NCAA Namibia PPL Theory flashcards
NCAA Namibia PPL Theory · Build recall with a focused review session.
37 cards. Read the term and the definition here. The deck at the top of this page is optional.
- Namibia Civil Aviation Act
- The Civil Aviation Act (Act 6 of 2016) establishes the Namibia Civil Aviation Authority and the legal framework for aviation regulation, safety oversight, and enforcement in Namibia.
- NCAR Part 61
- Namibian Civil Aviation Regulation Part 61 governs personnel licensing, including PPL requirements, privileges, ratings, and medical certificate validity for pilots.
- PPL minimum flight hours
- A Private Pilot Licence (Aeroplane) requires at least 45 hours total flight time, including 25 hours dual instruction and 10 hours solo flight under Part 61.
- PPL privilege limits
- A PPL holder may act as pilot-in-command of an aeroplane in non-commercial operations but may not carry passengers for remuneration or engage in commercial air transport.
- Class 2 medical
- A Class 2 medical certificate is the minimum required to exercise PPL privileges; it must be valid on the day of flight and is subject to periodic renewal.
- Four-stroke engine cycle
- The reciprocating engine operates on induction, compression, combustion, and exhaust strokes; the crankshaft converts reciprocating motion into rotation while the camshaft operates valves.
- Carburettor icing conditions
- Carburettor icing is most likely at ambient temperatures between about -10 °C and +20 °C with high humidity, and can occur in clear air with no visible moisture.
- Static port blockage
- A blocked static port causes the airspeed indicator to behave like an altimeter and the vertical speed indicator to freeze, while the altimeter reading becomes unreliable.
- Magnetos and ignition
- Magnetos are engine-driven, self-contained ignition sources; the engine runs on two independent magnetos, and the run-up magneto check verifies each circuit separately.
- Flap effects
- Flaps increase lift and drag and lower stall speed, permitting steeper approaches and shorter landing rolls, but extended flaps reduce climb performance after take-off.
- Density altitude formula
- Density altitude equals pressure altitude plus 120 times the difference between actual and ISA temperature; high density altitude reduces power, thrust, and lift.
- Take-off distance required
- Take-off distance required is the ground roll plus distance to 50 ft; it increases with mass, altitude, temperature, tailwind, and upslope and must not exceed the available distance.
- Centre of gravity limits
- The CG must remain within forward and aft limits; forward CG increases stability and pitch force, while aft CG reduces stability and may impair spin recovery.
- Crosswind component
- The crosswind component equals wind speed multiplied by the sine of the angle between wind and runway; it must not exceed the aircraft's demonstrated crosswind limit.
- Weight and balance moment
- Moment equals mass multiplied by arm; total moment divided by total mass gives the CG position, which must lie within the loading envelope.
- Hypoxia symptoms
- Hypoxia impairs judgement and may cause euphoria and cyanosis; time of useful consciousness decreases rapidly with altitude, so oxygen and descent are the correct responses.
- Spatial disorientation
- Spatial disorientation occurs when visual cues conflict with vestibular inputs, especially in IMC and at night; the remedy is to trust the flight instruments.
- Carbon monoxide poisoning
- Carbon monoxide from exhaust leaks is odourless and causes headache, drowsiness, and confusion; cabin heat sources are common origins and a detector is the reliable safeguard.
- Yerkes-Dodson curve
- The Yerkes-Dodson curve shows that performance improves with arousal up to an optimum point, after which excessive stress impairs judgement, reaction time, and motor control.
- Standard atmosphere values
- The ISA defines sea level pressure of 1013.25 hPa and temperature of 15 °C, with a tropospheric lapse rate of about 2 °C per 1 000 ft.
- Cumulonimbus hazards
- Cumulonimbus clouds contain severe turbulence, icing, hail, lightning, and microbursts; they require moisture, instability, and a lifting trigger and should be avoided widely.
- QNH and QFE
- QNH is the altimeter setting that indicates altitude above mean sea level, while QFE indicates height above the aerodrome reference datum.
- CAVOK meaning
- CAVOK indicates visibility of at least 10 km, no cloud below 5 000 ft or below the highest minimum sector altitude, and no significant weather phenomena.
- Wind triangle
- The wind triangle combines true heading and true airspeed with wind velocity to derive track and groundspeed; drift is the angle between heading and track.
- One in sixty rule
- The 1-in-60 rule states that a course error of one degree produces about one nautical mile of offset per 60 nautical miles flown, useful for estimating corrections.
- Magnetic variation rule
- Magnetic heading equals true course minus variation, using "east is least, west is best"; deviation from aircraft compass error is then applied separately.
- VOR radial
- A VOR radial indicates the magnetic bearing from the station to the aircraft; DME provides slant range, which exceeds ground distance at high altitude.
- Engine failure after take-off
- After engine failure, maintain control, pitch for best glide speed, select a landing area, attempt a restart per checklist, and brief passengers on the emergency.
- Wake turbulence avoidance
- Wake vortices are strongest from heavy, clean, slow aircraft; avoid them by spacing, flying above the preceding aircraft's path, and landing beyond its touchdown point.
- Radio failure code
- On radio failure, squawk 7600, follow the published lost-communication procedure, maintain VFR, and land at the nearest suitable aerodrome.
- Load factor in turns
- Load factor equals one divided by the cosine of the bank angle in a level turn; a 60-degree bank gives a load factor of two and increases stall speed by 41 percent.
- Critical angle of attack
- The critical angle of attack is the angle between the chord line and relative airflow at which the wing stalls; stall speed increases with mass and load factor.
- Induced and parasite drag
- Induced drag decreases with increasing speed while parasite drag increases with speed squared; total drag is minimum at the speed for best lift-to-drag ratio.
- MAYDAY call
- A MAYDAY call, repeated three times, signals distress and is followed by station, aircraft identification, nature of emergency, position, altitude, and intentions.
- Read-back requirement
- Pilots must read back clearances, runway and hold-short instructions, altimeter settings, and frequency changes, repeating them exactly and asking for clarification if unsure.
- Squawk codes
- Standard transponder codes are 7700 for emergency, 7600 for radio failure, and 7500 for unlawful interference, as defined by ICAO procedures.
- Standard position report
- A position report includes station called, aircraft identification, position, time, altitude, and next position with estimated time, spoken concisely in standard phraseology.