1.
Which 54h60-117 propeller propeller subassembly transmits engine torque to the propeller blades?
A. 
B. 
C. 
D. 
2.
Which 54h60-117 propeller subassembly carries high centrifugal loads created by the propeller blades?
A. 
B. 
C. 
D. 
3.
On the 54h60-117 propeller, which component delivers the actual propeller blade angle from the blade to the control assembly?
A. 
B. 
C. 
D. 
4.
On the 54h60-117 propeller, which pitchlock component mechanically holds the stationary and rotating pitchlock ratchets pitchlock ratchets apart during reversing and unfeathering operations?
A. 
B. 
C. 
D. 
Externally splined spacer ring
5.
On the 54h60-117 propeller, what component is installed on the blade before the blade butt is formed during manufacture?
A. 
B. 
C. 
D. 
6.
On the 54h60-117 propeller, which dome assembly part allows the rotating cam to turn while the stationary cam remains in a fixed position?
A. 
B. 
C. 
D. 
7.
On the 54h60-117 propeller, which dome assembly component limits cam travel and prevents the propeller from exceeding feather and reverse blade angles?
A. 
Rotating pitchlock ratchet
B. 
C. 
D. 
8.
On the 54h60-117 propeller propeller, what functions is a task of the low pitch stop assembly?
A. 
Prevents the propeller from going into the beta range when the throttle is positioned in the alpha range
B. 
Limits cam travel and prevents the propeller from exceeding feather and reverse blade angle angles
C. 
Prevents the blades from decreasing pitch if an overspeed condition occurs
D. 
Transmits engine torque to the blades
9.
On the 54h60-117 propeller, which component's purpose is to provide electrical circuits between the brush block assembly and the deicing elements of the blade assemblies?
A. 
B. 
C. 
D. 
Deicer contact ring holder
10.
On the 54h60-117 propeller, during normal propeller operation, the output of which pumps is used?
A. 
Main pressure and main scavenge
B. 
Standby pressure and main savenge
C. 
Auxiliary pressure and main scavenge
D. 
Auxiliary pressure and auxiliary scavenge
11.
On the 54h60-117 propeller, which pump(s) is/are used during propeller static operation?
A. 
B. 
C. 
Standby pressure and main scavenge
D. 
Auxiliary pressure and auxiliary scavenge
12.
On the 54h60-117 propeller, which cam disarms the NTS system linkage when the throttle is positioned in the beta range?
A. 
B. 
C. 
D. 
13.
On the 54h60-117 propeller, which cam schedules a desired blade angle in the beta range?
A. 
B. 
C. 
D. 
14.
On the 54h60-117 propeller, which valve connects the main, standby, and auxiliary pressure pumps' output to the increase pitch lines during negative torque conditions?
A. 
B. 
C. 
D. 
15.
On the 54h60-117 propeller, which valve assists the feather solenoid valve with hydraulic positioning of the feather and pilot valves?
A. 
B. 
C. 
D. 
16.
On the 54h60-117 propeller, what switch, located in the valve housing, is opened by a cam from 81 to 85 degress propeller blade angle?
A. 
B. 
C. 
D. 
17.
The 54h60-117 propeller governor speeder spring tension positions the pilot valve to maintain what percent rpm in the beta range?
A. 
B. 
C. 
D. 
18.
On the 54h60-117 propeller, if the main filter becomes clogged, which valve opens to assure continued flow?
A. 
B. 
C. 
D. 
19.
On the 54h60-117 propeller, when the backup valve is opened, the hydraulic pressure routed to th governor pilot valve is used for which operation?
A. 
B. 
C. 
D. 
20.
On the 54h60-117 propeller, which pressure pump is used to feather or unfeather the propeller during static propeller operation?
A. 
B. 
C. 
D. 
21.
On the 54h60-117 propeller, which type of valve opens to allow the output of the standby pump to combine with the output of the main pump?
A. 
B. 
C. 
D. 
22.
On the 54h60-117 propeller, when standby pump output is not required, where is it routed?
A. 
B. 
C. 
D. 
23.
What type of force used during pitchlock of the 54h60-117 propeller prevents the blades from decreasing pitch?
A. 
B. 
C. 
Centrifugal twisting moment
D. 
Aerodynamic twisting moment
24.
The purpose of the 54h60-117 propeller pitchlock assembly is to prevent?
A. 
B. 
Flow of hydraulic fluid to the pilot valve
C. 
An engine overspeed due to a loss of power
D. 
Engine overspeed due to a loss of hydraulic pressure
25.
What prevents engagement of the stationary and rotating ratchets on the 54h60-117 propeller when blade angle are below 25 and 55 degrees?
A. 
Loss of hydraulic pressure
B. 
The pitchlock control cam
C. 
An overspeed in excess of 103.5%
D. 
Increase- or decrease pitch pressure