DGCA CPL Technical General study materials
DGCA CPL Technical General study resources

DGCA CPL Technical General flashcards

DGCA CPL Technical General · Build recall with a focused review session.

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

Semi-monocoque structure
Aircraft structure in which the stressed skin carries most shear and tension loads, while stringers resist bending and frames maintain the fuselage shape.
Fail-safe structure
A design philosophy in which a component failure is contained by alternate load paths, allowing the aircraft to continue safely until the damaged part is detected and repaired.
Primary flight controls
Ailerons control roll, elevators control pitch, and the rudder controls yaw; these are the surfaces essential for manoeuvring the aircraft.
Wing spar
The main structural member of a wing that carries bending and shear loads from the wing to the fuselage; ribs attach to it to maintain aerofoil shape.
Cabin outflow valve
A valve that regulates the rate of air leaving the pressurised cabin, thereby controlling cabin altitude and differential pressure in response to the pressure controller.
Differential aileron
A linkage that deflects the upward-moving aileron more than the downward-moving one, reducing adverse yaw by creating more drag on the rising wing.
Four-stroke cycle
The operating cycle of a reciprocating engine with intake, compression, power and exhaust strokes, requiring two crankshaft revolutions to complete one cycle.
Detonation
Uncontrolled explosive combustion of the fuel-air mixture after normal spark ignition, causing high cylinder pressure, rising CHT and possible piston damage.
Pre-ignition
Ignition of the fuel-air mixture before the spark plug fires, often caused by a hot spot or glowing carbon deposit, leading to power loss and overheating.
Constant-speed propeller
A propeller whose blade angle is automatically adjusted by a governor to maintain a selected engine RPM as airspeed and power change.
Propeller slip
The difference between the theoretical forward distance a propeller would advance in one revolution and the actual distance travelled through the air.
Compressor surge
A violent reversal of airflow through a turbine compressor, often caused by excessive power at low RPM, producing loud bangs, high EGT and possible flameout.
Pitot-static system
A system that supplies total pressure from the pitot tube and static pressure from the static port to the airspeed indicator, altimeter, vertical speed indicator and Machmeter.
Altimeter subscale
The pressure-setting window on an altimeter; setting QNH makes it read altitude above mean sea level, while QFE makes it read height above a reference point.
Standard-rate turn
A turn through 3 degrees per second, completing 180 degrees in one minute; indicated by the turn coordinator at the standard-rate mark.
Heading indicator
A gyroscopic instrument that displays aircraft heading; it is not north-seeking and must be periodically aligned with the magnetic compass during straight-and-level flight.
Radio altimeter
An instrument that measures absolute height above the terrain by timing reflected radio waves; it is used for low approach and ground proximity warning, not en-route altitude.
Ohm's law
The relationship V = I × R, where voltage equals current multiplied by resistance; power can be calculated as P = V × I.
Parallel circuit
A circuit in which components are connected across the same voltage; total resistance is less than the smallest branch and reciprocal resistances are summed.
Aircraft bonding
The electrical connection of metal structure and components to provide a low-resistance path for static discharge and lightning current, reducing spark and fire risk.
Magnetos
Self-contained engine-driven ignition units that generate high voltage for spark plugs independently of the aircraft battery, ensuring ignition if the electrical system fails.
ARINC 429
A widely used avionics digital data bus that transmits parameters over a differential pair using 32-bit words with labels identifying the data.
2024 aluminium alloy
A copper-bearing aluminium alloy with high strength and good fatigue resistance, often used for aircraft skins, but it has lower corrosion resistance than 6061.
Alclad
Aluminium sheet with a thin pure-aluminium cladding bonded to each surface; the cladding corrodes preferentially and protects the stronger alloy core.
Galvanic corrosion
Corrosion caused by electrical contact between dissimilar metals in the presence of an electrolyte, where the more active metal becomes anodic and corrodes.
Fatigue
Progressive cracking of a material under repeated cyclic stress, often starting at stress concentrations and growing until the remaining section fails.
Dye penetrant inspection
A non-destructive method that applies a coloured penetrant to a cleaned surface, removes excess and uses a developer to reveal surface-breaking cracks.
Bolt grip length
The unthreaded portion of a bolt shank; it must match the thickness of the parts so that threads do not bear load in the shear plane.
Lockwire
Safety wire installed through drilled fastener heads and twisted so that tension resists loosening; it must be routed so any movement tends to tighten the fastener.
Airworthiness Directive
A mandatory instruction issued by the aviation authority to correct an unsafe condition on aircraft; it must be complied with within the stated time or usage limit.
MEL
Minimum Equipment List: an approved document that allows dispatch with specified equipment inoperative, subject to conditions and repair intervals, while maintaining an acceptable safety level.
Eddy current inspection
A non-destructive test that induces electrical currents in a conductive part and detects changes caused by cracks, corrosion or variations in conductivity and thickness.