Powered Flying Controls Flashcards

1
Q

Powered flight controls are operated by

A

Hydraulic actuators or powered flying controlled units

Each actuator is operated by a servo controlled valve

Have 2 or 3 actuators per fling control

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2
Q

Disconnect levers

A

Protects against jamming of controls

Reduces roll rate

Each pilot in control of their side

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3
Q

Shear rivets

A

Protect against control jamming - shear at a designated load - allows the remaining aileron to be used

Rudder centring may be lost when this is used

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4
Q

Power assisted control operation

A

Stick is connected to the valve and the hydraulic jack

When moved - hydraulic lock is unlocked in the power control unit/ hydraulic servo unit - moves the

High loads will get feedback - reversible - not artificial feel req

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5
Q

Fully powered control operation

A

Stick only operates the servo valve actuator or if fly by wire - cables and levers

Irreversible- needs artificial feel

Control is lost if hydraulic pressure is locked

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6
Q

Artificial feel systems are fitted

A

In parallel and duplicated

Senses dynamic pressure and control deflection - reduces the chances of over stressing the a/c

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7
Q

Artificial feel Q feel operation

A

Q pot - senses dynamic pressure by having a feed from pitot and static pressure

Diaphragm moves up and down depending on airspeed - as it moves upwards (more IAS) - allows more hydraulic pressure to go into the piston = harder to move the control column

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8
Q

The a/c may need to be trimmed in flight as a result of

A

Changes of speed and power

Varying CG posn

Trimming reduced the control loads to zero - either a control wheel or a selection of switches

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9
Q

Methods of trimming

A

The trim tab - moves in the opposite direction of the control surface

Variable incidence tailplane

CG adjustment - moving fuel around

Adjustment of the artificial feel unit - feel trim unit - combination of artificial and trim unit

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10
Q

Disadv of a trim tab

A

Reduces control authority in the direction of the trimming

Also increases drag

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11
Q

Fixed tabs

A

Not adjustable in flight

A/c has a permanent out of trim posn

Adjusted on the ground

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12
Q

Horizontal stabiliser trim is operated by

A

Older a/c - hydraulically

New a/c = electric

Both move a screw jack

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13
Q

If the variable incidence tailplane is not in the t/o posn for t/o

A

Intermittent horn will sound in the f/d

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14
Q

Variable incidence tailplane can be operated by

A

Trim wheel
Or
Switches that operate in pairs - one controls the power and another does the direction - prevents trim r/y - must be moved together

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15
Q

Adv of variable incidence tailplane

A

Drag is less

Trimming does not reduce the control authority

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16
Q

Mach trim purpose and operation

A

C or p moves rearwards at high airspeed - large nose down pitch moment - this prevents it

System will kick in at a datum speed - will move trim/fuel to prevent tuck under

17
Q

2 systems and diff in operation to prevent excessive rudder deflection at high airspeeds

A

Rudder ratio changer - Boeing - rudder pedals move through their full range - rudder deflection reduces with increasing IAS - not proportional

Variable stop systems - airbus - movement of the rudder is proportional to rudder travel - range of movement is reduced for both of them - starts to reduce at around 165kts

18
Q

Fly by wire

A

Mechanical input converted into an electrical output

19
Q

Adv of fly by wire

A

Relax the natural stability of the a/c - reduce the size of the tailplane - do not need to de ice as much - increases fuel efficiency - reduces weight

Reduces flight crew workloads

20
Q

Flight envelope protection takes into account

A

Pitch attitude protection
Load factor protection
Bank angle protection
AoA protection

21
Q

Control locks

A

A/c with reversible commands - when parked wind can damage the control surfaces - control locks manage this