The following data applies to an aircraft which is about to take off .maximum ? [ Study Manual ]
Question 69-1 : 2690 kg 1710 kg 3630 kg 3150 kg

1 ton equals approximately ?
Question 69-2 : 2200 lb 2000 lb 1200 lb 220 lb

Given .basic empty mass 5300 kg.dry operating mass 5500 kg.zero fuel mass 5980 ?
Question 69-3 : 2480 kg 2680 kg 2000 kg 480 kg

Based on actual conditions an aeroplane has the following performance take off ?
Question 69-4 : 4300 kg 4700 kg 4100 kg 4200 kg
Mass for individual passengers to be carried on an aeroplane may be determined ?
Question 69-5 : Passenger seats available is less than 10 passengers carried is less than 10 passenger seats available is less than 20 passengers carried is less than 20

The regulated take off mass is ?
Question 69-6 : The lower of performance limited take off mass and maximum structural take off mass the take off mass subject to departure airfield limitations the higher of performance limited take off mass and maximum structural landing mass the maximum permissible total mass of the aircraft at commencement of take off
Given .container size length x width x height 0 8 x 0 8 x 0 8 m.container has ?
Question 69-7 : 766 kg 383 kg 1532 kg 2393 kg

From the pilot's flight manual determine the maximum total volume of fuel which ?
Question 69-8 : 2367 l 1868 l 8240 l 2121 l

The basic advantage of standard size containers ?
Question 69-9 : Standard size containers are designed to fit and lock into the cargo compartment for maximum space efficiency maximum mass of cargo loaded in the containers is always limited by the mtom with the cargo loaded in containers one does not have to observe the maximum floor loading limit maximum mass of cargo loaded in the containers is often limited by the g forces in flight

From the pilot's flight manual determine the maximum total mass of fuel which ?
Question 69-10 : 1870 kg 2367 kg 2996 kg 8240 kg

The maximum floor loading of the cargo compartment is specified to be 732 ?
Question 69-11 : 1 2 m x 1 2 m 1 25 m x 1 25 m 1 3 m x 1 3 m 1 05 m x 1 05 m

The term 'landing mass' at destination is defined as ?
Question 69-12 : Final reserve fuel alternate fuel contingency fuel plus zero fuel mass final reserve fuel trip fuel plus zero fuel mass final reserve fuel alternate fuel contingency fuel plus landing mass at alternate final reserve fuel trip fuel contingency fuel plus zero fuel mass

Determine the take off mass tom for the following single engine aeroplane ?
Question 69-13 : 2809 lbs 2764 lbs 2799 lbs 2659 lbs

Refer to figure 031 15 .calculate the maximum fuel mass for the centre tank in ?
Question 69-14 : 15450 lbs 3178 lbs 15680 lbs 8640 lbs

What is the reason for cargo loads to be tied down ?
Question 69-15 : Preventing such loads from moving and to remain within the cg limits of the aircraft maximising the space and increasing the maximum payload of the aircraft maximising the performance of the aircraft during take off and landing procedures maintaining enough space in the compartment hold in case of evacuation

The structural limitation of a baggage compartment is 50 lb/ft a load has a ?
Question 69-16 : 1 31 m² 6 4 m² 0 76 m² 14 11 m²

The loaded centre of gravity cg of an aeroplane is 713 mm aft of datum .the ?
Question 69-17 : 16% 41% 60% 10%

The centre of gravity location of the aeroplane is normally computed along the ?
Question 69-18 : Longitudinal axis lateral axis vertical axis horizontal axis

In mass and balance calculations which of the following describes the datum ?
Question 69-19 : It is the point on the aircraft designated by the manufacturer from which all centre of gravity measurements and calculations are made it is the most forward position of the centre of gravity it is the most aft position of the centre of gravity it is the distance from the centre of gravity to the point through which the weight of the component acts
An aircraft has its centre of gravity located 7 metres from the datum line and ?
Question 69-20 : 343000 nm 1 43 nm 7000 nm 34000 n/m

Which one of the following is correct ?
Question 69-21 : Arm = moment / force arm = force x moment arm = force / moment moment = force / arm
Which of the following statements is correct ?
Question 69-22 : A rear centered aircraft is less stable and stalls at a slower speed than a forward centered aircraft if the actual centre of gravity is located behind the aft limit of centre of gravity it is possible that the aeroplane will be unstable making it necessary to increase elevator forces if the actual centre of gravity is close to the forward limit of the centre of gravity the aeroplane may be unstable making it necessary to increase elevator forces the lowest stalling speed is obtained if the actual centre of gravity is located in the middle between the aft and forward limit of centre of gravity

