C172SP

Question 1

Vno

Answer 1

129KIAS

Question 2

Max crosswind component

Answer 2

15kts

Question 3

Va and turbulence penetration speed

Answer 3

1159kg: 105kts
1000kg: 98kts
863kg: 90kt

Question 4

Vs

Answer 4

Flaps up: 53kts
Flaps down: 48kts

Question 5

Vx

Answer 5

62kts

Question 6

Vy

Answer 6

74kts

Question 7

Vfe

Answer 7

10 degrees: 110kts
10 - 30: 85kts

Question 8

Vne

Answer 8

163kts

Question 9

Max load factor flaps up - Normal category

Answer 9

+3.8g, -1.52g

Question 10

Max load factor with flaps down - Normal category

Answer 10

+3g

Question 11

Max load factor flaps up - utility category

Answer 11

+4.4g, -1.76g

Question 12

Max load factor flaps down - utility category

Answer 12

+ 3g

Question 13

Best glide speed

Answer 13

68kts

Question 14

RPM used to check the ignition system

Answer 14

1800RPM

Question 15

Acceptable drop and difference in magnetos during test

Answer 15

individual drops not greater than 150RPM.
No greater than 50RPM difference

Question 16

Describe the leaning procedure in a cruise

Answer 16

Turn the mixture counterclockwise until EGT reaches the peak and the clockwise until peak temp is -50.

Question 17

Max ramp weight

Answer 17

1162kg

Question 18

Max TO weight

Answer 18

1159kg

Question 19

Max landing weight

Answer 19

1159kg

Question 20

max baggage weight

Answer 20

BA1: 54kg
BA2: 22kg

Combined 54kg

Question 21

What are the weight limitation in the utility category?

Answer 21

Ramp weight: 1003kg
TO and LDG: 1000kg

Question 22

Correct grade of fuel

Answer 22

100LL (Green)
Alternate is 100grade AVGAS (Blue)

Question 23

Total usable fuel

Answer 23

200L

Question 24

Total fuel (including unusable)

Answer 24

212L

Question 25

Minimum amount of oil

Answer 25

5 quarts

Question 26

Maximum amount of oil

Answer 26

8 quarts

Question 27

How much BHP does the power plant produce?

Answer 27

180BHP @ 2700RPM

Question 28

Max continuous power

Answer 28

2700RPM

Question 29

Flap range

Answer 29

0 - 30

Question 30

Wing span

Answer 30

11m

Question 31

Sources of power

Answer 31

Main battery, alternator, standby battery

Question 32

DC system voltage

Answer 32

28V

Question 33

How long can the standby battery supply power for?

Answer 33

at last 30mins

Question 34

Which instruments are operating gyroscopically?

Answer 34

Standby AH (engine driven vacuum)

Question 35

Emergency procedure for engine fire on the ground

Answer 35

Magnetos START IF ENGINE STARTS: power to 1800RPM for a few minutes then shutdown and secure engine IF ENGINE DOES NOT START: Throttle FULL Mixture CUTOFF Magnetos START Fuel shutoff valve OFF Fuel pump OFF Magnetos OFF Standby battery OFF Master OFF Secure engine and use fire extinguisher

Question 36

Emergency procedure for electrical fire

Answer 36

Standby battery OFF Master switch OFF Vents, cabin air and heat CLOSED Use fire extinguisher Avionics OFF All switches except magneto's OFF Vents OPEN Check circuit breakers Master ON Standby battery ON Avionics ON

Question 37

Engine failure after take off

Answer 37

1. Lower the nose – Glide attitude 2. Close the throttle 3. Select a landing area 4. Landing area should be within 30° of the nose 5. Set and trim for glide 6. Lower flap as required 7. Conduct C-F-M checks 8. Fuel on both, shut off not engaged, sufficient quantity 9. Mixture full rich 10. Mayday call 11. Shutdown checks