CPAER General Questions With Correct
Answers
If |an |airplane |stalls |in |a |coordinated |climbing |right |turn
left |wing |stalls |first, |leading |to |an |incipient |spin |to |the |left |-- |e.g., |upper |wing |stalls |first |
causing |the |wing |to |drop |and |spin |to |the |left
What |marshalling |signal |has |arms |extended |at |elbows |and |wands |moving |up |and |down |from |
chest |height |to |head |height
Move |Forward
If |oil |pressure |is |lost |in |a |hydraulic, |non |counterweight, |constant |speed |propeller
The |propeller |will |move |to |full |fine
The |fuel-air |ratio |for |best |power |is
14 |parts |air |to |1 |part |fuel |by |WEIGHT
If |a |turn |coordinator |indicates |needle |right |(Rate |1 |turn) |ball |left, |what |is |the |correct |actiion
In |this |case |you |could |slow |the |aircraft |down |that |would |increase |the |rate |1 |turn |angle |and |
therefore |undo |the |skid.
In |a |free |turbine |engine, |are |the |compressor |and |power |turbines |connected?
No |... |this |is |why |the |exhaust |of |the |power |turbine |is |in |the |front
Which |enhances |stability, |Dihedral |or |washout |Washout
Dihedral
Approaching |on |a |3 |degree |approach |with |a |3 |bar |basis, |the |middle |bar |will |appear(red/white)
|to |a |wide |bodied |airplane |and |(red/white) |to |a |small |aircraft?
For |the |large |aircraft |-- |WHITE, |for |the |small |aircraft |-- |RED
How |many |lights |for |each |3 |bar |VASIS, |2 |bar |Vasis, |PAPI |and |APAPI
3 |bar |VASIS |has |5 |lights, |2 |bar |has |4 |lights, |PAPI |has |4 |lights |and |APAPI |has |2 |lights
, 2 |bar |VASIS, |how |many |lights |if |you |are |on |the |glide-path
2, |the |top |two |or |Upwind |Bar |will |be |red
In |high |winds |turning |from |base |to |final |to |land |into |the |wind |there |will |be |a |visual |illusion |of
An |illusion |of |a |skid
If |a |large |aircraft |takes |off |on |a |runway |with |less |than |5 |knots |of |crosswind, |what |happens |to |
the |wing |vortices
They |remain |stationary |for |up |to |several |minutes
How |do |you |calculate |useful |load?
It |is |Gross |Weight |- |Basic |Empty |Weight
With |the |same |weight |and |power |setting, |which |aircraft |will |have |a |higher |cruise |speed, |one |
with |forward |or |aft |CoG
Aft |C |of |G |will |go |faster |due |to |less |drag
What |are |standard |rate |females |and |males
Standard |Weight |Male |Summer |-- |206
Standard |Weight |Male |Winter |-- |212
Standard |Weight |Female |Summer |-- |172
Standard |weight |female |winter |-- |178
Children |2-11 |-- |75
Infants |-- |30
What |is |the |best |angle |for |maximum |range
Lift/Drag |is |maximized
What |is |the |maximum |speed |for |lowering |landing |gear
Vlo
If |you |have |ice |on |lifting |and |control |surfaces |that |is |like |coarse |sandpaper |how |does |that |
affect |the |aeroplane
Loss |of |lift |of |30% |increase |in |drag |of |40%
A |gyrosin |compass |system |is
a |gyro |that |needs |electrical |power |and |sends |compass |signals |to |heading |indicators |RMI's |and |
other |instruments
Answers
If |an |airplane |stalls |in |a |coordinated |climbing |right |turn
left |wing |stalls |first, |leading |to |an |incipient |spin |to |the |left |-- |e.g., |upper |wing |stalls |first |
causing |the |wing |to |drop |and |spin |to |the |left
What |marshalling |signal |has |arms |extended |at |elbows |and |wands |moving |up |and |down |from |
chest |height |to |head |height
Move |Forward
If |oil |pressure |is |lost |in |a |hydraulic, |non |counterweight, |constant |speed |propeller
The |propeller |will |move |to |full |fine
The |fuel-air |ratio |for |best |power |is
14 |parts |air |to |1 |part |fuel |by |WEIGHT
If |a |turn |coordinator |indicates |needle |right |(Rate |1 |turn) |ball |left, |what |is |the |correct |actiion
In |this |case |you |could |slow |the |aircraft |down |that |would |increase |the |rate |1 |turn |angle |and |
therefore |undo |the |skid.
In |a |free |turbine |engine, |are |the |compressor |and |power |turbines |connected?
No |... |this |is |why |the |exhaust |of |the |power |turbine |is |in |the |front
Which |enhances |stability, |Dihedral |or |washout |Washout
Dihedral
Approaching |on |a |3 |degree |approach |with |a |3 |bar |basis, |the |middle |bar |will |appear(red/white)
|to |a |wide |bodied |airplane |and |(red/white) |to |a |small |aircraft?
For |the |large |aircraft |-- |WHITE, |for |the |small |aircraft |-- |RED
How |many |lights |for |each |3 |bar |VASIS, |2 |bar |Vasis, |PAPI |and |APAPI
3 |bar |VASIS |has |5 |lights, |2 |bar |has |4 |lights, |PAPI |has |4 |lights |and |APAPI |has |2 |lights
, 2 |bar |VASIS, |how |many |lights |if |you |are |on |the |glide-path
2, |the |top |two |or |Upwind |Bar |will |be |red
In |high |winds |turning |from |base |to |final |to |land |into |the |wind |there |will |be |a |visual |illusion |of
An |illusion |of |a |skid
If |a |large |aircraft |takes |off |on |a |runway |with |less |than |5 |knots |of |crosswind, |what |happens |to |
the |wing |vortices
They |remain |stationary |for |up |to |several |minutes
How |do |you |calculate |useful |load?
It |is |Gross |Weight |- |Basic |Empty |Weight
With |the |same |weight |and |power |setting, |which |aircraft |will |have |a |higher |cruise |speed, |one |
with |forward |or |aft |CoG
Aft |C |of |G |will |go |faster |due |to |less |drag
What |are |standard |rate |females |and |males
Standard |Weight |Male |Summer |-- |206
Standard |Weight |Male |Winter |-- |212
Standard |Weight |Female |Summer |-- |172
Standard |weight |female |winter |-- |178
Children |2-11 |-- |75
Infants |-- |30
What |is |the |best |angle |for |maximum |range
Lift/Drag |is |maximized
What |is |the |maximum |speed |for |lowering |landing |gear
Vlo
If |you |have |ice |on |lifting |and |control |surfaces |that |is |like |coarse |sandpaper |how |does |that |
affect |the |aeroplane
Loss |of |lift |of |30% |increase |in |drag |of |40%
A |gyrosin |compass |system |is
a |gyro |that |needs |electrical |power |and |sends |compass |signals |to |heading |indicators |RMI's |and |
other |instruments
