From the following list:1. Fire extinguishers2. Portable oxygen supplies3. First-aid kits4. Passenger meals5. Alcoholic beveragesWhich are classed as Dangerous Goods that are required to be on the aircraft in accordance with relevant JAR's for operating reasons:4
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Astronomic precession:4
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A commercial aeroplane is scheduled to be operated at FL 390 and has the following characteristics:Maximum approved passenger seating configuration = 230 Number of seats on board= 200Scheduled number of passengers on board= 180The minimum number of oxygen dispensing units provided in the aeroplane cabin compartment should be:4
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In accordance with the PART-CAT, a single deck airplane, equipped with an approved seating capacity of 61 seats and carrying passengers, must be equipped with:4
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The number of spare fuses available for use in flight must be:4
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For a pressurised aeroplane, certificated to fly above 25 000 ft, all occupants of flight deck seats on flight deck duty shall be supplied with supplemental oxygen during a period in any case no less than:4
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You plan to fly from point A (60N 010E) to point B (60N 020E).The gyro North of the gyro compass, assumed to be operating perfectly, with no rate correction device, is aligned with the true North of point4
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The inertial navigation system (INS) indicates: Position: 71° 55.1'N 094°55.3'WDrift: 6°L (left)The route followed in order to return to the VOR station is the meridian of the VOR station used:RESOLUTE BAY (74°43.6'N 094°55.3W), this VOR has North set on the local geographic meridian.The gyro compass has just been reset to Grid North (chart used: polar stereographic chart, grid parallel to zero meridian, Grid North in the direction of geographic North Pole).The correct representation of the RMI VOR/DME is at this moment: (the distance DME is in the box)4
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During a flight from Europe, scheduled in MNPS (Minimum Navigation Performance Specification) airspace, you expect to cross the 30°W meridian at 1330 UTC4
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In the absence of wind and without the astronomic precession effect, an aircraft would, at a constant gyro heading, follow a:4
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