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GROUND SCHOOL MIDTERM EXAM QUESTIONS WITH COMPLETE SOLUTIONS VERIFIED GRADED A+

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Determine the density altitude for these conditions: altimeter setting 29.25, Runway temperature +81°F, Airport elevation 5,250 MSL A: 4600 Feet MSL B: 5877 Feet MSL C: 8500 Feet MSL - ANSWERSC: 8500 Feet MSL Determine the pressure altitude at an airport that is 3,563 feet MSL with an altimeter setting of 29.96. A: 3527 feet MSL B: 3556 feet MSL C: 3639 feet MSL - ANSWERS3527 feet MSL During an approach to a stall, an increased load factor will cause the airplane to A: stall at a higher airspeed B: have a tendency to spin C: be more difficult to control - ANSWERSstall at a higher airspeed An abnormally high engine oil temperature indication may be caused by A: the oil level being too low B: operating with too high viscosity oil C: operating with excessively rich mixture - ANSWERSthe oil level being too low

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Institution
Ground School
Course
Ground school

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GROUND SCHOOL MIDTERM EXAM
QUESTIONS WITH COMPLETE
SOLUTIONS VERIFIED GRADED A+

Determine the density altitude for these conditions: altimeter setting 29.25, Runway
temperature +81°F, Airport elevation 5,250 MSL


A: 4600 Feet MSL
B: 5877 Feet MSL
C: 8500 Feet MSL - ANSWERSC: 8500 Feet MSL

Determine the pressure altitude at an airport that is 3,563 feet MSL with an altimeter
setting of 29.96.

A: 3527 feet MSL
B: 3556 feet MSL
C: 3639 feet MSL - ANSWERS3527 feet MSL

During an approach to a stall, an increased load factor will cause the airplane to

A: stall at a higher airspeed
B: have a tendency to spin
C: be more difficult to control - ANSWERSstall at a higher airspeed

An abnormally high engine oil temperature indication may be caused by

A: the oil level being too low
B: operating with too high viscosity oil
C: operating with excessively rich mixture - ANSWERSthe oil level being too low

An electrical system failure (battery and alternator) occurs during flight. In this situation,
you would?

A: experience avionics equipment failure
B: probably experience failure of the engine ignition system, fuel gauges, aircraft lighting
system, and avionics equipment.
C: probably experience failure due to the loss of the engine-driven fuel pump and also
experience failure of the radio equipment, lights, and all instruments that require
alternating current - ANSWERSexperience avionics equipment failure.

, While cruising at 9,500 feet MSL, the fuel/air mixture is properly adjusted. What will
occur if a descent to 4,500 feet MSL is made without readjusting the mixture?

A: the fuel/air mixture may become excessively lean
B: there will be more fuel in the cylinders than is needed for normal combustion, and the
excess fuel will absorb heat and cool the engine.
C: the excessively rich mixture will create higher cylinder head temperatures and may
cause detonation. - ANSWERSThe fuel/air mixture may become excessively lean.

If a pilot suspects that the engine (with a fixed-pitch propeller) is detonating during
climb-out after takeoff, the initial corrective action to take would be to?

A: lean the mixture
B: lower the nose slightly to increase airspeed
C: apply carburetor heat - ANSWERSlower the nose slightly to increase airspeed

In the northern hemisphere, a magnetic compass will normally indicate a turn toward the
north if?

A: An aircraft is decelerated while on an east or west heading
B: a left turn is entered from a west heading
C: an aircraft is accelerated while on an east or west heading - ANSWERSC. an aircraft
is accelerated while on an east or west heading.

Under what condition will pressure altitude be equal to true altitude?

A: when the atmospheric pressure is 29.92" Hg.
B: when standard atmospheric conditions exist
C: when indicated altitude is equal to pressure altitude - ANSWERSWhen standard
atmospheric conditions exist

Under what condition will true altitude be lower than indicated altitude?

A: in colder than standard air temperatures
B: in warmer than standard temperatures
C: when density altitude is higher than indicated altitude - ANSWERSIn colder than
standard air temperatures

What is the maximum wind velocity for a 30° crosswind if the maximum crosswind
component for the airplane is 12 knots?

A: 16 kts
B: 20 kts
C: 24 kts - ANSWERS24 kts

Determine the approximate landing ground roll distance.

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Institution
Ground school
Course
Ground school

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Uploaded on
May 8, 2026
Number of pages
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Written in
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Type
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