PRIVATE PILOT STAGE 1 NEWEST EXAM
2025 WITH MULTIPLE CHOICE
QUESTIONS AND DETAILED SOLVED
SOLUTIONS ALREADY GRADED A+ AND
100% GUARANTEE PASS (JUST
RELEASED!!!!!!!!)
Excessive cylinder head and engine oil temperatures can be
caused by - THE CORRECT ANSWER-using a lower-than-normal fuel
grade.
The three pressure instruments connected to the pitot-static
system are the - THE CORRECT ANSWER-airspeed indicator, altimeter,
and vertical speed indicator.
According to the markings on the accompanying airspeed
indicator, what is the maximum speed with flaps fully
extended? - THE CORRECT ANSWER-85 knots (white arc)
Assume that you land at an airport with the altimeter set to
29.92 instead of the current setting of 30.00. What will the
altimeter read if the field elevation is 2,000 feet MSL? - THE
CORRECT ANSWER-2,080 feet MSL (10 feet per .01 in. Hg.)
The turn coordinator provides a direct indication of aircraft -
THE CORRECT ANSWER-rate of turn.
, The attitude indicator reflects the airplane's movement about
the - THE CORRECT ANSWER-longitudinal and lateral axes.
How often should you check the heading indicator and align it
with the magnetic compass? - THE CORRECT ANSWER-Every 15
minutes
After departing runway 36, you make a left turn to a heading of
180º. If the magnetic compass initially indicates a turn in the
opposite direction, you should know that this reaction is - THE
CORRECT ANSWER-normal for all magnetic compasses under similar
conditions. (magnetic dip)
What two conditions normally cause an increase in lift? - THE
CORRECT ANSWER-Increased angle of attack and increased speed
What causes the separation of air over the wing during a stall? -
THE CORRECT ANSWER-The angle formed by the wing chord line and
the relative wind is excessive, regardless of airspeed or altitude.
How are the lift and drag components of the wing affected when
you lower the flaps? - THE CORRECT ANSWER-Both lift and drag
increase
Wingtip vortices contribute to the production of - THE CORRECT
ANSWER-induced drag.
What are the control characteristics of an aircraft with the CG
forward of limits? - THE CORRECT ANSWER-Very stable pitch,
2025 WITH MULTIPLE CHOICE
QUESTIONS AND DETAILED SOLVED
SOLUTIONS ALREADY GRADED A+ AND
100% GUARANTEE PASS (JUST
RELEASED!!!!!!!!)
Excessive cylinder head and engine oil temperatures can be
caused by - THE CORRECT ANSWER-using a lower-than-normal fuel
grade.
The three pressure instruments connected to the pitot-static
system are the - THE CORRECT ANSWER-airspeed indicator, altimeter,
and vertical speed indicator.
According to the markings on the accompanying airspeed
indicator, what is the maximum speed with flaps fully
extended? - THE CORRECT ANSWER-85 knots (white arc)
Assume that you land at an airport with the altimeter set to
29.92 instead of the current setting of 30.00. What will the
altimeter read if the field elevation is 2,000 feet MSL? - THE
CORRECT ANSWER-2,080 feet MSL (10 feet per .01 in. Hg.)
The turn coordinator provides a direct indication of aircraft -
THE CORRECT ANSWER-rate of turn.
, The attitude indicator reflects the airplane's movement about
the - THE CORRECT ANSWER-longitudinal and lateral axes.
How often should you check the heading indicator and align it
with the magnetic compass? - THE CORRECT ANSWER-Every 15
minutes
After departing runway 36, you make a left turn to a heading of
180º. If the magnetic compass initially indicates a turn in the
opposite direction, you should know that this reaction is - THE
CORRECT ANSWER-normal for all magnetic compasses under similar
conditions. (magnetic dip)
What two conditions normally cause an increase in lift? - THE
CORRECT ANSWER-Increased angle of attack and increased speed
What causes the separation of air over the wing during a stall? -
THE CORRECT ANSWER-The angle formed by the wing chord line and
the relative wind is excessive, regardless of airspeed or altitude.
How are the lift and drag components of the wing affected when
you lower the flaps? - THE CORRECT ANSWER-Both lift and drag
increase
Wingtip vortices contribute to the production of - THE CORRECT
ANSWER-induced drag.
What are the control characteristics of an aircraft with the CG
forward of limits? - THE CORRECT ANSWER-Very stable pitch,