ATPL principles of flight 081: practice questions and syllabus
Principles of flight is ATPL paper 081: subsonic and high-speed aerodynamics, stall, stability, controls, limitations, propellers, flight mechanics. Our bank has 1,335 questions on this subject, from ground effect to spoilers, by way of Mach number, deep stall and directional stability.
- explained questions in the bank
- 1,335
- in the EASA paper
- 46 q. · 90 min
- pass mark per paper (EASA)
- 75 %
What the syllabus covers
The topics of the EASA syllabus for this subject, with what each one lists.
081 01Subsonic aerodynamics
basic laws and definitions, two-dimensional airflow about an aerofoil, coefficients, three-dimensional airflow, total drag, ground effect, relation between lift coefficient and speed, high-lift devices, aerodynamic degradation.
081 02High-speed aerodynamics
speeds, shock waves, effects of exceeding the critical Mach number (MCRIT), means to influence MCRIT.
081 03Stall, Mach tuck, upset prevention and recovery
the stall, buffet onset boundary, situations in which buffet or stall can occur, stall recognition.
081 04Stability
static and dynamic stability, longitudinal, static directional and lateral stability, dynamic lateral and directional stability.
081 05Control
pitch, yaw and roll control, roll–yaw interaction, means to reduce control forces, fly-by-wire, trimming.
081 06Limitations
operating limitations, manoeuvring envelope, gust envelope.
081 07Propellers
conversion of engine torque to thrust, engine failure, power absorption, secondary effects of propellers.
081 08Flight mechanics
forces acting on the aeroplane, asymmetric thrust, significant points of the polar curve.
Source: EASA, Easy Access Rules for Aircrew (AMC to Part-FCL)
The illustrated course
To understand before you answer: 14 chapters and 136 key points, 136 of them with a diagram or an illustration. The first chapter, « Basics: physical laws, air and airspeeds », is free to read.
- Basics: physical laws, air and airspeeds
- The aerofoil, the wing and lift
- The boundary layer and separation
- Drag, the polar curve and ground effect
- High-lift devices, spoilers and speed brakes
- The stall and stall protection
- High-speed aerodynamics
- Flight envelope at altitude and buffeting
- Longitudinal stability
- Directional stability and lateral stability
- Flight controls and trimming
- Load factor, limitations and gusts
- Propellers
- Flight mechanics
3 questions to practise
Taken from the site's English bank and checked one by one. Read the question, choose your answer, then open the explanation. Like every explanation on the site, they may contain errors.
Question 1 · 081 01 Subsonic aerodynamics
The lift force, acting on an aerofoil :
- Ais mainly caused by overpressure at the underside of the aerofoil.
- Bis maximum at an angle of attack of 2 degrees.
- Cincreases, proportional to the angle of attack until 40 degrees.
- Dis mainly caused by suction on the upperside of the aerofoil.
Show the answer+
Answer: D. is mainly caused by suction on the upperside of the aerofoil.
Lift is mainly caused by reduced (suction) pressure on the aerofoil's upper surface.
Question 2 · 081 02 High-speed aerodynamics
Some aeroplanes have a 'waist' or 'coke bottle' contoured fuselage. This is done to
- Aapply area rule.
- Bimprove the low speed characteristics.
- Cfit the engine intakes better to the fuselage.
- Dincrease the strength of the wing root junction.
Show the answer+
Answer: A. apply area rule.
A 'coke-bottle' waisted fuselage shape applies the area rule, smoothing the aircraft's total cross-sectional area distribution to reduce transonic wave drag.
Question 3 · 081 04 Stability
Sensitivity for spiral dive will occur when :
- Athe dutch roll tendency is too strongly suppressed by the yaw damper.
- Bthe static directional stability is positive and the static lateral stability is relatively weak.
- Cthe static directional stability is negative and the static lateral stability is positive.
- Dthe static lateral and directional stability are both negative.
Show the answer+
Answer: B. the static directional stability is positive and the static lateral stability is relatively weak.
Spiral instability appears when directional (weathercock) stability is strong and lateral stability (dihedral effect) is weak. After a disturbance the nose follows the sideslip and the bank increases, leading into a steepening spiral dive.
9 more free questions, no sign-up: Free ATPL principles of flight questions
How to approach this subject
Learn the qualitative relations: ground effect reduces induced drag, stall speed increases with mass, T-tails are prone to deep stall, directional stability is about the normal axis. Also redo the simple calculations: Mach = TAS / speed of sound, load factor in a turn.
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