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Drone Pilot Certification > Becoming Remote Pilot > Flashcards

Becoming Remote Pilot Flashcards

You may prefer our related Brainscape-certified flashcards:
Charter Pilot (Part 135) - Oral flashcards
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
Q

LATERAL AXIS MOTION ____

CONTROL _____

A

PITCH, ELEVATOR (OR STABILATOR)

25
Q

VERTICAL AXIS rotational MOTION_____

CONTROL _____

A

YAW, RUDDER

26
Q

AIRFOIL

A

AN OBJECT THAT PRODUCES AN AERODYNAMIC FORCE WHEN MOVED THROUGH A FLUID

27
Q

AIRFOIL IS USED TO PRODUCE

A

LIFT

28
Q

AIRFOIL IS DEFINIED BY

A

LEADING EDGE, TRAILING EDGE, AND CAMBER

29
Q

LINE FROM LEADING EDGE AND TRAILING EDGE

A

CHORD

30
Q

DIRECTION OF FLIGHT IS OPPOSED BY

A

RELATIVE WIND

31
Q

RELATIVE WIND IS ALWAYS

A

OPPOSITE OF THE DIRECTION OF FLIGHT

32
Q

HOW IS LIFT PRODUCED?

A

AIRFLOW UNDER AND OVER THE WING

33
Q

WEIGHT IS

A

CONSTANT

34
Q

ANGLE OF ATTACK

A

THE ANGLE FORMED BY THE WING’S CHORD LINE AND THE RELATIVE WIND

35
Q

POSITIVE ANGLE OF ATTACK IS REQUIRED TO PRODUCE

A

LIFT

36
Q

ATTACHED AIRFLOW

A
36
Q

ATTACHED AIRFLOW

A

AIR FOLLOWS THE SURFACE OF THE AIRFOIL UNDER AND OVER AND LIFT IS PRODUCED

37
Q

IN CRUISE FLIGHT THERE IS

A

RELATIVELY LOW ANGLE OF ATTACK

38
Q

INCREASING ANGLE OF ATTACK INCREASES

A

LIFT

39
Q

CRITICAL ANGLE OF ATTACK

A

THE FARTHEST THE ANGLE OF ATTACK CAN GO BEFORE IT STALLS

40
Q

STALL

A

ABRUPT LOSS OF LIFT. OCCURS WHEN THE CRITICAL ANGLE OF ATTACK IS EXCEEDED

41
Q

ANGLE OF ATTACK

A

THE ANGLE DESCRIBED BY THE RELATIVE WIND AND THE WING’S CHORD LINE

42
Q

BERNOULLI’S PRINCIPLE

A

WHEN THE SPEED OF A FLUID IS INCREASES ITS PRESSURE DECREASES

43
Q

AS A DENSITY OF A FLUID DECREASES (IT’S THINNING OUT)

A

SO DOES IT’S PRESSURE

44
Q

AIRFLOW MOLECULES GO FASTER OVER THE CAMBER, WHICH PRODUCES A ___ ____ _____

A

LOW AIR PRESSURE

45
Q

UNDER THE WING, THERE IS A _____ AIR PRESSURE

A

HIGHER

46
Q

FLUIDS MOVE FROM AREA’S OF ____ PRESSURE TO AREAS OF _____ PRESSURE

A

HIGH, LOW

47
Q

NEWTONS THIRD LAW OF MOTION

A

FORCES BETWEEN TWO OBJECTS EXIST IN EQUAL MAGNITUDE AND IN OPPOSITE DIRECTIONS (EVERY ACTION HAS AN EQUAL AN OPPOSITE REACTION)

48
Q

AIR MOLECULES FLOWING UNDER THE WING ARE DEFLECTED DOWN, AND

A

PUSH UP THE WING BECAUSE OF NEWTONS LAW

49
Q

PROPELLER EQUALS

A

AIRFOIL

50
Q

LOAD FACTOR

A

AMOUNT OF FORCE IMPOSED ON AN AIRCRAFT STRUCTURE BASED ON THE amount of LIFT BEING PRODUCED. MEASURED IN G’s

51
Q

LOAD FACTOR MAY INCREASE

A

ANYTIME THE AIRCRAFT IS SUBJECTED TO MANEUVERS OTHER THAN STRAIGHT AND LEVEL FLIGHT

52
Q

IN STRAIGHT AND LEVEL, UNNACELERATED FLIGHT, THE LOAD FACTOR IS

A

1

53
Q

TO MAINTAIN A LOAD FACTOR OF 1 IN A 30 DEGREE BANK, THE AIRCRAFT MUST BE….

A

DESCENDING

54
Q

WHICH BASIC FLIGHT MANEUVER INCREASES THE LOAD FACTOR ON AN AIRPLANE AS COMPARED TO STRAIGHT AND LEVEL FLIGHT

A

TURNS

55
Q

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

A

SPEED OF THE AIRCRAFT

56
Q

WHEN LOAD FACTOR INCREASES

A

STALL SPEED INCREASES

57
Q

WHEN ARE THE FOUR FORCES THAT ACT ON AN AIRPLANE IN EQUILIBRIUM?

A

DURING UNACCELERATED FLIGHT

57
Q

WHEN ARE THE FOUR FORCES THAT ACT ON AN AIRPLANE IN EQUILIBRIUM?

A

DURING UNACCELERATED FLIGHT

58
Q

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

A

LIFT EQUALS WEIGHT, THRUST EQUALS DRAG

Drone Pilot Certification (17 decks)

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