

A FORCE IN A DIRECTION

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17
Q

THRUST

A

FORWARD PULLING FORCE CREATED BY PROPELLOR

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18
Q

DRAG

A

FORCE THAT TRIES TO HOLD AIRCRAFT BACK

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19
Q

2 TYPES OF DRAG

A

PARASITE & INDUCED

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20
Q

FOUR FORCES OF FLIGHT

A

LIFT, THRUST, WEIGHT, DRAG

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21
Q

LIFT EQUALS ____ THRUST EQUALS ____ IN ___________ FLIGHT

A

WEIGHT, DRAG, UNACCELERATED

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22
Q

THREE AXES OF CONTROL

A

LONGITUDINAL AXIS, LATERAL AXIS, VERTICAL AXIS

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23
Q

LONGITUDINAL AXIS MOTION ____

ROLL ______

A

ROLL, AILERONS

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24
LATERAL AXIS MOTION ____ | CONTROL _____
PITCH, ELEVATOR (OR STABILATOR)
25
VERTICAL AXIS rotational MOTION_____ | CONTROL _____
YAW, RUDDER
26
AIRFOIL
AN OBJECT THAT PRODUCES AN AERODYNAMIC FORCE WHEN MOVED THROUGH A FLUID
27
AIRFOIL IS USED TO PRODUCE
LIFT
28
AIRFOIL IS DEFINIED BY
LEADING EDGE, TRAILING EDGE, AND CAMBER
29
LINE FROM LEADING EDGE AND TRAILING EDGE
CHORD
30
DIRECTION OF FLIGHT IS OPPOSED BY
RELATIVE WIND
31
RELATIVE WIND IS ALWAYS
OPPOSITE OF THE DIRECTION OF FLIGHT
32
HOW IS LIFT PRODUCED?
AIRFLOW UNDER AND OVER THE WING
33
WEIGHT IS
CONSTANT
34
ANGLE OF ATTACK
THE ANGLE FORMED BY THE WING'S CHORD LINE AND THE RELATIVE WIND
35
POSITIVE ANGLE OF ATTACK IS REQUIRED TO PRODUCE
LIFT
36
ATTACHED AIRFLOW
36
ATTACHED AIRFLOW
AIR FOLLOWS THE SURFACE OF THE AIRFOIL UNDER AND OVER AND LIFT IS PRODUCED
37
IN CRUISE FLIGHT THERE IS
RELATIVELY LOW ANGLE OF ATTACK
38
INCREASING ANGLE OF ATTACK INCREASES
LIFT
39
CRITICAL ANGLE OF ATTACK
THE FARTHEST THE ANGLE OF ATTACK CAN GO BEFORE IT STALLS
40
STALL
ABRUPT LOSS OF LIFT. OCCURS WHEN THE CRITICAL ANGLE OF ATTACK IS EXCEEDED
41
ANGLE OF ATTACK
THE ANGLE DESCRIBED BY THE RELATIVE WIND AND THE WING'S CHORD LINE
42
BERNOULLI'S PRINCIPLE
WHEN THE SPEED OF A FLUID IS INCREASES ITS PRESSURE DECREASES
43
AS A DENSITY OF A FLUID DECREASES (IT'S THINNING OUT)
SO DOES IT'S PRESSURE
44
AIRFLOW MOLECULES GO FASTER OVER THE CAMBER, WHICH PRODUCES A ___ ____ _____
LOW AIR PRESSURE
45
UNDER THE WING, THERE IS A _____ AIR PRESSURE
HIGHER
46
FLUIDS MOVE FROM AREA'S OF ____ PRESSURE TO AREAS OF _____ PRESSURE
HIGH, LOW
47
NEWTONS THIRD LAW OF MOTION
FORCES BETWEEN TWO OBJECTS EXIST IN EQUAL MAGNITUDE AND IN OPPOSITE DIRECTIONS (EVERY ACTION HAS AN EQUAL AN OPPOSITE REACTION)
48
AIR MOLECULES FLOWING UNDER THE WING ARE DEFLECTED DOWN, AND
PUSH UP THE WING BECAUSE OF NEWTONS LAW
49
PROPELLER EQUALS
AIRFOIL
50
LOAD FACTOR
AMOUNT OF FORCE IMPOSED ON AN AIRCRAFT STRUCTURE BASED ON THE amount of LIFT BEING PRODUCED. MEASURED IN G's
51
LOAD FACTOR MAY INCREASE
ANYTIME THE AIRCRAFT IS SUBJECTED TO MANEUVERS OTHER THAN STRAIGHT AND LEVEL FLIGHT
52
IN STRAIGHT AND LEVEL, UNNACELERATED FLIGHT, THE LOAD FACTOR IS
1
53
TO MAINTAIN A LOAD FACTOR OF 1 IN A 30 DEGREE BANK, THE AIRCRAFT MUST BE....
DESCENDING
54
WHICH BASIC FLIGHT MANEUVER INCREASES THE LOAD FACTOR ON AN AIRPLANE AS COMPARED TO STRAIGHT AND LEVEL FLIGHT
TURNS
55
THE AMOUNT OF EXCESS LOAD THAT CAN BE IMPOSED ON THE WING OF AN AIRPLANE DEPENDS UPON THE
SPEED OF THE AIRCRAFT
56
WHEN LOAD FACTOR INCREASES
STALL SPEED INCREASES
57
WHEN ARE THE FOUR FORCES THAT ACT ON AN AIRPLANE IN EQUILIBRIUM?
DURING UNACCELERATED FLIGHT
57
WHEN ARE THE FOUR FORCES THAT ACT ON AN AIRPLANE IN EQUILIBRIUM?
DURING UNACCELERATED FLIGHT
58
WHAT IS THE RELATIONSHIP OF LIFT, DRAG, THRUST, AND WEIGHT WHEN THE AIRPLANE IS IN STRAIGHT AND LEVEL FLIGHT?
LIFT EQUALS WEIGHT, THRUST EQUALS DRAG