Av Mechanics General

Front 1

Zero Fuel weight is the

Back 1

Maximum fuel

Front 2

The empty weight of an airplane is determined by

Back 2

Subtracting Point

Front 3

When dealing with weight and balance of an aircraft, the term “maxium weight” is interpreted to mean the maximum

Back 3

authorized contents

Front 4

The maximum weight of an aircraft is the

Back 4

Empty load

Front 5

What should be clearly indicated on the on the aircraft weighing form?

Back 5

Weighing points

Front 6

What determines wheter the value of the moment is preceded by a plus (+) or (-) sign in an aircraft weight and balance?

Back 6

Location of reference and weight

Front 7

1)Private aircraft are required by regulations to be weighed periodically.
2)Private aircraft are required to be weighed after making any alteration Regarding the above.

Back 7

NT

Front 8

To obtain useful weight data for the pupose of dtermining the CG, it is necessary that an aircraft be weighed

Back 8

in attitude

Front 9

When computing weight and balance, an airplane is considered to be inbalance when

Back 9

the its CG range

Front 10

What tasks are completed prior to weighing an aircraft to dtermine its empty weight?

Back 10

Remove Resivoir

Front 11

The useful load of an aircraft consists of the

Back 11

CC

Front 12

The useful load of an aircraft is the

Back 12

Difference gross weight

Front 13

The maximum weight as used in weight and balance control of a given aircraft can normally be found

Back 13

In Sheet

Front 14

As weighed the total empty weight of an aircraft is 5,862 pounds with a moment of 885,957. Howeverm when the aircraft was weighed, 20 pounds of potable was were on board at +84 and 23 pounds of hydraulic fluid were in a tank located at +101. What is the empty weight CG of the aircraft.?

Back 14

15

Front 15

Two boxes which weigh 10 pounds and 5 pounds are placed in an airplane so that their distance aft from the CG are 4-feet and 2 feet respectively. How far forward of the Cgshould a third box, weighing 20 pounds, be placed so that the CG will not be changed?

Back 15

25 feet

Front 16

If a 40 pounds generator applies + 1400 inch pounds to a reference axis.

Back 16

+ 35

Front 17

In a balance computation of an aircraft from which an item located aft of the datum was removed use

Back 17

NN

Front 18

Datum is forward of the main gear center points 30.24 in. Actual distance between tail gear and main gear center points –

1. Lavatory water tank full
2. 2. Hydraulic fluid
3. Removable ballast (146 pounds at +300

What is the empty weight CG of the aircraft described above?

Back 18

61

Front 19

When an empty aircraft is weighed, the ombined net weight at the main gears is 3,450 pounds with an arm of 195.5 inches. At the nose gear, the net weight is 2,322 pounds with an arm of 83.5 inches. The datum line is forward of the nose of the aircraft. What is the empty CG of the aircraft?

Back 19

11

Front 20

Find The empty weight CG location for the following tricylce gear aircraft. Each main wheel weighs 753 pounds, nosewheel weighs 22 pounds, distance between nosewheel and main wheels is 87.5 inches noosewheel location is +9.875 inches from datum , with 1 gallon of hydraulic fluid at – 21.0 inches included in the weight scale

Back 20

911

Front 21

An aircraft with an empty weight of 2,100 pouns and an empty weight CG + 32.5 was altered as follows:
(1) two 18-pound passenger seats located +73 were removed;
(2) structural modifications were made at +77 increasing weight by 17 pounds.
(3) A seat and safety belt weighing 25 pounds was installed at +95 What is the new empty weight CG?

Back 21

+38

Front 22

An aircraft as loaded weighs 4,954 pounds at a CG of +30.5 inches to +42.1 +30.5 inches. Find the minimum weight of the ballast necessary to bring the CG within the CG range. The ballast arm is +162 inches.

Back 22

+56

Front 23

An aircraft as loaded weighs 4,954 pounds at a CG of +30.5 inches to +42.1 +30.5 inches. Find the minimum weight of the ballast necessary to bring the CG within the CG range. The ballast arm is +162 inches.

Back 23

12

Front 24

When making a rearward weight and balnace check to determine that the CG will not exceed the rearward limit during extreme conditions, the items of useful load which should be computed at their minimum weights are those located forward of the

Back 24

Rearward limit

Front 25

The following alteration was performed on an aircraft: A model B
Engine weighing 175 pounds was replaced by a model D engine weighing 185 pounds at a -62.00 –inch station. The aircraft weight and balance records show the previous empty weight to be 998 pounds and an empty weight of 13.48 inches.

Back 25

13

Front 26

When computing the maximum forward loaded CG of an aircraft, minimum weights, arms, and moments should be used for items of useful load that are located aft of the

Back 26

forward limit.

Front 27

If the empty weight CG of an airplane lies within the empty weight CG limits,

Back 27

It Not Extremes

Front 28

True or False

(This is a ray question)

These flashcards are for studying purposes where the student knows the full question and has available with him or her the FAA testbank to double check the answers?

Back 28

True:For those who are outside of the normal Av Mechanics General from my school may not use these cards for passing anyother FAA tests. Unless their teachers states the following:
'I am copying and pasting the test directly of of FAA test bank from faa.gov since it's in public domain' or 'Do not use any other source to study from except the FAA test bank.'
Remember first and last words of answers ONLY!!!!!!!!!!!!!