Students > VFR : If the centre of gravity of an aeroplane moves forward during flight the ?

Question 65-1 : Heavier making the aeroplane more difficult to manoeuvre in pitch lighter making the aeroplane more difficult to manoeuvre in pitch heavier making the aeroplane more easy to manoeuvre in pitch lighter making the aeroplane more easy to manoeuvre in pitch

The determination of the centre of gravity in relation to the mean aerodynamic ?

Question 65-2 : Length of the mean aerodynamic chord and the leading edge length of the mean aerodynamic chord and the trailing edge position of the aerodynamic convergence point position of the aerodynamic centre of pressure

The maximum zero fuel mass ?

Question 65-3 : Is calculated for a maximum load factor of +2 5 g is calculated for a maximum load factor of +3 5 g can be increased by stiffening the wing imposes fuel dumping from the outer wings tank first

When has the centre of gravity to be computed ?

Question 65-4 : Prior to every flight at least every four years during every yearly inspection after every 400 hours inspection

The operating mass om is ?

Question 65-5 : The take off mass minus the traffic load the take off mass minus the basic empty mass and crew mass the maximum zero fuel mass minus the traffic load the landing mass minus the traffic load

The 'regulated landing mass' is the ?

Question 65-6 : Lowest of the structural limited landing mass and the performance limited landing mass maximum landing mass established by the aircraft operator maximum landing mass established by the aircraft manufacturer maximum difference between performance limited landing mass and structural landing mass

Given .dry operating mass= 29 800 kg.maximum take off mass= 52 400 kg.maximum ?

Question 65-7 : 12 900 kg 13 300 kg 9 300 kg 14 600 kg

The take off mass of an aircraft is 117 000 kg comprising a traffic load of 18 ?

Question 65-8 : 53 000 kg 71 000 kg 99 000 kg 64 000 kg

The dry operating mass includes ?

Question 65-9 : Crew and crew baggage catering removable passenger service equipment potable water and lavatory chemicals unusable fuel and reserve fuel fuel and passengers baggage and cargo passengers baggage and cargo

The maximum load per running metre of an aircraft is 350 kg/m the width of the ?

Question 65-10 : A load of 400 kg in a crate with dimensions 1 2 m x 1 2 m x 1 2 m a load of 500 kg in a crate with dimensions 1 5 m x 1 m x 1 m a load of 400 kg in a crate with dimensions 1 4 m x 0 8 m x 0 8 m a load of 700 kg in a crate with dimensions 1 8 m x 1 4 m x 0 8 m

Given the following . maximum structural take off mass 48 000 kg. maximum ?

Question 65-11 : 47 800 kg 48 000 kg 48 400 kg 53 000 kg

The maximum zero fuel mass .1 is a regulatory limitation.2 is calculated for ?

Question 65-12 : 1 3 5 1 2 3 2 3 5 2 3 4

At the flight preparation stage the following parameters in particular are ?

Question 65-13 : The dry operating mass includes fixed equipment needed to carry out a specific flight the operating mass is the mass of the aircraft without take off fuel the dry operating mass includes take off fuel the operating mass includes the traffic load

Which of the following corresponds to zero fuel mass ?

Question 65-14 : The take off mass of an aeroplane minus all usable fuel take off mass minus fuel to destination and alternate operating mass plus passengers and cargo operating mass plus luggage of passengers and cargo

Given that . maximum structural take off mass 146000 kg. maximum structural ?

Question 65-15 : 120 300 kg 120 900 kg 121 300 kg 146 000 kg

Given . maximum structural take off mass 72 000 kg. maximum structural landing ?

Question 65-16 : 69 600 kg 74 000 kg 72 000 kg 70 400 kg

The actual take off mass is equal to 41 545 kg . catering 300 kg. safety and ?

Question 65-17 : 30 665 kg 30 300 kg 30 785 kg 38 300 kg

The zero fuel mass of an aeroplane is always ?

Question 65-18 : The take off mass minus the mass of take off fuel the take off mass minus the wing fuel mass the take off mass minus the fuselage fuel mass the maximum take off mass minus the take off fuel mass

Given .maximum structural take off mass 146 900 kg.maximum structural landing ?

Question 65-19 : 120 900 kg 121 300 kg 113 900 kg 120 300 kg

Traffic load is the ?

Question 65-20 : Zero fuel mass minus dry operating mass dry operating mass minus the disposable load dry operating mass minus the variable load take off mass minus zero fuel mass

While making mass and balance calculation for a particular aircraft the term ?

