ATP CTP (2025) Actual Exam Questions
and Answers A+ Graded
Which .of .the .following .statements .regarding .energy .is .true? .- .CORRECT
.ANSWER .-Kinetic .energy .can .be .traded .for .potential .energy, .and .potential
.energy .can .be .traded .for .kinetic .energy.
The .objective .in .maneuvering .the .airplane .is .to .manage .energy .so .that: .-
.CORRECT .ANSWER .-All .of .the .above .(objective .in .maneuvering .the .airplane)
What .is .the .effect .on .total .drag .if .airspeed .slows .below .L/Dmax? .- .CORRECT
.ANSWER .-Drag .increases .because .of .increased .induced .drag
A .jet .pilot .flying .at .L/Dmax .will .obtain .best: .- .CORRECT .ANSWER .-Endurance
When .a .jet .aircraft .is .flown .at .the .appropriate .airspeed .for .maximum .range,
.which .type .of .drag .predominates? .- .CORRECT .ANSWER .-Parasite
When .already .at .high .speed, .what .happens .if .Mach .is .allowed .to .increase? .-
.CORRECT .ANSWER .-All .of .the .above .(what .happens .if .Mach .is .allowed .to
.increase)
What .is .the .result .of .a .shock-induced .separation .if .airflow .occurring
.symmetrically .near .the .wing .root .of .a .swept .wing .aircraft? .- .CORRECT
.ANSWER .-A .severe .moment .or ."Mach .tuck"
The .speed .of .sound .generally .decreases .with .increasing .altitude. .This .occurs
.because: .- .CORRECT .ANSWER .-The .air .temperature .decreases
Critical .Mach .number .can .be .defined .as: .- .CORRECT .ANSWER .-The .speed .of
.an .aircraft .in .which .airflow .over .any .part .of .the .aircraft .or .structure .first
.reaches, .but .doesn't .exceed, .Mach .1.0
The .most .dynamic .stability .about .the .vertical .axis .on .modern .jet .transports .is
.from: .- .CORRECT .ANSWER .-An .active .stability .augmentation .system/yaw
.damper
Swept .wings .causes .a .significant .- .CORRECT .ANSWER .-Reduction .in
.effectiveness .of .flaps
, Why .is .convergence .of .stall .AOA .and .Mmo .hazardous? .- .CORRECT .ANSWER .-
All .of .the .above .(convergence .of .stall .AOA .hazardous)
To .maintain .altitude .in .a .banked .turn, .the .lift .produced .by .the .airplane .must .be:
.- .CORRECT .ANSWER .-Greater .than .the .airplane .weight, .and .the .amount .is .a
.function .of .bank .angle
Excessive .bank .angles .at .high .altitudes .can .be .hazardous .because .- .CORRECT
.ANSWER .-All .of .the .above
High .altitude .recovery .from .slow .flight .turning .is .best .accomplished .by: .-
.CORRECT .ANSWER .-Increasing .thrust .to .maximum .available .thrust .and
.reducing .bank .angle .while .accelerating .to .airspeed .above .L/D .max .speed. .In .a
.thrust .limited .situation, .exiting .slow .flight .will .require .an .immediate .descent .as
.an .aerodynamic .stall .is .imminent
Maximum .altitude .for .an .airplane .is: .- .CORRECT .ANSWER .-The .lowest .of .the
.above .listed .altitudes
Exceed .the .critical .angle .of .attack .and .the .surface .will .stall, .and .lift .will
.decrease .instead .of .increasing. .This .is .true: .- .CORRECT .ANSWER .-Regardless
.of .airplane .speed .or .attitude
Which .of .the .following .statements .is .true? .- .CORRECT .ANSWER .-Recovery
.from .approach .to .stall .warning .is .the .same .as .recovery .from .a .stall
The .airplane .angle .of .attack .is .the .angle .between .the .wing .chord .and .the
.oncoming .air .or .relative .wind .- .CORRECT .ANSWER .-True
Therefore, .if .a .pilot .maintains .airspeed .above .the .appropriate .speed .listed .for
.the .aircraft .weight .p, .the .aircraft .will .not .stall. .- .CORRECT .ANSWER .-False
The .stall .speed .of .an .airplane .is: .- .CORRECT .ANSWER .-Affected .by .weight .and
.bank .angle
Large .downward .aileron .deflections: .- .CORRECT .ANSWER .-Could .induce .air
.separation .over .that .portion .of .the .wing .at .very .high .angles .of .attack
Place .the .steps .from .stall .recovery .template .in .the .correct .order: .- .CORRECT
.ANSWER .-Disconnect .autopilot
Nose .down .pitch
Bank .wings .level .
Apply .thrust .
Retract .spoilers .
