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Checkride V2 > Checkride Additional GK > Flashcards

Checkride Additional GK Flashcards

1
Q

AOA Comp Fail Effect on TP Stalls

A

AOA circuit breaker (batt buss front cockpit)
Land as soon as practical
Stick shaker and aural tones/warnings for CWS and LDG GR will be inop
Fly known pitch and power settings

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2
Q

Oil tank and system capacities

A

Oil tank: 10 quarts
Oil systems: 18.5 quarts

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3
Q

Oil specification

A

MIL -PRF-23699

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4
Q

Battery voltage limits

A

23.5 minimum
do not connect external power if below 22.0

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5
Q

Prop limits

A

62-80%
Overspeed limit is 110%

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6
Q

VMO (max operating speed)

A

316

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7
Q

MMO (max operating mach)

A

0.67

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8
Q

VG (turbulent air penetration speed)

A

195 max
180 recommended

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9
Q

Prohibited maneuvers

A

inverted spins
inverted stalls
aggravated spins past 2 turns
spins with pcl above idle
spins above/below 22000/10000ft PA
abrupt cross-controlled (snap) maneuvers
tail slides
aerobatics with greater than 50lbs fuel imbalance

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10
Q

Weight limits

A

max ramp weight: 6550
max TO weight: 6500
max LDG wight: 6500
max zero fuel weight: 5500
max weight in baggage compartment: 80lbs
max weight on glareshield: 8.5lbs

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11
Q

Barrier limits

A

taxi over arresting cables as slowly as possible, avoid contact with support donuts
TO/land beyond arresting cables
taxiing over lowered net barries should be avoided, idle and discontinue braking before crossing
raised web barrier should never be used, steer around or eject

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12
Q

Icing limits

A

climb or descend out of icing layer
aerobatics prohibited when icing is present
30 degree AOB and 2Gs
approach speed increased by 10 knots

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13
Q

fuel limits

A

aerobatics prohibited below 150lbs each side
799PPH all phases of flight
engine driven high pressure pump is limited to 10 hours without back up of boost pump/engine driven low pressure pump

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14
Q

max fuel imbalance

A

50 pounds

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15
Q

runway surface limits

A

tarmac, concrete or similar

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16
Q

Eejction seat nude BW limits

A

103lbs - 231lbs

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17
Q

How does RCR affect TOLD

A

Max abort speed increases as RCR increases

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18
Q

Maximum braking speed

A

if max abort speed is > (VB-20knots), then VB-20 is the new abort speed

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19
Q

Max Range

A

level flight speed that produces most miles (white triangle, 4.9 units)

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20
Q

Max Endurance

A

speed for minimum fuel flow in level flight time (white diamond 8.8 units)

21
Q

Landing distance assumptions

A

a 3 degree approach to the 50ft obstacle height
idle power and threshold speed as determined by chart at 50ft
2 second delay from touchdown to initiation of braking
max braking once a/c is firmly on the ground
braking friction coefficient for dry asphalt or concrete rwy corresponds to an RCR of 23

22
Q

FOD prevention

A

do not approach an operating engine
no excessive power
avoid prop/jet blast from other a/c
loose items stowed/secured before opening canopy
do not place anything on the canopy

23
Q

GPS approach minimums used

A

LNAV and circling lines of minima listed

24
Q

When not to request high key from initial

A

a/c between 5 & 2 NM on straight in
a/c between report high key and lowkey
when a/c reports OH field direct to VFR entry
orbiting high key
high pattern

25
Q

when not to request high key from elsewhere in pattern (CW, ODW)

A

when more than 3 (HONCHO)/5(WIZARD) in pattern
a/c on breakout
a/c between report HK/LK
state position when making request
remain clear of center rwy groundtrack and associated airspace

26
Q

when not to request high key from initial

A

5 & 2NM on a straight in
report HK and LK
OH the field proceeding to VFR entry
orbiting high key
high pattern

27
Q

Unable VMC in MOA

A

advise controller
standard IFR separation until 3SM and CoC
wingman sqwuaks 0000 while in MOA

28
Q

When does reduced rwy separation not apply

A

when T-6 is following a formation, T-38 or T-1
alternate side procedures are not used = 6000 ft
when T6 formation is following another AETC trainer cat a/c

29
Q

STEADY GREEN LIGHT

A

ground: cleared for TO
In-Flight: Cleared to land

30
Q

FLASHING GREEN LIGHT

A

Ground: Cleared to taxi
In-Flight: Return for ldg

31
Q

STEADY RED

A

ground: stop
in-flight: give way to other a/c

32
Q

FLASHING RED

A

ground: taxi clear of rwy
in-flight: do not land

33
Q

FLASHING WHITE

A

return to start point

34
Q

ALTERNATING GREEN AND WHITE

A

exercise extreme caution

35
Q

Airborne NORDO procedures

A

squawk 7600
turn on all exterior lights (night)
VMC: recover via entry point using IFG groundtrack and altitudes
rock wings at initial
look for stead green to land

36
Q

When can a destination be filed to?

A

WX @ destination from 1hr before to 1hr after ETA is forecasted to be at or above lowest compatible app mins
TEMPO conditions may be below published app mins
straight in or sidestep app forecasted WX must meet vis mins
circling app forecasted WX must meet both ceiling and vis mins

37
Q

when is an alternate required?

A

no compatible inst app at destination
WX forecast 1hr before and after ETA at destination including TEMPO lines are less than 2000 and 3SM
forecasted crosswinds are out of limits

38
Q

what are the alternate requirements

A
  • 1hr before and after ETA including TEMPO (except thunderstorms/rain/snow showers)
    ceilings are 1000ft or 500ft above lowest compatible app mins whichever is higher and 2 SM vis or 1SM vis above lowest compatible app mins, whatever is greater
  • if no compatible app, VMC must be available at alternate
39
Q

when to not use an airport as an alternate

A
  • unmonitored NAVAID for app
  • no weather observation
  • if Ana is on all applicable approaches
  • any note disquaifying the airfield or all compat app in the IFR alternate mins section
40
Q

control and performance method

A

establish
trim
cross-check
adjust

41
Q

ILS usable range

A

localizer - 18NM w/i 10 degree sector and 10NM within a 35 degree sector

42
Q

localizer is within how many degrees of rwy centerline?

A

3 degrees FAA/ 5 degrees ICAO

43
Q

LDA (localizer type directional aid)

A

greater than 3 degree offset from rwy center line

44
Q

Established on track meaning

A

full scale deflection (one dot)
within +/- 5 of required bearing for NDB
within full scale deflection for LOC (case break)
within 1x the required accuracy for RNAV or RNP segments flown

45
Q

Aircraft category

A

A = less than 91 knots
B = 91 - 120
C = 121 - 140
D = 141 - 165
E = greater than 166

46
Q

procedure turn methods

A

45/180
80/260
teardrop

47
Q

SNERT (no procedure turn)

A

straight-in
No-PT
Established on IB course
Radar vectors
Timed approach

48
Q

Decision Altitude

A

specified barometric altitude; pilot decides to continue or go missed

Checkride V2 (1 decks)

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