Validation > Marking : A public transport aeroplane with reciprocating engines the final reserve ?

Question 89-1 : Fuel to fly for 45 minutes fuel to fly for 2 hours fuel to fly for 1 hour at holding speed fuel to fly for 30 minutes at holding speed

Assuming the following data .ground distance to be covered 1 500 nm.cruise ?

Question 89-2 : 23 500 kg 21 500 kg 21 700 kg 19 900 kg

For a flight of 2400 ground nautical miles the following apply .tail wind 25 ?

Question 89-3 : A 14000 kg b 5h 35 min a 15800 kg b 6h 20 min a 14600 kg b 5h 45 min a 15000 kg b 6h 00 min

Given .brake release mass 58 000 kg.temperature isa +15.the fuel required to ?

Question 89-4 : 1250 kg 1400 kg 1450 kg 1350 kg

The flight crew of a turbojet aeroplane prepares a flight using the following ?

Question 89-5 : 34 430 kg 30 440 kg 32 480 kg 28 720 kg

The purpose of the decision point procedure is ?

Question 89-6 : To reduce the minimum required fuel and therefore be able to increase the traffic load to reduce the landing weight and thus reduce the structural stress on the aircraft to increase the safety of the flight to increase the amount of extra fuel

At reference or see flight planning manual mrjt 1 figure 4 7 2.for the purpose ?

Question 89-7 : M/kias 74/330 lrc m/kias 74/290 m/kias 70/280

Using the power setting table for the single engine aeroplane determine the ?

Question 89-8 : 134 kt and 55 7 lbs/h 131 kt and 56 9 lbs/h 125 kt and 55 7 lbs/h 136 kt and 56 9 lbs/h

For turbojet engine driven aeroplane given .taxi fuel 600 kg.fuel flow for ?

Question 89-9 : 77 800 kg 76 100 kg 80 500 kg 79 200 kg

The following apply .temperature isa +15°c.brake release mass 62000 kg.trip ?

Question 89-10 : 13500 kg 13000 kg 13200 kg 13800 kg

At reference or see flight planning manual mrjt 1 figure 4 3 1c. for a flight ?

Question 89-11 : A 17600 kg b 6 hr 50 min a 16200 kg b 6 hr 20 min a 17000 kg b 6 hr 10 min a 20000 kg b 7hr 00 min

At reference or see flight planning manual mrjt 1 figure 4 3 5. for a flight of ?

Question 89-12 : A 18100 kg b 7hr 20 min a 15800 kg b 6hr 00 min a 21800 kg b 9hr 25 min a 19000 kg b 7hr 45min

Mark the correct statement .if a decision point procedure is applied for flight ?

Question 89-13 : The trip fuel to the destination aerodrome is to be calculated via the decision point the trip fuel to the destination aerodrome is to be calculated via the suitable enroute alternate a destination alternate is not required the fuel calculation is based on a contingency fuel from departure aerodrome to the decision point

An aeroplane has the following masses .estimated landing weight 50 000 kg.trip ?

Question 89-14 : 4 300 kg 6 185 kg 9 000 kg 6 400 kg

In a flight plan when the destination aerodrome is a and the alternate ?

Question 89-15 : 30 minutes holding 1 500 feet above aerodrome b 30 minutes holding 2 000 feet above aerodrome b 15 minutes holding 2 000 feet above aerodrome a 30 minutes holding 1 500 feet above aerodrome a

A jet aeroplane has a cruising fuel consumption of 4060 kg/h and 3690 kg/h ?

Question 89-16 : 8120 kg 7380 kg 1845 kg 3500 kg

Given .fuel density = 0 78 kg/l .dry operating mass = 33500 kg .traffic load = ?

Question 89-17 : 17 350 kg 22 100 kg 17 550 kg 21 900 kg

Planning an ifr flight from paris to london for the twin jet aeroplane ?

Question 89-18 : 1000 kg 1500 lbs 1100 kg 1000 lbs

Provided that flight conditions on the leg gamma to delta remain unchanged and ?

Question 89-19 : 4475 kg 4745 kg 4635 kg 4250 kg

The required time for final reserve fuel for turbojet aeroplane is ?

Question 89-20 : 30 minutes 45 minutes 60 minutes variable with wind velocity

A flight has to be made with a single engine aeroplane .for the fuel ?

Question 89-21 : 276 lbs 265 lbs 208 lbs 250 lbs

See flight planning manual mrjt 1 figure 4 5 2 and 4 5 3 1.given .distance c d ?

