JAR - Principle Of Flight Q&As
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JAR - Principle Of Flight Q&As
Just to jump on the Q&A's Bandwagon....
These are all feedback questions, got me through P of F with a fairly high mark!!!.
1
At a constant CAS when flying below sea level an Aircraft will have:
a) a higher TAS than at sea level
b) a lower TAS than at sea level at ISA conditions
c) the same TAS than at sea level
d) the same TAS, but an increase in IAS
2
What happends to static pressure as air flows through an expansion wave:
a) Increase
b) Decrease
c) stay the same
d) Initially increases then decreases
3
If the stalling speed in a 15 bank turn is 60kt, what would the stall speed be in a 45 bank?
a) 83kt
b) 70kt
c) 85kt
d) 60kt
4
Under which of the following conditions would a aircraft be most stable?
a) CG on the forward limit
b) CG on the aft limit
c) CG on the aft neutral limit
d) CG just forward of the neutral point
5
Which of the following is a correct design gust value?
a) 25ft/sec at VB
b) 50ft/sec st VC
c) 66ft/sec at VD
d) 55ft/sec at VD
6
What phenomena causes induced drag?
a) Wing tip vortices
b) Wing Tanks
c) The increased pressure at the leading edge
d) Spanwise flow, inward below, outward above
7
Which of the following aircraft designs would be most prone to super stall
a) 'T' Tail
b) Swept forward wing
c) Swept back wing
d) pod mounted engines beneath the wing
8
If an aircraft is statically unstable it:
a) can never be dynamically stable
b) will always be dynamically stable
c) may or may not be dynamically stable
d) will only be dynamically stable at high speeds
9
The Mach trim system:
a) Operates at all Mach numbers
b) at low Mach numbers only
c) at high Mach numbers only
d) operates at supersonic speeds only
10
An aircraft whose weight is 237402N stalls at 132kt. At a weight of 356103N it would stall at:
a) 88kt
b) 162kt
c) 108kt
d) 172kt
I'll post some more when I get the time...
ANSWERS:
1 b
2 b
3 b
4 a
5 b
6 a
7 c
8 a
9 c
10 b
------------------
I've Got Bad Attitude!
[This message has been edited by JB007 (edited 22 June 2001).]
These are all feedback questions, got me through P of F with a fairly high mark!!!.
1
At a constant CAS when flying below sea level an Aircraft will have:
a) a higher TAS than at sea level
b) a lower TAS than at sea level at ISA conditions
c) the same TAS than at sea level
d) the same TAS, but an increase in IAS
2
What happends to static pressure as air flows through an expansion wave:
a) Increase
b) Decrease
c) stay the same
d) Initially increases then decreases
3
If the stalling speed in a 15 bank turn is 60kt, what would the stall speed be in a 45 bank?
a) 83kt
b) 70kt
c) 85kt
d) 60kt
4
Under which of the following conditions would a aircraft be most stable?
a) CG on the forward limit
b) CG on the aft limit
c) CG on the aft neutral limit
d) CG just forward of the neutral point
5
Which of the following is a correct design gust value?
a) 25ft/sec at VB
b) 50ft/sec st VC
c) 66ft/sec at VD
d) 55ft/sec at VD
6
What phenomena causes induced drag?
a) Wing tip vortices
b) Wing Tanks
c) The increased pressure at the leading edge
d) Spanwise flow, inward below, outward above
7
Which of the following aircraft designs would be most prone to super stall
a) 'T' Tail
b) Swept forward wing
c) Swept back wing
d) pod mounted engines beneath the wing
8
If an aircraft is statically unstable it:
a) can never be dynamically stable
b) will always be dynamically stable
c) may or may not be dynamically stable
d) will only be dynamically stable at high speeds
9
The Mach trim system:
a) Operates at all Mach numbers
b) at low Mach numbers only
c) at high Mach numbers only
d) operates at supersonic speeds only
10
An aircraft whose weight is 237402N stalls at 132kt. At a weight of 356103N it would stall at:
a) 88kt
b) 162kt
c) 108kt
d) 172kt
I'll post some more when I get the time...
ANSWERS:
1 b
2 b
3 b
4 a
5 b
6 a
7 c
8 a
9 c
10 b
------------------
I've Got Bad Attitude!
[This message has been edited by JB007 (edited 22 June 2001).]
