EXAM 1 OFFICIAL Flashcards

1
Q

**3 conditions for entering settling with power

multiple choice questions

A

vertical or near vertical descent rate of at lease 300 FPM
the engine must be using 20-100% power
speed less than ETL

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2
Q

**2 initial physical responses to settling with power:

A

increase airspeed with cyclic (fwd)

reduce collective pitch as attitude permits

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3
Q

**autorotation (definition)

A

an event in which no engine power is supplies, main rotor is driven by the relative wind only

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4
Q

**3 conditions for onset of dynamic rollover: (in order)

A

establish a pivot point, initiate a rolling motion, exceeding the critical angle

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5
Q

**2 Factors that effect dynamic rollover

A

human and physical

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6
Q

**what is the recommended action at the onset of dynamic rollover?

A

smooth and moderate collective reduction

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7
Q

**primary cause of retreating blade stall:

A

excessive airspeed

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8
Q

**what are the 2 symptoms of a retreating blade stall?

A

pitch up of the nose followed by a roll to the left

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9
Q

**what are the 2 initial responses for a retreating blade stall?

A

reduce collective pitch

regain control of the aircraft

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10
Q

military TAF is valid for how many hours?

A

30

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11
Q

9999 is what type of visibility

A

greater than 7 statute miles

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12
Q

ceiling definition

A

lowest layer aloft which is reported broken or overcast when skies are considered totally obscured

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13
Q

3 weather proximity stations and distances

A

OS- on station, center of runway to 5 miles
VC- in vicinity of 5-10 miles
DSNT- Distant, greater than 10 miles

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14
Q

terms for unlimited visibility

A

sky clear/ clear skies (CLR)

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15
Q

terms for layers (sky coverage not considered ceiling)

A

scattered/ few

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16
Q

terms for ceilings

A

broken/ overcast

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17
Q

When is VV used in sky coverage reporting

A

Vertical visibility is used when the skies are considered totally obscured (TO)

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18
Q

**in IMC conditions, if the static system dumps, what should your first physical action be?

(may be write in)

A

activate alternate static source

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19
Q

which instrument does the pitot tube connect to?

A

airspeed indicator

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20
Q

view altimeters barometric pressure through:

A

the kollsman window

21
Q

freezing level on standard air and PA day

A

7500 feet

22
Q

lag delay when you level off with ISVI

A

0 seconds

23
Q

which instruments would static system failure affect?

A

all 3 (airspeed indicator, altimeter, vertical speed indicator)

24
Q

how does induced flow move?

A

vertically downward

25
Q

rotor blade coning is a compromise between what forces?

A

lift and centrifugal force

26
Q

relationship of total forces to a tip path place

A

perpendicular

27
Q

2 conditions for attailain ETL

A

horizontal flight of hovering in a headwind

28
Q

ETL speed range

A

16-24KIAS

29
Q

3 ways to compensate for tail rotor thrust (translating tendency)

A

left cyclic, tilt mast, left cyclic input by pilot

30
Q

speed for transverse flow effect

A

10-20kts

31
Q

4 causes of excessive coning (also retreating blade stall)

A

low RPM, high GWT, high G maneuvers, turbulent air

32
Q

only way to diminish the effects induced flow

A

increase forward airspeed

33
Q

what is the dominant force in the rotor system

A

centrifugal force. provides rigidity by taking the gravitational droop out of the blades

34
Q

pressure and temperature at MSL / standard lapse rate

A

29.92Hg and 15 degrees Clapse rate is 1’ per 1000 ft, 2 degrees

35
Q

what 2 pressures affect systems?

A

static and dynamic pressure

36
Q

how does total force act in relation to tip path place?

A

perpendicular

37
Q

two components of total force

A

a. vertical acts as lift which opposes weight

b. horizontal acts as thrust which opposes drag

38
Q

2 conditions of flight

A

balanced and unbalanced

39
Q

how do pilots control blowback?

A

forward airspeed

40
Q

purpose of the kollsman window

A

to correct barometric pressure changes

41
Q

pressure altitude

A

height above standard datum plane

42
Q

absolute altitude

A

hight above surface terrain or ground

43
Q

max mechanical altimeter error

A

plus or minus 75 ft

44
Q

calibrated airspeed (def)

A

indicated airspeed corrected for instrument

45
Q

indicated airspeed (def)

A

airspeed indicated on instrument, uncorrected

46
Q

aviators can ensure accuracy of any altimeter by regularly obtaining what along route?

A

current altimeter setting

47
Q

which of newton =s laws relates to takeoff to a hover

A

action/reaction (3)

48
Q

rotational relative wind

A

parallel and opposite to the direction of the airfoil

49
Q

what is resultant relative wind

A

rotational relative wind modified by induced flow