propa Flashcards

1
Q

what is the manufacturers name and designation?

A
5- Major modifications to the original prop design
4- No of blades
H- Blade shank size
60- SAE spline size
77- Minor modification size
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2
Q

What 3 pubs state the fluid for the prop

A

Flight manual
F700
FOLS
Aircraft servicing form

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3
Q

Definition of the ground range of the co ordinator

A

0-34 degrees

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4
Q

What is the force that dries blades to a fine angle

A

Centrifugal twisting force

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5
Q

Force that drives the blades to a coarse pitch

A

Aerodynamic twisting force

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6
Q

what action needs to be done before removing the prop nut

A

Check torque. If there is movement, prop is considered to be loose on the shaft

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7
Q

Purpose of a stop ring

A

Provides a mechanical stop at 86.65* for feather and -14 for maximum reverse blade angle

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8
Q

What is the name of the component on dome that meshes with blade segment gears

A

Rotating cam has a bevel gear that meshes with blade segment gears

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9
Q

Where do you find the shim thickness

A

Written on the dome shelf

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10
Q

What is the purpose of the feather latches on the bottom of the dome

A

This will lock the prop to feather

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11
Q

4 major parts of a spinner assy

A

front spinner
rear spinner
bulkhead
afterbodies

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12
Q

major functions of the barrel assy

A

retain blades
secure the prop to the shaft
transmit the drive from the engine to the blades

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13
Q

when will PP2 pressure assist PP1

A

large loads

main pump fail

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14
Q

purpose of sump relief valve and at what pressure

A

maintains a positive pressure to prevent cavitation within the pressurised system and
provides a constant reference pressure
mounted between P.S and A.S, 20 psi

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15
Q

what are the 5 pumps and how much psi

A
PP1- 20
PP2-40
Aux pump-15
Main scav- 20
Aux scav-15
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16
Q

What is the angle of the blades when they are at the feather position

A

86.65

17
Q

2 conditions that move the feather valve to feather

A

e handle

nts

18
Q

where is the standby filter located

A

top of the valve housing

19
Q

what is the precaution with the no 1 blade

A

dont turn the blade cuff as the drive cog beta gear could be close to the end of its run

20
Q

2 functions of the manual feather cam

A

mechanically position the feather valve to the feather position when the e handle is pulled

cam out the nts when the throttle is retarded below 25* co ord

21
Q

what are the 2 flight deck controls that rotate the alpha shaft

A

throttle

e handle

22
Q

what is the purpose of the beta set cam

A

sets blade angle in the ground range
provide beta follow up in the flight range and guarantees a minimum of 23 deg Blade angle when the throttle is at take off

23
Q

what is the purpose of the pressure cut out switch

A

prevents termination of the aux pump before 74* BA should pressure surges occur

24
Q

What is the blade angle range when the beta light comes on

A

Beta range is 10*

25
Q

Precaution when separating valve housing and control housing

A

ensure the pin is fitted to prevent damage

26
Q

Where is the low pitch stop located

A

front of the dome

27
Q

True or false
auto feather tss mechanically position the valve???

the prop cannot fully feather is the aux pump fails?

The e handle cannot feather if mechanically at the co ordinator fails???????

A

false
true
false

28
Q

3 systems that will send the prop towards auto feather

A

e handle
nts
tss
feather button

29
Q

what will happen if the prop is unfeathered without pressing pco button

A

it will hunt towards 46.65/45

30
Q

how do you measure blades

A

using the blade reference station, dimple and dimpled slot in loc foam.
blade alignment reading number is used to calculate if a blade has been bent

31
Q

BA used for setting up protractor in valve housing

A

86.65 feather angle

32
Q

2 methods of holding pitchlock teeth disengaged

A

cam out ring

hyd pressure

33
Q

what forces the engagement of the 2 teeth of the rotating and stationary ratchet together

A

springs

34
Q

2 conditions to initiate pitchlock

A

overspeed of 103.5%

loss of oil

35
Q

pitchlock reset conditions

A

throttle below 28 * co ord

blade above 10*

36
Q

purpose of the low pitch stop assy

A

prevents blades reducing pitch into the ground range <13* while the throttle is in the flight range 34-90* co ord

37
Q

angle at which lowpitch stop hits the blades

A

13* degrees