Multiple > protocol : Using the data given at the appendix to this question if the fuel index ?

Question 71-1 : 49130 kg and 19% 52900 kg and 21 6% 49130 kg and 21 8% 52900kg and 19%

Using the data given at the appendix determine which of the following correctly ?

Question 71-2 : 48600 kg and 57 0 51300 kg and 57 0 46300 kg and 20 5 35100 kg and 20 5

For this question use annex ecqb 031 mb 02 v2015 03.from the data given at the ?

Question 71-3 : 18% 19% 15% 14%

From the data contained in the attached appendix the maximum allowable take off ?

Question 71-4 : 61600 kg and 12150 kg 68038 kg and 18588 kg 66770 kg and 17320 kg 60425 kg and 10975 kg

An aeroplane is carrying a traffic load of 10320 kg .complete the necessary ?

Question 71-5 : 1830 kg 655 kg 7000 kg 8268 kg

When has the centre of gravity to be computed ?

Question 71-6 : Prior to every flight after every 400 hours inspection at least every 4 years during every yearly inspection

What mass has to be entered in the loading chart for aviation fuel f 34 if 170 ?

Question 71-7 : 133 kg 133 dan 170 kg 218 kg

An aeroplane with a two wheel nose gear and four main wheels rests on the ?

Question 71-8 : 40 cm 25 cm 4 m 41 6 cm

Using the reference provided without the crew the weight and the cg position of ?

Question 71-9 : 4 615 m 0 217 m 4 783 m 4 455 m

Given that the flight time is 2 hours and the estimated fuel flow will be 1050 ?

Question 71-10 : 24 cm aft of datum 25 cm aft of datum 22 cm aft of datum 27 cm aft of datum

An aeroplane with a two wheel nose gear and four main wheels rests on the ?

Question 71-11 : 57 cm 93 cm 108 cm 176 cm

An aeroplane has a planned take off mass of 200 000 kg .its cg is located at 15 ?

Question 71-12 : 4600 kg 5600 kg 3600 kg it is impossible to move the cg at the requested value

The index method in mass and balance calculations is used for ?

Question 71-13 : Reducing the magnitude of the moment reducing the magnitude of the useful load increasing the magnitude of the useful load increasing the magnitude of the moment

What are the advantages of using the index method to determine moments .it ?

Question 71-14 : Reduces the magnitude of the moments making it less time consuming to compute is digitalised and can be automatically uploaded to the aircraft fmc to determine stabiliser trim setting directly produces the position of the cg and the stabiliser trim setting enabled the pilots to calculate the position of the cg by mental arithmetic and thereby expedites mass and balance calculations

What is the principle of the index method ?

Question 71-15 : To divide high magnitude moments by a constant and make result more easier to use to refer every item of the aircraft to a position called the ba balance arm to compute the cg position and stabiliser trim setting without completing a load sheet to round all values for easier and much faster calculation

Define the 'under load' ?

Question 71-16 : Allowed tom dom useful load actual tom dom useful load allowed tl tom actual tl tom

For this question use annex ecqb 031 046 v2015 01 .the aircraft is loaded as ?

Question 71-17 : 300000 kg mm 30000 kg mm 34800 kg mm 348000 kg mm

The planned take off mass of a turbojet aeroplane is 180 000 kg with its centre ?

Question 71-18 : 22 1 % 30 0 % 21 1 % 24 2 %

A turbojet aeroplane has a planned take off mass of 190 000 kg following cargo ?

Question 71-19 : 3000 kg from cargo 4 to cargo 1 2000 kg from cargo 4 to cargo 1 1000 kg from cargo 4 to cargo 1 it is not possible to obtain the required centre of gravity

The planned take off mass of an aeroplane is 190 000 kg with its centre of ?

Question 71-20 : 32 2 % 31 % 27 % 25 %

The planned take off mass of an aeroplane is 180 000 kg with its centre of ?

