SET 2 Flashcards
You are on the ILS 09R and lose the localizer between the outer and middle marker. What do you do?
Climb immediately and fly the missed approach procedure.
Continue approach as long as you have a glideslope.
Advice ATC and continue approach.
Change approaches if possible.
Climb immediately and fly the missed approach procedure.
You are 6nm from the rwy on final, and the localizer shows 1 degree of deflection. How far from the runway course are you? .5nm .4nm .1nm .2nm
.1nm
ILS 6 MI = 1 DOT = .1
ILS 3 MI = 1 DOT = .5 I THINK
What happens in a skid?
Inside of turn, turn radius decreases, turn rate decreases.
Inside of turn, turn radius decreases, turn rate increases.
Inside of turn, turn radius increases, turn rate increases.
Inside of turn, turn radius decreases, turn rate increases.
An axial flow engine has-
High compression low efficiency.
Low compression, high efficiency.
High compression ratio, high efficiency.
High compression ratio, high efficiency.
You maintain a constant Mach and fly below the optimum cruise altitude-
Fuel burn remains the same.
Fuel burn will increase and time aloft will decrease.
Fuel burn will decrease and time aloft will decrease.
Fuel burn will increase and time aloft will increase.
Fuel burn will increase and time aloft will decrease.
If right rudder is applied in a right turn, what happens to turn radius? Rate?
Radius is increased, Rate is increased.
Radius is decreased, Rate is increased.
Radius is decreased, Rate is decreased.
Radius is decreased, Rate is increased.
You are at the aircraft load limit. What will NOT cause you to exceed the load limit? Increase in speed. Increase in G. Increase of weight. Increase in AOB.
Increase of weight.
If you blow your right tire on landing, what happens to your landing distance?
Decreases.
Increases.
Remains the same.
Increases.
LOSE AN EXTRA BRAKE TO HELP STOP YOU
You are flying at FL370 in cruise flight, and the OAT increases 5 degrees C, and the headwind increases 5kts. What happens to your TAS and GS?
TAS increases by 4kts, therefore GS increases by 1kt.
TAS increases by 6kts, therefore GS increases by 1kt.
TAS increases by 10kts, therefore GS increases by 1kt.
TAS increases by 6kts, therefore GS increases by 1kt.
Correct
TAS increases approx. 1.2kts/1o C increase. So 50C x 1.2kts = 6KTAS increase
6KTAS-5KTS headwind = 1kt GS increase.
When do you slow down to hold if no clearance beyond a fix has been given?
Within 3min of the fix.
Within 3 miles of the fix.
Within 5 miles of the fix.
Within 3min of the fix.
You are cleared to “taxi to runway 22 via taxiway XYZ”. Taxiway X crosses RWY 9, taxiway Y crosses runway 30. Taxiway Z ends at the departure end of 22. How do you proceed?
“Taxi via Y and hold short of RWY 9.”
“Taxi via X and hold short of RWY 9.”
“Taxi via X and hold short of RWY 22.”
“Taxi via X and hold short of RWY 9.”
YOU HAVEN’T BEEN CLEARED TO CROSS 9
Level flight, increase in Temp does what to TAS? And True Altitude?
TAS Increases, True Altitude decreases.
TAS decreases, True Altitude Increases.
TAS Increases, True Altitude Increases.
TAS Increases, True Altitude Increases.
Flying an approach to rwy 18, circle to land rwy 7 and lose sight of the rwy. You should-
Turn in the shortest direction to rwy 18 and execute the published missed approach (for rwy 7).
Turn in the longest direction to rwy 7 and execute the published missed approach (for rwy 18).
Turn in the shortest direction to rwy 7 and execute the published missed approach (for rwy 18).
Turn in the shortest direction to rwy 7 and execute the published missed approach (for rwy 18).
TURN TO THE RUNWAY YOU ARE CIRCLING 7 BUT YOU HAVE TO DO THE MAP FOR THE CHART YOU HAVE OUT 18
You are flying at FL230 and told to slow down, then descend to 12,000. RAT will-
Ram Air Temp remains the same.
Ram Air Temp increases.
Ram Air Temp will decrease.
Ram Air Temp will decrease.
Correct
There are two types of air temperature measurements on aircraft, Ram Air Temperature and Static Air Temperature. (slower aircraft don’t normally have RAT gages) Ram Air Temperature, sometimes known as Total Air Temperature, is the air temperature outside the aircraft increased by the heat resulting from the compressibility of the air. The faster the aircraft, the more the rise in the temperature. Static Air Temperature, also known as Outside Air Temperature, is a temperature reading corrected for the compressibility rise to give a true outside air temperature which is used in all sorts of calculations relating to engine performance, aircraft speed, etc.
You are at 35000feet and suffer a rapid decompression. What is your time of useful consciousness? 5MIN. 3MIN. 2MIN. 1MIN.
1MIN.