Cessna C172S Open Book exam

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CESSNA 172S
OPEN BOOK EXAM - STUDENT VERSION
EXAMEN AVEC DOCUMENTATION
References:
Pilot's Operating Handbook
Cessna Skyhawk Model 172S (2004)
This open book exam is a self study guide that will help familiarize the pilot with the airplane’s
systems, operating limitations, normal and emergency procedures. It should be completed
prior to ground school.
Page 1

SECTION 1 (SYSTEMS)
1. Conventional control surfaces are operated by
(a)
(b)
(c)
(d)
Cables.
Pushrods.
Electrical power.
Hydraulics.
2. How is rudder trim accomplished
(a)
(b)
(c)
(d)
Rudder trim is optional in this aircraft.
Through a rudder trim tab.
By the use of a bungee in the control system.
The rudder trim tab is adjusted on the ground.
3. What precaution must be taken when moving the airplane around on the ground
(a)
(b)
(c)
(d)
Use a tow bar if available.
Use the wing struts as push points.
Do not use the vertical or horizontal surfaces.
All of the above.
4. What type of flaps are used and how are they operated
(a)
(b)
(c)
(d)
Simple flaps, manually operated.
Fowler flaps, electrically operated.
Single-slot type, electrically operated.
Split flaps, automatic operation.
5. Can we carry hazardous material or dangerous goods in the baggage compartment
Yes
No
6. Should a cabin door open in flight, what is the recommended speed
(a)
(b)
(c)
(d)
80 KIAS.
179 KIAS.
Any speed.
75 KIAS.
7. What type of engine powers the C172S
(a)
(b)
(c)
(d)
Continental O-300.
Continental IO-320.
Lycoming IO-360.
Continental O-320.
Page 2

8. What is the power rating at 2700 RPM
(a)
(b)
(c)
(d)
150 HP.
160 HP.
180 HP.
230 HP.
9. The engine of this aircraft is:
(a)
(b)
(c)
(d)
Normally aspirated and fuel injected.
Supercharged and carburetor equipped.
Normally aspirated and carburetor equipped.
Supercharged and fuel injected.
10. How is the oil pressure reading obtained
(a)
(b)
(c)
(d)
By a pressure-sensing switch at the oil pump outlet.
From a direct pressure oil line from the engine.
By a combination of pressure line/transducer.
Electrical wire from the main oil line.
11. If the air filter becomes blocked what will happen
(a)
(b)
(c)
(d)
Drop in RPM and 10% loss of engine power.
Drop in manifold pressure and 15 % loss of engine power.
Engine will stop.
Nothing.
12. Oil pressure is used by the propeller governing system.
True
Not applicable
False
13. What is the recommended oil level for extended flights
(a)
(b)
(c)
(d)
10 quarts.
9 quarts.
5 quarts.
8 quarts.
14. Carb heat is air heated by _________________ .
(a)
(b)
(c)
(d)
the carb heat control.
air passing through a shroud around the muffler.
the cabin heat control.
Not applicable.
Page 3

15. The types of fuels approved for this airplane are 100LL (blue) and 100 (green). What
is the total usable fuel quantity of an aircraft with the long range tanks
(a)
(b)
(c)
(d)
53 USG
48 USG
61 USG
56 USG
16. How is the left fuel tank vented
(a) Interconnecting line from the right fuel tank.
(b) From a vent line protruding under the left wing near the strut area.
(c) From the fuel caps.
(d) All of the above.
17. When should the fuel tanks be drained
(a)
(b)
(c)
(d)
After every refuelling
Before every flight
(a) and (b)
Only in cold weather
18. The electrical system is 28 vdc. Maximum alternator output is:
(a)
(b)
(c)
(d)
60 amps
14 amps
24 amps
28 amps
19. What important precaution should be taken prior to turning the master switch ON or
OFF.
(a)
(b)
(c)
(d)
Make sure the area ahead the prop is clear.
Wear a hard hat.
Make sure the avionics power switch is OFF.
The alternator is OFF.
20. The ammeter indicates_________ .
(a)
(b)
(c)
(d)
The load on the alternator.
The charging rate applied to the alternator.
The current in amps produced by the battery.
Flow of current to and from the battery.
21. What does the low voltage light indicate
(a)
(b)
That system voltage has dropped below normal
That the charging rate applied to the alternator is too high
Page 4