Question 71-21 : 25% 34% 38% 21%

What is dry operating index doi ?

Question 71-22 : The index for the position of the centre of gravity at dry operating mass the distance from datum to the centre of gravity of a mass the point through which the force of gravity is said to act on a mass the product of the mass and balance arm

A 3 m long plank is on a pivot halfway along its length a 1 kg mass is ?

Question 71-23 : 0 5m to the left 0 5m to the right 1m to the left 1m to the right

For the following see saw to be in balance with a mass of 35 kg suspended on ?

Question 71-24 : 22 kg 136 kg 57 kg 14 kg

Refer to figure 031 13 .for a medium range twin jet aircraft with a cg located ?

Question 71-25 : 3 0 2 5 3 25 2 75

Consider a conventional aircraft with three wheels the nose jack is located 161 ?

Question 71-26 : Bem 40900 lb cg 740 5 in bem 21600 lb cg 722 3 in bem 40900 lb cg 722 3 in bem 21600 lb cg 709 6 in

Refer to figure 031 57 .calculate the cg position and moment for the basic ?

Question 71-27 : 115 7 in aft of datum and the moment is 365074 in lb 111 4 in aft of datum and the moment is 489666 in lb 95 3 in aft of datum and the moment is 380373 in lb 113 6 in aft of datum and the moment is 430998 in lb

The mass and the cg of an aircraft must be established by actual weighing by the ?

Question 71-28 : Operator prior to initial entry into service owner operator before the first flight of the day pilot on entry of aircraft into service engineers before commencing service

Refer to figure 031 59 .the see saw is in a state of equilibrium calculate the ?

Question 71-29 : 30 49 m 37 1 m 29 49 m 22 49 m

Given .length of the mac 114 inches.forward gc limit 12% mac.aft cg limit 38% ?

Question 71-30 : 2 28 inches 8 77 inches 25 08 inches 10 53 inches

Consider a conventional aircraft with three wheels the nose jack is located 161 ?

Question 71-31 : Bem 42054 lb cg 680 3 in bem 24271 lb cg 610 9 in bem 42054 lb cg 570 3 in bem 24271 lb cg 936 in

Refer to figure 031 61 .originally there has been 225 l of fuel in the tank of ?

Question 71-32 : The cg will move towards the nose of the aircraft the cg will move towards the tail of the aircraft the cg will move towards the bottom of the aircraft the cg will remain the same

Refer to figure 031 05 .given .force fa 100 n.distance a 6 m.distance b 3 ?

Question 71-33 : 200 n 300 n 50 n 100 n

Refer to figure 031 34 .given.bem 1200 kg.bem cg 3 00.pilot and front pax ?

Question 71-34 : 2 96 m 2 99 m 3 03 m 3 00 m

Refer to figure 031 04 .given .force fa 100 n.distance a 6 m.distance b 3 ?

Question 71-35 : 50 n 200 n 300 n 50 n

Select the correct statement for the cg safe range ?

Question 71-36 : The safe range falls between the front and rear cg limits and includes both limits the safe range falls between the front and rear cg limits but does not include them the safe range falls between the front and rear cg limits but only includes the aft limit the safe range falls between the front and rear cg limits but only includes the forward limit

The fuel index is ?

Question 71-37 : Used to calculate the correct position of the cg due to different locations of the fuel tanks the difference between the zero fuel mass index and the doi a standard value given by easa and can be used for different types of aircraft only used for aeroplanes with wing tip tanks

Refer to figure 031 03 .given .force fa 300 n.force fb 150 n.distance a 3 ?

Question 71-38 : 6 m 2 m 1 5 m 9 m

Refer to figure 031 60 .given .weight 110800 kg.mac 31 6%..from the given ?

Question 71-39 : 120 4 122 0 122 2 120 7

Refer to figure 031 55 .find the cg position as %mac for the take off ?

Question 71-40 : 24% 10 8% 20% 27%