CAAP PPL Knowledge Exam study materials
CAAP PPL Knowledge Exam study resources

CAAP PPL Knowledge Exam flashcards

CAAP PPL Knowledge Exam · 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.

QNH
Altimeter setting that makes the instrument read elevation above mean sea level when on the ground at the reporting station; used below the transition altitude for terrain clearance.
Critical angle of attack
The angle of attack at which the wing reaches maximum lift coefficient; exceeding it causes a stall regardless of airspeed, attitude, or aircraft mass.
Mayday call
International distress signal spoken three times, followed by callsign, nature of distress, position, altitude, and intentions; indicates grave and imminent danger requiring immediate assistance.
Semi-circular rule
Cruising level rule based on magnetic track: 000-179 degrees uses odd thousands, 180-359 degrees uses even thousands, with 500-foot increments for VFR at or above 3,000 feet AGL.
Density altitude
Pressure altitude corrected for non-standard temperature, approximated as pressure altitude plus 120 times the difference between actual and ISA temperature in degrees Celsius; higher values reduce performance.
Centre of gravity
Point where the aircraft's total weight acts; computed as total moment divided by total mass, and must remain within forward and aft limits throughout the flight for controllability.
Induced drag
Drag caused by the generation of lift, proportional to the square of the lift coefficient and inversely proportional to the square of airspeed; it decreases as speed increases.
Carburettor icing
Ice formation in the carburettor venturi caused by fuel vaporisation and pressure drop cooling; most likely at ambient temperatures between about minus 7 and plus 21 degrees Celsius with high humidity.
VOR radial
Magnetic bearing from a VOR station, selected with the omni-bearing selector; the course deviation indicator centres when the aircraft is on that radial.
Relative bearing
Angle measured clockwise from the aircraft's heading to the direction of a radio station; adding it to the magnetic heading gives the magnetic bearing to the station.
Class 2 medical certificate
Minimum medical certification for a private pilot licence, confirming fitness to fly; it must be valid on the day of flight and is issued under PCAR Part 2.
Hypoxia
Insufficient oxygen supply to body tissues, causing euphoria, impaired judgement, headache, and cyanosis; time of useful consciousness falls rapidly above 25,000 feet.
Spatial disorientation
Failure to perceive the aircraft's attitude or motion correctly, producing illusions such as the leans and graveyard spiral; the remedy is to rely on flight instruments.
Advection fog
Fog formed when warm, moist air moves over a colder surface and is cooled below its dewpoint; common over sea and coastal areas and can persist through the day.
METAR
Routine aerodrome weather observation issued at scheduled times, reporting wind, visibility, weather, cloud, temperature, dewpoint, and QNH; SPECI is a special non-routine observation.
1-in-60 rule
A one-degree angular error produces a one nautical mile offset after 60 nautical miles; used to calculate track corrections and closing angles during navigation.
Variation
Angular difference between true north and magnetic north at a given location, shown on charts as east or west; magnetic heading equals true heading minus easterly variation.
Squawk 7600
Transponder code indicating radio communication failure; the pilot continues under VFR, remains clear of controlled airspace, and lands at the nearest suitable aerodrome.
Wake turbulence
Wingtip vortices generated by lift, strongest when the aircraft is heavy, clean, and slow; avoid by taking off before the rotation point and landing after touchdown point.
Engine failure after take-off
Emergency requiring immediate pitch for best glide speed, selection of a landing area, attempted restart, and a controlled forced landing; turn back only if altitude and conditions permit.
Load factor
Ratio of lift to weight; a level 60-degree bank produces a load factor of two and increases stall speed by about 41 percent; limits are shown on the V-n diagram.
Ground effect
Reduction in induced drag and increase in lift when flying within about one wingspan of the ground, causing floating during landing and reduced climb performance after take-off.
Moment
Product of a mass and its arm measured from the datum; summing moments and dividing by total mass gives the centre of gravity position for mass and balance calculations.
Altimeter setting QFE
Pressure setting that makes the altimeter read height above a specified reference point, often aerodrome elevation; used in some approach and aerodrome procedures.
Magnetic compass deviation
Aircraft-specific error caused by magnetic fields from the airframe and electrical systems; it is recorded on a compass correction card and applied to magnetic heading.
Pan-Pan call
Urgency signal spoken three times, used for a serious but not immediately life-threatening situation, followed by callsign, nature of urgency, position, and intentions.
ILS glideslope
Vertical guidance component of the instrument landing system, transmitted in the 329.15 to 335 MHz band and typically set to a three-degree descent path.
DME slant range
Distance measured by the distance measuring equipment, which is line-of-sight range rather than ground distance; error is greatest at high altitude and close to the station.
PPL privileges
A private pilot may act as pilot-in-command or co-pilot of a non-revenue aeroplane and carry passengers, but may not fly for compensation or hire.
Hyperventilation
Excessive breathing that lowers carbon dioxide in the blood, causing dizziness, tingling, and muscle spasms; treatment is controlled breathing and reassurance.
Standard atmosphere
Model with sea-level temperature 15 degrees Celsius, pressure 1013.25 hPa, and a lapse rate of about 1.98 degrees Celsius per 1,000 feet up to the tropopause.
Crosswind component
Component of wind perpendicular to the runway, calculated as wind speed times the sine of the angle between wind and runway; compare with the aircraft demonstrated limit.