EASA ATPL021 aircraft general knowledge foundations study materials
EASA ATPL021 aircraft general knowledge foundations study resources

EASA ATPL021 aircraft general knowledge foundations flashcards

EASA ATPL021 aircraft general knowledge foundations · Build recall with a focused review session.

20 cards. Read the term and the definition here. The deck at the top of this page is optional.

Limit load
A design load associated with the maximum expected service condition, distinguished from an unrestricted promise that any repeated loading or damage is harmless.
Damage tolerance
A design and inspection approach considering the presence and growth of damage before it reaches a critical structural condition.
Mass balance
Control-surface mass distribution used to address inertial effects and flutter susceptibility, distinguished from aerodynamic assistance to the hinge moment.
Anti-servo tab
A tab moving with a stabilator’s trailing-edge direction in the relevant design to increase control feel, rather than merely reduce every pilot force.
Anti-skid
A braking-control function responding to wheel behavior to reduce a developing skid, without removing runway, tire or brake-energy limitations.
Hydraulic actuator
A device converting hydraulic pressure acting over an effective area into mechanical force or movement under the actual circuit conditions.
Accumulator
A system component storing hydraulic energy through a compressible element, with capacity and use determined by its charge and installation.
Power transfer unit
A device transferring mechanical power between suitable hydraulic circuits, distinguished from mixing their fluid or creating a new independent energy source.
Outflow valve
A valve regulating cabin air escape as part of pressurization control, distinguished from a component directly setting aircraft geometric altitude.
Inverter
An electrical conversion device producing AC from DC, distinguished from a rectifier that converts in the other direction.
Detonation
Abnormal end-gas combustion associated with damaging pressure behavior, distinguished from combustion beginning before the intended spark through a hot ignition source.
Wastegate
A valve controlling exhaust flow through a turbocharger turbine, influencing boost rather than directly selecting a propeller’s blade angle.
Compressor surge
A major breakdown of the intended compressor airflow, distinguished from an ordinary commanded thrust change or merely reduced fuel quantity.
Constant-speed governor
A control changing propeller blade angle within its governing range to maintain a selected rotational speed as operating load changes.
Feathering
A high-blade-angle configuration intended to reduce drag from an inoperative propeller, distinct from ordinary cruise pitch or a low-pitch windmilling condition.
Usable fuel
The quantity available for the intended engine supply under the approved definition, distinguished from total capacity or an automatic legal reserve allowance.
Crossfeed
A fuel-system path enabling an alternative engine-feed arrangement in the actual design, not necessarily a tank-transfer or equalization function.
Ullage
The space above liquid fuel in a tank, whose gas composition is relevant to the purpose of a fuel-tank inerting system.
Anti-icing
A protective method intended to prevent ice formation under specified conditions, distinguished from removing ice that has already accumulated.
Chemical oxygen generator
An oxygen source using a chemical reaction after activation, with equipment-specific supply and heat characteristics unlike a simple stored-gas bottle.