Purpose of mass and balance considerations
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Mass and balance details of aircraft
Determination of CG position
Cargo handling
100

The stall speed of an aircraft is highest when gross mass is _____ and CG is ______?


High gross mass and forward CG 

100

TOM - traffic load = 

Operating mass 

100

Where are CG limitations found?

Aircraft flight manual (AFM)

100

Simplified, scaled down value of a moment is called....

Index

100

Where are passenger baggage usually stored?

(bulk cargo, containers or pelletized cargo)

Containers 

200

What effect does the CG on the aft limit have on the fuel consumption and endurance of an airplane? 

Fuel consumption decreases and endurance increases

200

An aircraft is carrying 12 passengers and the total number of passenger seats is 19. What mass must be used for the passengers baggage?

Actual mass

200

Which axis is the CG normally computed along? (Vertical, lateral, longitudinal or horizontal)

Longitudinal

200

"Moment divided by 100" is an example of....

moment index 

200

Rush bags, last minute baggage and cabin crew baggage is held in/on:

Bulk cargo

300

Is flat spin more likely to happen to a stable or unstable aircraft?

Unstable

300

What is our most limiting mass for takeoff, given the following information? 


MZFM: 39 000kg

PLLAM: 43 000kg

MLAM : 40 000kg

MTOM : 47 000kg

PLTOM : 45 000kg 

Takeoff fuel : 4000kg 

Trip fuel : 2000kg

42 000kg

300

What is the formula for moment?

Force x arm

300

What is the CG position formula for ballast?

Mass original x shift = load of ballast x distance between the compartment and the new CG

MxS=LxD

300

What is the formula for area load?

kg = kg/m² x m²

400

At what CG position is degradation or loss of nose wheel steering likely to be encountered?

Too far aft

400

What does the basic empty mass consist of? 

(4 items)

Empty mass 

Unusable fuel 

Safety equipments 

Non fuel based liquids (i.e. oil, hydraulic fluids)

400

The distance from the datum to the center of gravity of a mass is called....

Moment arm or balance arm

400

Current CG position : 2.7 aft of the datum 

Actual takeoff mass : 6630kg

Calculate the mass that must be moved aft by a distance of 2.8m, in order to move the current CG to 2.8m aft of the datum. 

237kg 

400

Calculate the smallest required floor contact area of a box with a mass of 105kg, if the maximum floor load is 600kg/m²?

0.175m²

500

Forward CG limit: 8% MAC

Aft CG limit : 64% MAC 

Actual CG position : 10% MAC 

What is the effect on stall speed and range compared to a more neutral CG position?



Stall speed increases, Range Decreases

500

What additional traffic load could the crew accept for takeoff, given the following information?

Dry operating mass : 12 445lb

Traffic load : 241 lb

Fuel loaded : 5000lb 

Trip fuel : 3000lb 

Taxi fuel : 100lb 

Max takeoff mass : 18 386lb

800lb

500

MAC: 3.08m

LEMAC: 14.72m aft of datum 

Calculate the CG position in % MAC when the CG is located 16.13m aft of the datum.

45,78%

500

The actual mass of an airplane is 1950lb, it's CG is located 2.15 aft of the datum. An additional mass of 450 lb is loaded 1.75m aft of the datum. Calculate its new CG position.

2.075m

500

Pallet: 1.4m x 1.4m 

Max running load: 2 015 lb/m

Find the maximum allowed mass which can be loaded on the pallet without exceeding the maximum running load 

2821lb

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