There is a seemingly endless list of crucial components within an aircraft, and today we’ll be testing you on two of them – propellers and small gas turbines! Think you know your stuff? Find out today!
Barrel
Control
Low pitch stop
Pitchlock requlator
Microadjusting ring
Beta feedback shaft
Blade segment gear
Blade bushing
Stops the dome piston from increasing blade angle above 23.3
Prevents the blades from decreasing pitch if hydraulic pressure is lost
Prevents cam bearing rollers from bottoming out in the track slopes
Prevents the propeller from going into the beta range when the throttle is positioned in alpha range
Pitchlock control cam
Pitchlock ratchet piston
Externally threaded ring
Externally splined spacer ring
Beveled thrust washer
Stationary ratchet
Beta segment gear
Blade barrel shim
Roller shaft
Track slopes
Ball bearings
Roller bearings
Prevents the popeller from goin in to the beta range when the throttle is positioned in the alpha range
Limits cam travel and prevents the propeller from exceeding feather and reverse balde angles
Prevents the blades from decreasing pitch if an overspeed condition occurs
Transmits engine torque to the blades
Deicer cnotact ring holder
Hub mounting bulkhead
Front spinner
Afterbody
Valve housing
Low pich stop
Transfer bearing
Pitchlock regulator
Drives the main and standby pressure pumps
Controls operation of the pilot valve and serves as an electrical ground
Drives the rotation sleeve when the throttle is positioned in the beta range
Transmits blade angle movement to the valve housin and drives the propeller governor flyweights
Main pressure and main scavenge
Standby pressure and main scavenge
Auxiliary pressure and main pressure
Auxiliary pressure and auxiliary scavenge
Manual feather
Beta follow up
Speed set
Beta set
Standby
Feather
Backup
Pilot
99 to 103%
104 to 108%
109 to 113%
114 to 118%
0*
18*
34*
90*
Beta indicator
Landing gear warning
Low speed ground idle
Synchrophaser disarming
Landing gear touchdown
Low speed ground idle
Landing gear warning
Air start
Feather shaft
Potentiomether
65* microswitch
66* microswitch
Auxiliary pressure
Standby pressure
Backkup pressure
Main pressure
Check
Bypass
Low pressure relief
High pressure relief
Check
Bypass
Low-pressure relief
High-pressure relief
Pitchlock
Standby
Reverse
Airstart
Main
Backup
Standby
Auxiliary
Check
Bypass
Low pressure relief
High pressure relief
The loss of oil pressure
An engine overspedd due to a loss of power
The flow of hydraulic fluid to the pilot valve
An engine ovespeed due to a loss fo hydraulic pressure
An overspeed of 103.5%
The pitchlock control cam
A loss fo hydrulic pressure
Increase- or decrease pitch pressure
An overspeed of 103.5%
The pitchlock control cam
A loss fo hydrulic pressure
Increase- or decrease pitch pressure
Propeller barrel from decreasing blade angle below 23.3* +_ .5*
Dome piston from decresing blade angle below 23.3* +_ .5*
Propeller barrel from decreasing blade angle below 34* +_ .5*
Dome piston from dereasing blade angle below 34* +_ .5*
Wedge
Servo valve
Dome piston
Hydraulic pressure
Blade pitch and engine fuel flow
Blade pitch and temperature limiting
Engine fuel flow and constant speed governing
Temperature limiting and constant speed governing
Beta set
Speed set
Backup balve
Beta follow-up
Beta set
Speed set
Backup valve
Beta follow-up
Decreased hydraulic pressure
Increased hydraulic pressure
Speeder spring
Flyweights
Throttle
Beta shaft
Pilot valve
Manual feather cam
Aft end of the dome piston
Forward end of the dome piston
Decreased-pitch side of the pilot valve
Increased-pitch side of the pilot valve
Pilot
Feather solenoid
Feather actuating
Standby pump check
Auxiliary pressure
Auxiliary scavenge
Main scavenge
Feather
0 to 200
300 to 500
600 to 800
900 to 1,100
Feather relay
Feather solenoid
Pressure cutout switch
PCBS
Any throttle position
Above FLT IDLE
At TAKE OFF
At GND IDLE
Manual feather and pressure cutout backup switch
Speed set and pressure cutout backup switch
Speed set and beta follow-up
Manual feather and beta set
200
400
600
800
Speed set cam
Feather valve
Beta set cam
Pilot valve
100%
102%
104%
106%
No. 1 blade
Pump housing
Valve housing
Deicer contact ring holder assembly
To drive the feedback potentiometer
As a backup for throttle anticipation
When a master propeller is selected
To indicate actual rpm
Throttle anticipation potentiometer speeds up or slows down the engine
Speed bias motor rotates, and increases or decreases blade angle
Speed bias sevo control locks the clutch and brake unit
Feedback potentiomether recenters the speed bias motor
No. 1 and no. 2
No. 2 and no. 3
No. 3 and no. 4
All four propellers
Double slave
Power supply
Power amplifier
Master synchrophaser
2%
4%
6%
8%
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