Question 89-22 : 14 500 kg 14 200 kg 17 800 kg 17 500 kg

At reference or see flight planning manual mrjt 1 figure 4 5 4.planning an ifr ?

Question 89-23 : 273 kg 320 kg 210 kg 263 kg

At reference or see flight planning manual mrjt 1 paragraph 2 1 and figure 4 ?

Question 89-24 : Fmp 4% fmp 0% fmp 1% fmp 10%

The final reserve fuel for aeroplanes with turbine engines is ?

Question 89-25 : Fuel to fly for 30 minutes at holding speed at 1500 ft 450 m above aerodrome elevation in standard conditions fuel to fly for 45 minutes at holding speed at 1500 ft 450 m above aerodrome elevation in standard conditions fuel to fly for 45 minutes at holding speed at 1000 ft 300 m above aerodrome elevation in standard conditions fuel to fly for 60 minutes at holding speed at 1500 ft 450 m above aerodrome elevation in standard conditions

The fuel burn of an aircraft turbine engine is 220 l/h with a fuel density of 0 ?

Question 89-26 : 235 l/h 206 l/h 220 l/h 176 l/h

At reference or see flight planning manual mep1 figure 3 1.a flight is to be ?

Question 89-27 : 6 us gallon 9 us gallon 12 us gallon 3 us gallon

When using decision point procedure you reduce the ?

Question 89-28 : Contingency fuel by adding contingency only from the burnoff between decision point and destination contingency fuel by adding contingency only from the burnoff between the decision airport and destination reserve fuel from 10% down to 5% holding fuel by 30%

A jet aeroplane is to fly from a to b the minimum final reserve fuel must allow ?

Question 89-29 : 30 minutes hold at 1500 ft above destination aerodrome elevation when no alternate is required 20 minutes hold over alternate airfield 30 minutes hold at 1500 ft above mean sea level 15 minutes hold at 1500 ft above destination aerodrome elevation

At reference or see flight planning manual mrjt 1 figure 4 5 1. given brake ?

Question 89-30 : 1138 kg 1040 kg 1238 kg 1387 kg

At reference or see flight planning manual sep 1 figure 2 2 table 2 2 3.using ?

Question 89-31 : 160 kt and 69 3 lbs/h 158 kt and 74 4 lbs/h 160 kt and 71 1 lbs/h 159 kt and 71 7 lbs/h

At reference or see flight planning manual mep 1 figure 3 3.a flight has to be ?

Question 89-32 : 91 us gallons 76 us gallons 118 us gallons 86 us gallons

Integrated range' curves or tables are presented in the aeroplane operations ?

Question 89-33 : To determine the fuel consumption for a certain still air distance considering the decreasing fuel flow with decreasing mass to determine the flight time for a certain leg under consideration of temperature deviations to determine the still air distance for a wind components varying with altitude to determine the optimum speed considering the fuel cost as well as the time related cost of the aeroplane

At reference or see flight planning manual sep 1 figure 2 4 .using the range ?

Question 89-34 : 865 nm 739 nm 851 nm 911 nm

At reference or see flight planning manual mrjt 1 figure 4 4. the final reserve ?

Question 89-35 : Pressure altitude aeroplane mass and flaps up with minimum drag airspeed pressure altitude aeroplane mass and flaps down with maximum range speed pressure altitude aeroplane mass and flaps up with maximum range speed pressure altitude aeroplane mass and flaps down with minimum drag airspeed

Finish the endurance/fuel calculation and determine atc endurance for a twin ?

Question 89-36 : Atc endurance 04 07 atc endurance 04 12 atc endurance 03 37 atc endurance 03 52

Given .oat +5°c.during climb average head wind component 20 kt.take off from ?

Question 89-37 : 9 min 3 3 usg 10 min 3 6 usg 7 min 2 6 usg 9 min 2 7 usg

Maximum allowable take off mass 64 400 kg.maximum landing mass 56 200 ?

Question 89-38 : 11 100 kg 11 400 kg 14 400 kg 8 600 kg

At reference or use flight planning manual sep 1 table 2 2 3 .given .fl 70.oat ?

Question 89-39 : 12 35 gph tas 159 kt 73 90 gph tas 159 kt 12 35 gph tas 151 kt 11 95 gph tas 160 kt

At reference or see flight planning manual mrjt 1 figure 4 5 3 1. given flight ?

Question 89-40 : 345 nam. 2000 kg 350 nam. 2000 kg 345 nam. 2100 kg 437 nam. 2100 kg