23. MODULE 17A (B1) — PROPELLER
32 multi-choice. Time allowed 40 minutes.
1 / 32
Metal Fixed-pitch Propellers Are Made From
2 / 32
Constant Speed Non-feathering Mccauley, Hartzell And Other Propellers Of Similar Design Without Counterweights Increase Pitch Angle Using
3 / 32
On An Underspeed Condition The Blades Are Turned To
4 / 32
The Holding Coil Of A Hydromatic Propeller Feathering Button Switch Holds A relay Closed That Applies Power To The Propeller
5 / 32
Synchronisation Controls Rpm Within What Range?
6 / 32
In What Position Is The Constant-speed Propeller Control Placed To Check The Magnetos?
7 / 32
An Aerodynamic Braking Propeller Goes Through
8 / 32
If The Propeller Cone Or Hub Cone Seats Show Evidence Of Galling And Wear, The Most Likely Cause Is
9 / 32
If The Spur Gear Pump In A Single Acting Propeller Governor Failed, The
10 / 32
How Is The Power Output Of A Turbo Prop Engine Assessed?
11 / 32
An Aerodynamic Correction Factor That Is Preceded By The Letter ‘q’ Indicates
12 / 32
Aerodynamic Correction Factor (acf)
13 / 32
How Is The Oil Pressure Delivery On A Hydromatic Propeller Normally Stopped After The Blades Have Reached Their Full-feathered Position?
14 / 32
In A Hydromatic (hamilton-standard) Propeller With Counterweights, What Is Used To Make The Propeller Move To Fine Pitch?
15 / 32
In Cruise
16 / 32
A Propeller Has A Model Number 1f100/cm 69 54. What Does 69 And 54 Mean?
See 61-00-01 Page1 Of Macauley Manual
17 / 32
If The Hydraulic Safety Stop Operates, In Which Direction Can The Pitch Of Propeller Move?
18 / 32
An Adjustment Is Required To The Maximum Rpm. Where Is The Adjustment Carried Out?
19 / 32
The Function Of Counterweights On A Propeller Is
The Additional Centrifugal Force Means That The Max. Rpm Must Be Reduced.
20 / 32
Which Tapered Cone Are Split In Half With Serial Numbers?
21 / 32
In A De-icing System, How Is Continuous Operation Observed?
22 / 32
The Holding Coil Of A Hydromatic Propeller Feathering Button Switch Holds A Relay Closed That Applies Power To The Propeller
23 / 32
Aerodynamic Twisting Moment Tends To
24 / 32
Electrically De-iced Propeller Slip Rings Have Regular Resistance Checks For
25 / 32
A Propellor Brake Has An Interlock, This Is Connected To
26 / 32
A Propeller Blade Absorbs More Torque At
27 / 32
In A Propeller Synchrophasing System, An Electric Actuator
28 / 32
Manually Feathering A Hydromechanical Propeller Means To
29 / 32
Insulation Testing Of Electrical De-icing Systems Should Be Periodically Carried Out Because Of
30 / 32
A Hydraulic Pitch Lock Is Utilised In A Hydromatic Propeller To
31 / 32
How Is The Oil Pressure Delivery On A Hydromatic Propeller Normally Stopped after The Blades Have Reached Their Full-feathered Position?
32 / 32
If The Tas Of An Aircraft Increases, The Csu (constant Speed Unit) Will
this Causes Blade To Coarsen Off To Stop Overspeeding And As A Result The Speed Remains The Same
Your score is
The average score is 0%
Restart quiz
Your email address will not be published. Required fields are marked *
Comment *
Name *
Email *
Website
Save my name, email, and website in this browser for the next time I comment.
