Oman CAA ATPL(A) Theory flashcards
Oman CAA ATPL(A) Theory · Build recall with a focused review session.
42 cards. Read the term and the definition here. The deck at the top of this page is optional.
- Semi-circular rule
- IFR cruising levels: magnetic tracks 000-179 use odd flight levels, 180-359 use even flight levels; RVSM applies between FL290 and FL410.
- MAYDAY vs PAN PAN
- MAYDAY is the distress call for grave and imminent danger; PAN PAN is the urgency call for urgent but non-distress situations.
- Class A airspace
- Airspace where only IFR flights are permitted and all flights receive ATC separation; VFR is not allowed.
- VMC minima above 10000 ft
- In Class C above 3050 m AMSL, VMC requires 8 km flight visibility and 1500 m horizontal, 300 m vertical distance from cloud.
- Compressor surge cause
- Excessive angle of attack of compressor blades, often from abrupt throttle changes or disturbed intake airflow, causing flow reversal and bang.
- Bleed air source
- Pressurisation and anti-ice air is normally tapped from the high-pressure compressor stage; excessive extraction reduces engine thrust margin.
- Hydraulic accumulator function
- Stores pressurised fluid to damp pressure surges, absorb thermal expansion and supply transient demand during high-load operations.
- Pitot heat failure
- Blocked or unheated pitot tube produces erroneous airspeed; static blockage affects airspeed, altitude and vertical speed together.
- QNH vs QFE
- QNH set on the subscale gives altitude above mean sea level; QFE gives height above the aerodrome reference datum.
- High-to-low pressure error
- Flying from high to low pressure without resetting the altimeter subscale causes the aircraft to be lower than indicated.
- Turn coordinator indication
- Shows rate of turn and roll attitude; the turn-and-slip indicator shows rate of turn only without roll information.
- Magnetic compass errors
- Turning and acceleration errors make the compass unreliable in manoeuvres; it is most accurate in straight, level, unaccelerated flight.
- CG shift formula
- Moving mass m by distance d shifts the CG by (m × d) / total mass; the CG moves toward the added or moved mass.
- Maximum zero-fuel mass
- Structural limit for the aircraft without usable fuel; take-off mass is MZFM plus fuel and must not exceed MTOM.
- Forward CG limit
- Set by elevator authority for rotation and landing flare; an excessively forward CG may prevent rotation or flare.
- Dry operating mass
- Basic empty mass plus crew, crew baggage, catering and unusable fuel; traffic load is added to give zero-fuel mass.
- V1 decision speed
- Speed at which a take-off must be continued after failure; before V1 a rejected take-off must be possible.
- Balanced field length
- Field length where accelerate-stop distance equals accelerate-go distance, giving the minimum required runway length.
- Density altitude effect
- Higher temperature and pressure altitude increase density altitude, reducing engine power, lift and climb performance.
- Climb gradient formula
- Climb gradient (%) = (height gained / horizontal distance) × 100; 3.3% corresponds to about 200 ft per nautical mile.
- Specific range
- Distance flown per unit fuel (NM/kg); best specific range occurs near the speed for maximum lift-to-drag ratio.
- Equal time point
- Point where time to destination equals time back to departure; equal fuel point uses fuel burn instead of time.
- Descent rate planning
- For a 3-degree path, required rate of descent in ft/min is approximately groundspeed in knots multiplied by five.
- Headwind fuel penalty
- A headwind increases trip fuel and time; the penalty is greater at lower true airspeed for a given wind component.
- Time of useful consciousness
- Duration of effective performance after loss of oxygen; falls rapidly with altitude, from minutes at FL350 to seconds at FL500.
- Hyperventilation treatment
- Reduce breathing rate and depth, reassure the patient; symptoms include dizziness, tingling and anxiety from low CO2.
- Vestibular system function
- Semicircular canals sense angular acceleration; otoliths sense linear acceleration and gravity; neither detects constant velocity.
- Night vision characteristics
- Rods provide night vision, are slow to adapt and poor at colour; bright light destroys dark adaptation for many minutes.
- ISA sea level values
- Sea level temperature 15 °C and pressure 1013.25 hPa; temperature lapse rate 1.98 °C per 1000 ft up to the tropopause.
- Cold front characteristics
- Steep slope, rapid passage, cumuliform cloud, showers, squalls and good visibility behind the front.
- Radiation fog conditions
- Forms when temperature reaches dewpoint with clear skies, light wind and high humidity, typically overnight over land.
- Great circle vs rhumb line
- Great circle is the shortest distance with continuously changing track; rhumb line maintains constant track but is longer.
- 1-in-60 rule
- Distance off track equals track error in degrees divided by 60, multiplied by distance flown; valid for small angles.
- VOR radial indication
- CDI centred with TO/FROM flag indicates the aircraft is on the selected radial; the radial is the magnetic bearing from the station.
- DME slant range
- DME measures slant range, which exceeds ground distance at high altitude and close range; error grows near the station.
- Transponder emergency codes
- 7700 for emergency, 7600 for radio failure, 7500 for hijack; Mode C transmits pressure altitude.
- Rejected take-off actions
- Close throttles, apply maximum braking, maintain directional control and use reverse thrust as available.
- Emergency descent procedure
- Don oxygen masks, descend at maximum rate to 10000 ft or MSA, notify ATC with MAYDAY and advise intentions.
- Minimum fuel declaration
- Declare minimum fuel when committed to land at a specific aerodrome and any change causes landing below final reserve.
- Lift formula
- Lift equals half rho V squared S CL; induced drag equals L squared divided by half rho V squared S pi e AR.
- Stall angle of attack
- Stall occurs at the critical angle of attack regardless of speed, mass or attitude; load factor increases stall speed by square root of n.
- Dihedral effect
- Wings set at an upward angle provide lateral stability; a sideslip produces a rolling moment restoring wings level.