Bahrain CAA ATPL Theory flashcards
Bahrain CAA ATPL 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.
- Semi-circular rule
- Magnetic tracks 000-179 use odd flight levels; tracks 180-359 use even flight levels. Above FL290 VFR uses 4000 ft intervals.
- Class C airspace
- IFR separated from IFR and VFR; VFR separated from IFR and receives traffic information about other VFR. VMC minima apply.
- Squawk 7700
- The transponder code indicating an emergency. It alerts ATC to give priority and is not used for routine identification.
- Balanced field length
- The runway length where accelerate-stop distance equals accelerate-go distance, with V1 chosen to minimise required field length.
- V1
- The decision speed: below it a rejected take-off is possible; above it the take-off must continue. It is at least VMCG and at most VR.
- Second segment climb gradient
- Required climb gradient with one engine inoperative, gear up, take-off flaps: 2.4% for a twin, 2.7% for a three-engine aircraft.
- Maximum zero-fuel mass
- The maximum mass of the aircraft without usable fuel. It limits structural loads and is a separate limit from MTOM.
- Dry operating index
- A moment-based index for the aircraft's empty mass and crew, used with load indices on the load sheet to compute final CG.
- Blocked pitot tube
- With total pressure trapped, the ASI behaves like an altimeter: it indicates increasing speed in a climb and decreasing speed in a descent.
- Turn coordinator
- A rate gyro instrument displaying rate of turn and roll. It is not an attitude indicator and does not show pitch.
- Radio altimeter
- Measures height above terrain using frequency modulation. Valid only at low altitude; used for approach callouts and automatic landing.
- Hypoxia time of useful consciousness
- At FL350 after rapid decompression, useful consciousness lasts about 30-60 seconds. Oxygen must be applied immediately.
- Somatogravic illusion
- During acceleration, the otolith organs signal a pitch-up sensation. The pilot may incorrectly lower the nose during take-off.
- Inverted-U stress curve
- Performance improves with moderate stress but degrades at high stress, when attention narrows and error rates rise.
- ISA conditions
- Sea level temperature 15 °C, pressure 1013.25 hPa, lapse rate 1.98 °C per 1000 ft up to the tropopause at 36 090 ft.
- QNH versus QFE
- QNH is pressure reduced to sea level and shows elevation on the ground. QFE is pressure at the aerodrome and shows zero on the ground.
- Clear ice
- Ice formed from large supercooled droplets in stratiform cloud. It spreads over the surface and is difficult to remove.
- Great circle
- The shortest path between two points on a sphere. Its track changes continuously and it appears curved on a Mercator chart.
- Mercator projection
- A cylindrical projection where rhumb lines are straight and scale increases with latitude. Great circles appear curved.
- 1-in-60 rule
- A 1° track error over 60 NM gives 1 NM off track. Correction angle equals distance off track times 60 divided by distance flown.
- VOR radial
- The magnetic bearing from the VOR station. The CDI centres when the selected radial matches the aircraft's position.
- DME slant range
- Distance measured directly to the station, not along the ground. Error is largest when directly overhead the station.
- ILS Category I
- An ILS approach with decision height not lower than 200 ft and runway visual range of at least 550 m.
- Final reserve fuel
- Fuel required to hold for 30 minutes at 1500 ft above the alternate aerodrome, computed at the planned landing mass.
- Equal time point
- The point where time to continue equals time to return, determined by wind and true airspeed rather than by distance alone.
- Critical angle of attack
- The angle at which airflow separates and the wing stalls. It is independent of mass, but stall speed rises with mass.
- Load factor in a turn
- In a level turn, n = 1/cos(bank angle). At 60° bank the load factor is 2, doubling stall speed's square root factor.
- Sweepback effect
- Increases critical Mach number and lateral stability but lowers lift coefficient and can promote Dutch roll.
- Sterile flight deck
- No non-essential communication or activity during taxi, take-off, approach, and landing, and below 10 000 ft.
- MAYDAY FUEL
- The distress call when fuel is below final reserve. ATC gives priority and the aircraft lands at the nearest suitable aerodrome.
- VHF line-of-sight range
- Approximate range in nautical miles equals 1.23 times the square root of antenna height in feet.
- Readback requirement
- Clearances for route, altitude, heading, and frequency must be read back. Ambiguous clearances must be clarified, not assumed.