23. MODULE 17A (B1) — PROPELLER
32 multi-choice. Time allowed 40 minutes.
1 / 32
How is the oil pressure delivery on a hydromatic propeller normally stopped after the
2 / 32
A compound twin spool engine is
3 / 32
If force is applied to the speeder spring, what will happen?
4 / 32
A windmilling propeller has
5 / 32
Forces acting on a propeller are.
6 / 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
7 / 32
Electrical power supplies on large aircraft, for electrical deicing are
8 / 32
From reverse pitch, returning to normal pitch, the blade:
9 / 32
A conventional turboprop torque meter uses.
10 / 32
Temporary storage is generally defined as non use of aircraft for
11 / 32
To achieve reverse pitch the blade angle must be.
12 / 32
The Function Of Counterweights On A Propeller Is
The Additional Centrifugal Force Means That The Max. Rpm Must Be Reduced.
13 / 32
If A 2 Blade Prop Is Placed On A Knife Edge And It Ends Up Horizontal (blades At 3 And 9 O’clock Positions), It Is Said To Be In Balance
14 / 32
How is oil pressure delivery to a hydromatic propeller normally stopped after feathering?
15 / 32
The purpose of blade twist is to.
16 / 32
Counterweights are fitted to blade root to.
17 / 32
The limits for a tracking check are.
18 / 32
What Is The Angle Of Advance?
19 / 32
Ground running an aircraft with a fixed pitch prop with its tail into wind causes the
20 / 32
When on the ground with the engine idling the prop control should be.
21 / 32
Ground Running An Aircraft With A fixed Pitch Prop With Its Tail Into Wind Causes The Engine Rpm T
22 / 32
When in reverse pitch, CTM will tend to move propeller blades towards:
23 / 32
If governor flywheel overcomes the speeder spring, it indicates.
24 / 32
On an electrical de-icing system, when is the ‘fast cycle’ typically used?
25 / 32
The output of an anti-icing pump is controlled by.
26 / 32
At constant rpm, advance per revolution depends on
27 / 32
Which of the following generally renders an aluminium alloy propeller
28 / 32
After a lightning strike.
29 / 32
Multi engine aircraft synchronising works by
30 / 32
Propellers exposed to salt spray should be flushed with.
31 / 32
The limits for blade angle are controlled by pitch stops on the
32 / 32
A line of indentations across more than 25% of the chord at one blade section can be
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