Question 65-21 : Unusable fuel and full operating fluids all the oil fuel and hydraulic fluid but not including crew and traffic load all the oil and fuel all the consumable fuel and oil but not including any radio or navigation equipment installed by manufacturer

The term 'maximum zero fuel mass' consist of ?

Question 65-22 : The maximum permissible mass of an aeroplane with no usable fuel the maximum mass authorized for a certain aeroplane not including traffic load and fuel load the maximum mass authorized for a certain aeroplane not including the fuel load and operational items the maximum mass for some aeroplanes including the fuel load and the traffic load

The actual 'zero fuel mass' is equal to the ?

Question 65-23 : Dry operating mass plus the traffic load operating mass plus all the traffic load basic empty mass plus the fuel loaded actual landing mass plus trip fuel

The actual 'take off mass' is equivalent to ?

Question 65-24 : Dry operating mass plus take off fuel and the traffic load actual zero fuel mass plus the traffic load dry operating mass plus the take off fuel actual landing mass plus the take off fuel

With respect to aeroplane loading in the planning phase which of the following ?

Question 65-25 : Lm = tom trip fuel mtom = zfm + full tank fuel mass mzfm = traffic load + dom reserve fuel = tom trip fuel

Given an aeroplane with.maximum structural landing mass 125000 kg.maximum zero ?

Question 65-26 : 130500 kg and 26500 kg 130500 kg and 31500 kg 125500 kg and 21500 kg 125500 kg and 26500 kg

For the purpose of completing the mass and balance documentation the traffic ?

Question 65-27 : Less the operating mass plus the operating mass plus the trip fuel mass less the trip fuel mass

For the purpose of completing the mass and balance documentation the operating ?

Question 65-28 : Take off fuel mass ramp fuel mass trip fuel mass ramp fuel mass less the fuel for apu and run up

When establishing the mass breakdown of an aeroplane the empty mass is defined ?

Question 65-29 : Standard empty mass plus specific equipment mass plus trapped fluids plus unusable fuel mass empty mass dry plus variable equipment mass basic mass plus variable equipment mass basic mass plus special equipment mass

For the purpose of completing the mass and balance documentation the dry ?

Question 65-30 : The total mass of the aircraft ready for a specific type of operation excluding all usable fuel and traffic load the total mass of the aircraft ready for a specific type of operation excluding all usable fuel the total mass of the aircraft ready for a specific type of operation excluding all traffic load the total mass of the aircraft ready for a specific type of operation excluding crew and crew baggage

An aircraft's weighing schedule indicates that the empty mass is 57320 kg .the ?

Question 65-31 : Operational items have a mass of 2800 kg and the maximum traffic load for this aeroplane is 11980 kg operational items have a mass of 2800 kg and the maximum traffic load for this aeroplane is 14780 kg operational items have a mass of 2800 kg and the maximum useful load is 11980 kg operational items have a mass of 2800 kg and the maximum useful load is 14780 kg

An aeroplane is to depart from an airfield where the performance limited take ?

Question 65-32 : 21080 kg 21500 kg 21220 kg 20870 kg

The empty mass of an aircraft as given in the weighing schedule is 61300 kg ?

Question 65-33 : 68400 kg 29600 kg 70700 kg 26900 kg

The following data applies to an aeroplane which is about to take off ?

Question 65-34 : 78900 kg 78150 kg 18200 kg 17450 kg

A revenue flight is to be made by a jet transport the following are the ?

Question 65-35 : 17 840 kg 25 800 kg 18 170 kg 13 950 kg

A revenue flight is to be made by a jet transport .the following are the ?

Question 65-36 : 17 810 kg 21 170 kg 21 070 kg 20 420 kg

A revenue flight is to be made by a jet transport the following are the ?

Question 65-37 : 17 840 kg 19 500 kg 19 100 kg 19 200 kg

The following data is extracted from an aeroplane's loading ?

Question 65-38 : Is 87300 kg and excess structural stress could result is 83200 kg which is in excess of the regulated landing mass and could result in overrunning the runway must be reduced to 81700 kg in order to avoid a high speed approach is 87300 kg which is acceptable in this case because this is a diversion and not a normal scheduled landing

With respect to multi engine piston powered aeroplane determine the ramp mass ?

Question 65-39 : 4720 lbs 4120 lbs 4390 lbs 4372 lbs

The crew of a transport aeroplane prepares a flight using the following data . ?

Question 65-40 : 25 800 kg 55 800 kg 25 000 kg 55 000 kg