Aless PREP

the systoms of windshear may include: Loss of altitude buffet. a high rate of descent combined with excessive pitch attitude. A significant change of airspeed, divergence from the required flight path, normal control inputs are insufficient to maintain the flight path. Loss of airspeed, increasing rate of descent and pre-stall buffet.

After landing on a dry runway which is the most effective retardation device?. The airbrakes/spoilers. Reverse Thrust. The antisky brakes.

Fuel Jettison when required can be carried out ___________. At 10.000 feet AGL and preferably over the sea. At 7.000 feet AGL in winter and 4.000 feet AGL in summer. All of the above.

When the plannned route is via ADIZ you are required to ________. In Some cases Call the atc prior to entry and obtain Air Defense clearance. Call ATC on entering ADIZ. Comply with the specific conditions and instructions as prescribed by the relevant state.

At 1000 feet on a manually flown ILS approach you notice the handling pilot has let the aircraft drop below the Glide slope GS, Would you_______. Verbally warn the handling pilot, monitor the response and look for a correction. Verbally warn the handling pilot and take control immediatly. Verbally warn the handling pilot, increase thrust and lightly cover the controls.

Optimum altitude normally provides a buffet margin of______. 1.45 G. 1.3 G. 1.35 G.

When flying in RVSM airspace utilising the semi-circular rule what is the lowest RVSM hight level on a track 270. FL 250. FL 290. FL 300.

When flying in RVSM airspace utilising the semi-circular rule what is the highest RVSM level flying on track 110. FL 390. FL 400. FL 410.

The minimum generally acceptable buffet margin in cruise is ______. 1.2 G. 1.3 G. 1.45 G.

Which of the following masses are considered to be part of the payload of an aircraft?. Passangers, Cargo, Mail, Catering, Reserve and Contingency fuel. Passangers, Cargo, Mail, Reserve fuel and baggage. Passangers, Baggage, Cargo and Mail.

When operating at the long Range Cruise (LRC) Mach number. The specific range corrresponds to 95% of the maximum specific range. The specific range corresponds to 100% of the maximum specific range. The specific range corresponds to 99% of the maximum specific range.

The optimum cruise altitude is _________. Determined by weight and MAch number and ensures the optimum CL and maximum specific range. Determined by weight Mach number, SAT/OAT and ensures the optimum CL and Maximum specific range. Determined by weight, SAT/OAT and ensures that maximum specific range.

At 1700 feet on the ILS approach in IMC the GPWS sounds Whoop Whoop Whoop pull up. Checj the ILS glidslope is within one dot and the limit. Immediatly go around and inform ATC. Cancel GPWS check on the glidepath and increase thrust as a precaution.

what distance from the stop and of the runway do the centre line lights change from red/white to solid red. 900m. 600m. 300m.

While in a descent under radar control you receive a TCAS RA, You would. Continue with the descent, advice ATC of the RA and look out for other aircraft. Continue with the descent but turn 90 degrees, on the heading by ATC. Manouver to follow the RA guidance and advice ATC.

Taxiway lighting consists of. Green centre line lights with blue edge lighting. Green centre line lights with green edge lights on corners. White centre line lights with red edge lights on corners.

In the cruise at high altitude when flying into an area of known turbulence you would. Stop the cabin service and fly at the turbulence speed. Secure the cabin and cockpit, select turbulance speed and mantain a constant altitude. Secure the cabin and cockpit and descent at MMO/VMO.

When calculation takeoff performance speeds. VMGC should be greater than V1. VMGC should be less than or equal to V1. VMGC must be greater than V1 by 30%.

Ice contamination of the wing upper and lower surface may cause. A reduction in stall margins and possible poor and lateral control on takeoff. a loss of lift and pitch control on the ground. a loss of lift and pitch control on the fround.

ILS cat 1 min allow operations down to DH of ______ and RVR of ______. 100 ft, 1200 and 300m. 200 ft, 1600 550m. 50 ft, 700 200m.

After landing in rain on a runway "slipery when wet" your aircraft starts to diverge from the runway centrerline what action do you take to stop the drift. Cancel reverse thrust. Use full opposite rudder to control the drift. Use differential reverse thrust until nosewheel steering becomes effective.

which type of clouds in indicative of very strong turbulance?. Standing lenticular. Nimbostatus. Cirrocumulus.

Under that conditions may ground deicing or anti-icing be required?. Anytime the outside air Temp is +10 or below with moisture. Anytime the outside air Temp is +5 or below with moisture. Anytime the outside air Temp is 0 or below with moisture.

What is the purpose of a negative pressure relief valve?. to prevent the internal cabin air pressure from exceeding the outside air pressure. to prevent the outside air pressure from exceeding the internal cabin air pressure. To prevent the internal cabin air pressure from exceeding the max pressurisation limits.

which of the following defines the ICAO requirements for fuel and oil for a turbojet aircraft? Sufficient fuel and oil to fly to the destination, then. To the alternate, plus 45 minutes at normal cruising speed, then approach and land. To the alternate, plus 30 minutes at normal cruising speed, then approach and land. To the most disntant alternate, hold for 30 mins at 1500 feet AGL, then approach and land.

Why do airplanes equipped with both inboard and outboard ailerons use the outboard ailerons only during low speed flight?. The increased surface area reduces controlability with flap extensions. Aerodynamic loads on the outboard ailerons tend to twist the wingtips at high speeds. Locking out the outboard ailerons in high speed flight provides a variable flight control feel.

Convective clouds which penetrate a stratus layer can produce which threat to instrument flight?. Embedded Thuderstorms. Freezing rain. Clear air turbulance.

RNP 4 ?. That total system error will be no greater than 2nm for 90% of the time. That total system error will be no greater than 8nm for 95% of the time. That total system error will be no greater than 4nm for 95% of the time.

For a 2 engine airplane the distance from the departure aerodrome to the takeoff alternate must not exceed. One hour at the normal 2 engines cruising speed. One hour at the one engine inoperative cruising speed. Two hours at the one engine inoperative cruising speed.

When operating in ECON (economy) cruise mode and fuel costs are high, the fms cost index (CI) value you expect to see will be. high. low. average.