(c)
(d)
Current is removed from the alternator field.
All of the above.
22. How many external static ports are provided on this airplane
One.
Two.
23. An alternate static pressure source is provided. Where is it located
(a)
(b)
(c)
(d)
Under the cabin floor.
Below the Throttle.
Adjacent to the parking brake.
On the left cowling near the normal static source.
24. What instruments are vacuum driven
(a)
(b)
(c)
(d)
The attitude indicator and directional indicator.
The turn & bank indicator ant the attitude indicator.
The turn & bank indicator ant the directional indicator.
The standby attitude indicator.
25. The stall warning system:
(a)
(b)
(c)
(d)
Uses electrical power.
Is operated by air pressure only.
Uses a whistle.
Uses a red light on the upper instrument panel
SECTION 2 (LIMITATIONS)
26. Speed limits: Figure 2-1
Vne
Vno
Va (2550 lbs)
Vfe flaps 0-10 _______ flaps 10-30 _______
27. Engine limits: Figure 2-3
Maximum RPM: ______ RPM
RPM green arc: _______ RPM at sea level
Oil pressure green arc: _______ PSI
Page 5

28. Weight limits:
Maximum ramp weight: ______ lbs
Maximum landing weight: ______ lbs
Maximum weight in baggage area A and B:
____ lbs
SECTION 4 (NORMAL PROCEDURES)
29. What is the maximum demonstrated crosswind velocity
(a)
(b)
(c)
(d)
TakeOff 15 K / Landing 20 K
TakeOff 20 K / Landing 15 K
TakeOff 25 K / Landing 25 K
TakeOff 15 K / Landing 15 K
30. When must the Elevator Trim pre-flight be carried out (RFC Checklist)
(a) Before every flight
(b) Before every flight above FL250
(c) Before every landing
(d) During the After Start Check, before a flight when the Electric Trim is planned
to be used.
31. When carrying out the magneto check, what is the maximum permissible differential
between magnetos
(a)
(b)
(c)
(d)
50 RPM
100 RPM
150 RPM
200 RPM
32. At what speed is the nose wheel lifted off for takeoff
(a)
(b)
(c)
(d)
60 KIAS
55 KIAS
57 KIAS
50 KIAS
33. What is the flap setting used for a short field takeoff
(a) 10°
(b) 20°
(c) Between 10 and 20°
(d) 0°
Page 6

34. At what speed should the flaps be retracted after takeoff
(a)
(b)
(c)
(d)
Between 60 and 85 KIAS
95 KIAS
80 KIAS
60 KIAS
35. What is the normal enroute climb speed
(a)
(b)
(c)
(d)
70 KIAS
70-85 KIAS
72-78 KIAS
90 KIAS
36. What is the Vy climb speed at sea level
(a)
(b)
(c)
(d)
80 KIAS
74 KIAS
70 KIAS
85 KIAS
37. What is the normal approach speed with full flaps
(a)
(b)
(c)
(d)
70 KIAS
60-70 KIAS
70-80 KIAS
60 KIAS
38. What is the normal approach speed for a short field landing
(a)
(b)
(c)
(d)
61 KIAS
70-80 KIAS
80 KIAS
70 KIAS
Page 7

39. In a balked landing, what wing flap setting should be selected and at what speed
should the airplane be climbed at
(a)
(b)
(c)
(d)
10° and 55 KIAS
20° and 60 KIAS
40° and 55 KIAS
20° and 55 KIAS
40. What is the time limit for the oil pressure to show an indication in the summer (per
RFC Checklists)
(a)
(b)
(c)
(d)
10 secs
20 secs
30 secs
60 secs
41. What is the maximum amount of flap deflection approved for use during take-off
(a) 10°
(b) 20°
(c) 30°
(d) 40°
42. What is the best angle of climb speed with flaps up
(a)
(b)
(c)
(d)
60 KIAS
70-80 KIAS
57 KIAS
62 KIAS
43. What flap setting is recommended for crosswind landing
(a)
(b)
(c)
(d)
Maximum flap setting.
Maximum flap setting for the field length.
Minimum flap setting.
Minimum flap setting for the field length
Page 8

SECTION 3 (EMERGENCY PROCEDURES)
44. Where is the fire extinguisher located
(a)
(b)
(c)
(d)
Behind the pilot’s seat.
Between the two front seats.
Under the pilot’s seat.
Under the right front seat
45. What is the glide speed with flaps up
(a)
(b)
(c)
(d)
68 KIAS
75 KIAS
89 KIAS
100 KIAS
46. Describe the procedure for an engine failure during flight.
47. Describe the procedure for an engine fire in flight.
48. Describe the procedure for an electrical fire in flight.
49. Describe the procedure for a cabin fire in flight.
Page 9