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AT 354 > Flight Controls > Flashcards

Flight Controls Flashcards

1
Q

Nose gear doors

A

mechanical, inboard hydraulic, outboard mechanical

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2
Q

nose wheel doors can be manually opened on ground (T/F)

A

true

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3
Q

a steering pin must be removed prior to taxi (T/F)

A

false - must be inserted prior to taxi

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4
Q

what position should the flaps be in for a belly landing

A

zero flaps

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5
Q

(T/F) Steering is inoperative with nose gear not down and locked

A

true

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6
Q

for towing, the steering disconnect pin must be ____

A

removed

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7
Q

EMRG BRK LO PRESS

A

emergency brake accumulator pressure below 2250 psi

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8
Q

Maxaret

A

completely mechanical
reduces brake pressure in event of skid
will not function until wheel are spinning

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9
Q

hawker cannot takeoff for _______ after taxi

A

5 minutes

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10
Q

rejected takeoff wait times

A

25 minutes below 90ts, 45 below 90kts
inspection of over 90kts

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11
Q

Elevator trim annunciator

A

weight on wheels, thrust levers more than 40-60% N1

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12
Q

Mach trim

A

electric trim motor to increase stability above .73M

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13
Q

what type of flaps

A

interconnected slotted flaps powered by hydraulic systems
0, 15, 25, 45

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14
Q

what does lift dump do

A

increase flaps to 75 by air brake lever

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15
Q

stall warning indicated by

A

stick shaker (you are not stalled yet)

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16
Q

stall identification by

A

stick pusher (you are stalled)

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17
Q

autopilot does what with stall warniing

A

disengages

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18
Q

steering pin positions

A

horizontal for towing / on the ground
vertical for taxi / flight

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19
Q

nose wheel steering

A

Manually controlled, hydraulically actuated system provides 45 degrees right and left of center deflection

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20
Q

if loss of hydraulic power, can we (ground) steer the hawker

A

no
nose wheel steering not available when main pressure less than 2300 psi

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21
Q

illumination of red annunciators mean what

A

gear in transit, gear unlocked, or gear down and locked with gear selector lever out of down position

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22
Q

if gear is up and locked lights

A

all out

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23
Q

if gear is unlocked

A

red lights

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24
Q

gear is down and locked

A

green lights

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25
Q

gear down and locked, handle in wrong position

A

all lights (green and red)

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26
Q

what is the max gear extended speed

A

220kts

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27
Q

calls for gear

A

three green (gear speed 220)
pin (main counsel by thrust levers, should be out for nose wheel)
pressure (don’t want brakes applied)
center (tiller should be centered)
back up (lights on right side)

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28
Q

what’s a way to tell if gear is down if all gear systems are being wonky so

A

try flaps 25 - if horn goes off, gear is not down

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29
Q

gear horns

A

Gear not down and flaps 25, 45
Gear not down when aircraft is on ground and starter bus on
Gear not down and thrust angle below 60-70% and airspeed below 150 kts

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30
Q

which gear horn warning can be overridden

A

Gear not down and thrust angle below 60-70% and airspeed below 150 kts

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31
Q

how is normal vs emergency vs parking brake selected

A

WHEEL BRAKe lever on center pedestal

32
Q

when is anti skid protection provided

A

during normal brake operations only

33
Q

what is the anti skid system called

A

maxaret

34
Q

when will you know if you need emergency brakes

A

if you land and the brakes don’t work!
or hydraulic system failure

35
Q

how does maxaret work

A

mechanical
wheel must be moving

36
Q

for lift dump to work

A

on ground
“selected” 45 flaps

37
Q

airbrake limitations

A

NO FLAPS

38
Q

what is/is not included in the landing distance in the POM

A

thrust reverser not included
lift dump included

39
Q

on landing what do we use first and second

A

lift dump first
thust reverse 2nd

40
Q

what are takeoff flaps

A

0, 15

41
Q

landing flaps

A

25, 45

42
Q

where are indicated flaps

A

FO mfd

43
Q

ELEV/AIL TRIM

A

elevator OR aileron trim has failed

44
Q

full flaps speed

A

165

45
Q

25 flap speed

A

175

46
Q

15 flap speed

A

220

47
Q

stall warning

A

stick shaker
disengages autopilot

48
Q

stall happening

A

stick pusher

49
Q

what does one and two channels do for stalls

A

one channel activates stick shaker
both channels must agree for stick pusher

50
Q

What is powered by the PE bus bar

A

normal landing gear annunciators
warning horn control
warning horn
L and R EMERG WHEEL BRAKE annunciators

51
Q

What does the PS1 bus bar power

A

landing gear lever lock solenoid
normal BRAKES applied pressure indicator

52
Q

What does the PS2 bus bar power

A

standby landing gear downlink annunciator (2)

53
Q

Inadvertent landing gear retraction on the ground is prevented by

A

a solenoid-operated device engaging the selector lever

54
Q

when all landing gear are up and locked, the position indications are

A

no green or red annunciators are illuminated

55
Q

the main landing gear inboard doors are closed

A

when the gear is in either the extended or the retracted position

56
Q

the landing gear warning horn will sound when

A

gear is not locked down with flaps selected 25
the gear is not locked down with either power lever between 60% and 70% N1 and airspeed below 150kts
the gear is down and locked, the LANDING GEAR lever is not selected down, and start power is selected

57
Q

an indication of landing gear down and locked accompanied by 3 red annunciators indicates

A

the LANDING GEAR lever is not in the down position and the landing gear is down and locked

58
Q

if the nose gear does not lock down during extension, the indication is that

A

the red N GEAR annunciator on the panel is illuminated and the mechanical indicator on the pedestal is not extended

59
Q

nose wheel steering with the gear retracted is prevented by

A

A mechanically actuated hydraulic shutoff valve

60
Q

the EMRG BRK LO PRESS annunciator illuminates

A

when emergency brake accumulator pressure drops to 2250 psi and below

61
Q

in order to select emergency brakes, the WHEEL BRAKE lever must be positioned

A

to first aft notch marked in red

62
Q

stall warning system uses ____ power

A

DC and AC

63
Q

Elevator trim tabs can be actuated

A

mechanically and electrically

64
Q

The purpose of the rudder bias system is

A

to automatically counteract asymmetrical thrust due to engine failure

65
Q

if takeoff is attempted with the aileron/elevator gust lock

A

only one throttle can be advanced to full power

66
Q

the guard is removed from a pitch trim switch

A

during testing, to ascertain that trimming cannot be accomplished with one element of the switch

67
Q

the flight control surfaces that are hydraulically actuated are

A

flaps and airbrakes

68
Q

asymmetrical flap operation is prevented by

A

a synchronizing cable arrangement that isolates the hydraulic supply to the flap motor, stopping the flaps

69
Q

the purpose of lift dump is

A

to increase drag and decrease lift on the ground

70
Q

stall warning is provided by

A

the stick shaker

71
Q

stall identification is provided by

A

the stick pusher

72
Q

in the stall warning and identification system

A

flap position is integrated with angle-of-attack signals to determine critical angle of attack of the wing

73
Q

inadvertent stick pusher operation can be prevented by inhibiting

A

Both channel 1 and channel 2 at the same time

74
Q

the rudder bias annunciator extinguishes when

A

Both RUDDER BIAS switches are on

75
Q

Emergency brake system annunciators

A

white L/F EMERG WHEEL BRAKE when 1000 psi or more applied to brakes with WHEEL BRAKE lever in EMERG or PARK BRAKE position

AT 354 (12 decks)

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