Notes

Question 1

Standard Temperature

Answer 1

15°C at sea level pressure altitude and decreases by 2°C for each 1000 feet of altitude

Question 2

Pressure Altitude

Answer 2

The altitude read from an altimeter when the altimeter’s barometric scale has been set to 29.92 inches of mercury.

Question 3

Reference Datum

Answer 3

Is an imaginary vertical plane from which all horizontal distances are measured for balance purposes

Question 4

Arm

Answer 4

Is the horizontal distance from the reference datum to the center of gravity of an item

Question 5

Moment

Answer 5

Is the product of the weight of an item multiplied by its arm.

Question 6

Standard Empty Weight

Answer 6

Is the weight of a standard airplane, including usable fuel, full operating fluids and full engine oil

Question 7

Basic Empty Weight

Answer 7

Is the standard empty weight plus the weight of optional equipment

Question 8

Useful Load

Answer 8

Is the difference between ramp weight the basic empty weight

Question 9

Maximum Engine Speed

Answer 9

2700 RPM

Question 10

Spin Recovery

Answer 10

Opposite rudder
Forward elevator
Neutralize controls

Question 11

Normal Climb out

Answer 11

75 - 85 KIAS

Question 12

Landing Approach,

Flaps Up

Flaps Full

Answer 12

65- 75 KIAS
60- 70 KIAS

Question 13

Maximum Recommended Turbulent Air Penetration Speed

2550 lbs
2200 lbs
1900 lbs

Answer 13

105 KIAS
98 KIAS
90 KIAS

Question 14

Weight X Arm =

Answer 14

Moment

Question 15

Total Moment ➗ Total Weight =

Answer 15

CG
(Center of gravity)

Question 16

Moment ➗ Weight =

Answer 16

Arm

Question 17

Moment ➗ Arm =

Answer 17

Weight

Question 18

Transponder Codes

1200

Answer 18

VFR operations

Question 19

Transponder Codes

7500

Answer 19

Hijack

Question 20

Transponder Codes

7600

Answer 20

Communication failure

Question 21

Transponder Codes

7700

Answer 21

Emergency