Return .to .flight .path
The .predominant .number .if .airplane .upsets .are .caused .by: .- .CORRECT
.ANSWER .-Environmental .factors
and Answers A+ Graded
Which .of .the .following .statements .regarding .energy .is .true? .- .CORRECT
.ANSWER .-Kinetic .energy .can .be .traded .for .potential .energy, .and .potential
.energy .can .be .traded .for .kinetic .energy.
The .objective .in .maneuvering .the .airplane .is .to .manage .energy .so .that: .-
.CORRECT .ANSWER .-All .of .the .above .(objective .in .maneuvering .the .airplane)
What .is .the .effect .on .total .drag .if .airspeed .slows .below .L/Dmax? .- .CORRECT
.ANSWER .-Drag .increases .because .of .increased .induced .drag
A .jet .pilot .flying .at .L/Dmax .will .obtain .best: .- .CORRECT .ANSWER .-Endurance
When .a .jet .aircraft .is .flown .at .the .appropriate .airspeed .for .maximum .range,
.which .type .of .drag .predominates? .- .CORRECT .ANSWER .-Parasite
When .already .at .high .speed, .what .happens .if .Mach .is .allowed .to .increase? .-
.CORRECT .ANSWER .-All .of .the .above .(what .happens .if .Mach .is .allowed .to
.increase)
What .is .the .result .of .a .shock-induced .separation .if .airflow .occurring
.symmetrically .near .the .wing .root .of .a .swept .wing .aircraft? .- .CORRECT
.ANSWER .-A .severe .moment .or ."Mach .tuck"
The .speed .of .sound .generally .decreases .with .increasing .altitude. .This .occurs
.because: .- .CORRECT .ANSWER .-The .air .temperature .decreases
Critical .Mach .number .can .be .defined .as: .- .CORRECT .ANSWER .-The .speed .of
.an .aircraft .in .which .airflow .over .any .part .of .the .aircraft .or .structure .first
.reaches, .but .doesn't .exceed, .Mach .1.0
The .most .dynamic .stability .about .the .vertical .axis .on .modern .jet .transports .is
.from: .- .CORRECT .ANSWER .-An .active .stability .augmentation .system/yaw
.damper
Swept .wings .causes .a .significant .- .CORRECT .ANSWER .-Reduction .in
.effectiveness .of .flaps
, Why .is .convergence .of .stall .AOA .and .Mmo .hazardous? .- .CORRECT .ANSWER .-
All .of .the .above .(convergence .of .stall .AOA .hazardous)
To .maintain .altitude .in .a .banked .turn, .the .lift .produced .by .the .airplane .must .be:
.- .CORRECT .ANSWER .-Greater .than .the .airplane .weight, .and .the .amount .is .a
.function .of .bank .angle
Excessive .bank .angles .at .high .altitudes .can .be .hazardous .because .- .CORRECT
.ANSWER .-All .of .the .above
High .altitude .recovery .from .slow .flight .turning .is .best .accomplished .by: .-
.CORRECT .ANSWER .-Increasing .thrust .to .maximum .available .thrust .and
.reducing .bank .angle .while .accelerating .to .airspeed .above .L/D .max .speed. .In .a
.thrust .limited .situation, .exiting .slow .flight .will .require .an .immediate .descent .as
.an .aerodynamic .stall .is .imminent
Maximum .altitude .for .an .airplane .is: .- .CORRECT .ANSWER .-The .lowest .of .the
.above .listed .altitudes
Exceed .the .critical .angle .of .attack .and .the .surface .will .stall, .and .lift .will
.decrease .instead .of .increasing. .This .is .true: .- .CORRECT .ANSWER .-Regardless
.of .airplane .speed .or .attitude
Which .of .the .following .statements .is .true? .- .CORRECT .ANSWER .-Recovery
.from .approach .to .stall .warning .is .the .same .as .recovery .from .a .stall
The .airplane .angle .of .attack .is .the .angle .between .the .wing .chord .and .the
.oncoming .air .or .relative .wind .- .CORRECT .ANSWER .-True
Therefore, .if .a .pilot .maintains .airspeed .above .the .appropriate .speed .listed .for
.the .aircraft .weight .p, .the .aircraft .will .not .stall. .- .CORRECT .ANSWER .-False
The .stall .speed .of .an .airplane .is: .- .CORRECT .ANSWER .-Affected .by .weight .and
.bank .angle
Large .downward .aileron .deflections: .- .CORRECT .ANSWER .-Could .induce .air
.separation .over .that .portion .of .the .wing .at .very .high .angles .of .attack
Place .the .steps .from .stall .recovery .template .in .the .correct .order: .- .CORRECT
.ANSWER .-Disconnect .autopilot
Nose .down .pitch
Bank .wings .level .
Apply .thrust .
Retract .spoilers .
Return .to .flight .path
The .predominant .number .if .airplane .upsets .are .caused .by: .- .CORRECT
.ANSWER .-Environmental .factors
