Mauritius DCA PPL Theory flashcards
Mauritius DCA PPL Theory · 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.
- VFR minimum visibility above 3 050 m
- In controlled airspace at or above 3 050 m AMSL, VFR requires 8 km flight visibility and cloud separation of 1 500 m horizontally and 300 m vertically.
- Semi-circular rule
- Magnetic tracks 000 to 179 degrees use odd flight levels and 180 to 359 degrees use even flight levels, so opposite-direction traffic is separated by 1 000 ft.
- Steady red light signal
- A steady red light directed at an aircraft on the ground means stop; in the air it means give way to other traffic and continue circling.
- Aircraft must carry documents
- Certificate of registration, certificate of airworthiness, crew licences, journey log and radio licence where radio is fitted must be carried on board.
- Alternator failure indication
- A zero or negative ammeter reading with an illuminated warning light indicates alternator failure; the battery then supplies limited power and non-essential loads should be shed.
- Magneto drop limits
- During the run-up, each magneto should not drop more than 150 RPM and the difference between the two magnetos should not exceed 50 RPM.
- Static pressure blockage
- With the static source blocked, the altimeter freezes at its last reading, the VSI reads zero, and the ASI behaves like an altimeter in climb or descent.
- Carburettor icing range
- Carburettor icing is most likely between about 0 and 15 degrees C with high humidity; applying carburettor heat usually causes an initial RPM drop before recovery.
- Detonation versus pre-ignition
- Detonation is explosive uncontrolled combustion after the spark, raising cylinder pressure and temperature; pre-ignition is ignition before the spark, often from a hot spot.
- Density altitude formula
- Density altitude equals pressure altitude plus 120 ft for every degree Celsius that the actual temperature exceeds the ISA temperature at that level.
- Crosswind component
- The crosswind component equals wind speed multiplied by the sine of the angle between the wind direction and the runway centreline.
- Centre of gravity calculation
- Total moment is the sum of each item's weight multiplied by its arm; CG position is total moment divided by total weight and must lie within the limits.
- VFR final reserve fuel
- For VFR flight, the final reserve is fuel for 30 minutes at holding speed at 1 500 ft above the aerodrome in ISA conditions.
- Pressure altitude from QNH
- Pressure altitude equals indicated altitude plus 30 ft for each hectopascal that QNH is below 1013.25, and minus 30 ft for each hectopascal above.
- Time of useful consciousness
- At FL 250, time of useful consciousness after loss of cabin pressure is about 3 to 5 minutes; it falls to 15 to 30 seconds at FL 430.
- Hyperventilation treatment
- Hyperventilation causes dizziness, tingling and cramps; treatment is to slow the breathing rate and, if hypoxia cannot be excluded, use 100 percent oxygen.
- Somatogravic illusion
- Linear acceleration is misperceived as a climb, so the pilot may pitch down; deceleration is misperceived as a descent, so the pilot may pitch up.
- Night vision and rods
- Rods provide night vision, are absent from the fovea so central vision is poor at night, and need about 30 minutes of dark adaptation.
- ISA standard values
- ISA assumes sea level temperature of 15 degrees C, pressure 1013.25 hPa, and a lapse rate of 2 degrees C per 1 000 ft up to 11 km.
- QNH versus QFE
- QNH set on the subscale makes the altimeter read altitude above mean sea level; QFE makes it read height above the aerodrome reference point.
- Cold front passage
- A cold front brings a rapid wind veer, temperature drop, pressure rise, squall lines and thunderstorms, with improving visibility after passage.
- Microburst recovery
- In a microburst, apply maximum power, pitch for the go-around attitude and accept the airspeed loss; do not chase the airspeed with pitch.
- Aircraft icing temperature range
- Structural icing is most likely between 0 and minus 20 degrees C in visible moisture; clear ice forms from large droplets, rime ice from small supercooled droplets.
- Variation versus deviation
- Variation is the angle between true north and magnetic north at a location; deviation is the error in the aircraft compass caused by its own magnetic fields.
- 1-in-60 rule
- A track error of 1 degree over 60 NM puts the aircraft 1 NM off track, so a 10 degree error gives 10 NM in 60 NM.
- VOR radial versus bearing
- A VOR radial is the magnetic bearing from the station, while the bearing to or from the aircraft is shown on the omni-bearing selector or HSI.
- Great circle versus rhumb line
- The great circle is the shortest distance between two points; the rhumb line keeps a constant track and is longer except on the equator or a meridian.
- Distress and urgency calls
- MAYDAY repeated three times announces distress; PAN PAN repeated three times announces urgency. Both are followed by call sign, position and intentions.
- Emergency transponder codes
- Squawk 7700 for emergency, 7600 for radio failure, and 7500 for unlawful interference; 7000 is the standard VFR conspicuity code in Europe.
- Engine failure after take-off
- Pitch for best glide speed, land ahead within about 30 degrees of the runway heading, and do not turn back below a safe height.
- Load factor in a level turn
- Load factor equals one divided by the cosine of the bank angle, so 60 degrees of bank gives 2 g and raises stall speed by about 41 percent.
- Adverse yaw
- Adverse yaw is yaw away from the turn caused by increased drag on the down-going aileron; it is countered by applying rudder into the turn.