C172RG

Question 0

What is the best rate of climb speed (Vy)?

Answer 0

84 KIAS at sea level

Question 1

What is the normal climb out speed?

Answer 1

70 - 80 KIAS

Question 2

What is the best angle of climb speed (Vx)?

Answer 2

67 KIAS at sea level

Question 3

What is the maximum flaps down speed (Vf)?

Answer 3

130 KIAS to 10° Flaps

100 KIAS - 10° to 30° Flaps

Question 4

What is the maximum gear down speed (V LE)?

Answer 4

164 KIAS

Question 5

What is the stall speed in the normal landing configuration (V so)?

Answer 5

50 KIAS

Question 6

What is the clean (flaps and gear up) stall speed (V s1)?

Answer 6

54 KIAS

Question 7

What is the approach to landing speed?

Answer 7

65 KIAS

Question 8

What is the maneuvering speed (V A)?

Answer 8

2650 lbs - 105 KIAS
2250 lbs - 98 KIAS
1850 lbs - 89 KIAS

Question 9

What is the never exceed speed (V NE)?

Answer 9

164 KIAS

Question 10

What is the maximum structural cruising speed? (Vno)?

Answer 10

145 KIAS

Question 11

What engine out glide speed will give you the maximum range?

Answer 11

70 KIAS

Question 12

What airspeed is used for a short field takeoff?

Answer 12

63 KIAS

Question 13

What is the airspeed for a short field landing?

Answer 13

63 KIAS

Question 14

What airspeed is used for a soft field takeoff?

Answer 14

KIAS

Question 15

What airspeed is used for a soft field landing?

Answer 15

KIAS

Question 16

What is the service ceiling?

Answer 16

16,800’ MSL

Question 17

What is e make and horsepower of the engine?

Answer 17

Lycoming 180 brake horse power at 2700 RPM

Question 18

What is the estimated true airspeed at 5,000 feet and 65% power?

Answer 18

127 KTAS

Question 19

What combination of RPM and manifold pressure yields 65% power at 5,000’ MSL?

Answer 19

2200 RPM 23 MP

Question 20

How many gallons of fuel are consumed per hour at 65% power at 5,000’ MSL

Answer 20

9.0 gallons per hour

Question 21

How many usable gallons of fuel aircraft carry?

Answer 21

62 gallons of usable fuel.

Question 22

Where are the fuel tanks located and what are their capacities?

Answer 22

There is a 33 gallon fuel tank located in each wing, Providing 66 gallons of total fuel and 62 gallons of usable fuel in all flight conditions.

Question 23

With full fuel, 65% power, at 5000 feet, allowing a 45 minute reserve, what is the maximum duration?

Answer 23

Five hours 15 minutes

Question 24

What speed will give you the best glide ratio?

Answer 24

2650 lbs 73 KIAS 2250 lbs 67 KIAS 1850 lbs 61 KIAS

Question 25

What is the octane rating and color of the fuel used by the aircraft?

Answer 25

100LL Blue

Question 26

What weight of oil is used?

Answer 26

MIL -L-6082 All temperatures use SAE 20W-50

Question 27

Is the landing gear fixed manual hydraulic or electric?

Answer 27

The landing gear extension, retraction, and maingear down lock release operation is accomplished by hydraulic actuators powered by an electrically driven hydraulic power pack. The power pack is located aft of the firewall between the pilots and copilots rudder pedals. The hydraulic system fluid level maybe checked by utilizing the dipstick located on the top left side of the powerpack adjacent to the motor mounting flange. The system should be checked at 25 hour intervals.

Question 28

If retractable what is the backup system for lowering the gear?

Answer 28

An emergency hand-operated hydraulic pump located between the front seats, is provided for manual extension of landing gear in the event of the hydraulic system failure. The landing gear cannot be retracted with the hand pump.

Question 29

What is the maximum demonstrated allowable Crosswind component for the aircraft?

Answer 29

15 KIAS

Question 30

How many persons will the aircraft safely carry with full fuel?

Answer 30

3

Question 31

What is the maximum allowable weight the aircraft can carry in the baggage compartments?

Answer 31

200lbs

Question 32

What take off distance is required to clear a 50 foot obstacle at maximum gross weight at a pressure altitude of 5000 feet and 90°F? (Assume no wind and a hard surface runway)

Answer 32

3550 ft

Question 33

What take off distance is required to clear a 50 foot obstacle at maximum gross weight at a pressure altitude of sea level and 90°F? (Assume no wind and a hard surface runway)

Answer 33

2100 feet

Question 34

Does high humidity increase or decrease the takeoff distance?

Answer 34

Increase