In mass and balance calculations the 'index' is ?
Question 69-23 : Is a figure without unit of measurement which represents a moment a location in the aircraft identified by a number an imaginary vertical plane or line from which all measurements are taken the range of moments the centre of gravity cg can have without making the aircraft unsafe to fly

Which of the following are the exact propositions .1 an aircraft belonging to ?
Question 69-24 : 1 is incorrect 2 is incorrect 1 is correct 2 is correct 1 is correct 2 is incorrect 1 is incorrect 2 is correct

At what mass is an aircraft weighed ?
Question 69-25 : The basic empty mass the basic mass the empty mass the dry operating mass

An aircraft is weighed and the following recordings are made .nose wheel ?
Question 69-26 : 30180 kg 28400 kg 31960 kg 32505 kg

If individual masses are used the mass of an aircraft must be determined prior ?
Question 69-27 : At intervals of 4 years if no modifications have taken place at regular annual intervals only if major modifications have taken place at intervals of 9 years

At the maximum landing mass the range of safe cg positions as determined from ?
Question 69-28 : Forward limit 7 4% mac aft limit 27 0% mac forward limit 8 0% mac aft limit 27 2% mac forward limit 8 6% mac aft limit 27 0% mac forward limit 8 0% mac aft limit 26 8% mac

At a given mass the cg position is at 15% mac if the leading edge of mac is at ?
Question 69-29 : 645 78 inches aft of datum 605 43 inches aft of datum 20 18 inches aft of datum 228 34 inches aft of datum

The aeroplane has a take off mass of 58 000 kg at this mass the range of safe ?
Question 69-30 : Forward limit 8 0% mac aft limit 26 5% mac forward limit 8 5% mac aft limit 26 1% mac forward limit 8 2% mac aft limit 26 2% mac forward limit 9 5% mac aft limit 26 1% mac

When preparing to carry out the weighing procedure on an aircraft which of the ?
Question 69-31 : Drain all engine tank oil drain all useable fuel drain all chemical toilet fluid tanks removable passenger services equipment to be off loaded

An aircraft is weighed prior to entry into service .who is responsible for ?
Question 69-32 : The operator the appropriate aviation authority the aircraft manufacturer or supplier the commander of the aircraft

An aircraft may be weighed ?
Question 69-33 : In an enclosed non air conditioned hangar in a quiet parking area clear of the normal manoeuvring area in an area of the airfield set aside for maintenance at a specified 'weighing location' on the airfield

A aeroplane has a landing mass of 53000kg the range of safe cg positions as ?
Question 69-34 : Forward limit 7 8% mac aft limit 27 0% mac forward limit 8 2% mac aft limit 27 0% mac forward limit 7 3% mac aft limit 26 8% mac forward limit 8 7% mac aft limit 26 8% mac

The aeroplane has a mass of 61 000 kg in the cruise the range of safe cg ?
Question 69-35 : Forward limit 8 3% aft limit 26 3% mac forward limit 7 7% aft limit 25 2% mac forward limit 7 6% aft limit 26 9% mac forward limit 8 0% aft limit 27 2% mac

An aeroplane must be re weighed at certain intervals where an operator uses ?
Question 69-36 : 9 years for each aeroplane 4 years for each aeroplane whenever the certificate of airworthiness is renewed whenever a major modification is carried out

A flight benefits from a strong tail wind which was not forecast on arrival at ?
Question 69-37 : The landing distance required will be longer the approach path will be steeper and threshold speed higher the landing distance will be unaffected the approach path will be steeper

The centre of gravity of an aeroplane is at 25% of the mean aerodynamic chord ?
Question 69-38 : The mean aerodynamic chord in relation to the leading edge the mean aerodynamic chord in relation to the trailing edge the mean aerodynamic chord in relation to the datum the aeroplane in relation to the leading edge

To measure the mass and cg position of an aircraft it should be weighed with a ?
Question 69-39 : 3 points of support 2 points of support 1 point of support 4 points of support

An aeroplane has a mean aerodynamic chord mac of 134 5 inches .the leading edge ?
Question 69-40 : 18 10% 85 50% 75 60% 10 50%

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