Cessna 182 Handbook Exam
- 1.Maximum take-off mass is
- A.
1750 lbs (794kg)
- B.
2450 lbs (1111kg)
- C.
2800 lbs (1270kg)
- D.
4000 lbs (1814kg)
- 2.Service ceiling is
- A.
12 500 feet
- B.
15 900 feet
- C.
18 900 feet
- D.
19 500 feet
- 3.Empty mass (Standard aircraft)
- A.
1691 lbs (767 kg)
- B.
2100 lbs (953 kg)
- C.
1620 lbs (735kg)
- D.
2303 lbs (1045 kg)
- 4.Maximum baggage mass
- A.
50 lbs
- B.
100 lbs
- C.
120 lbs
- D.
150 lbs
- 5.Maximum engine brake horse power at 2600 RPM
- A.
180hp
- B.
200hp
- C.
230hp
- D.
250hp
- 6.Vr
- A.
55 mph
- B.
60 mph
- C.
65 mph
- D.
67 mph
- 7.To minimize engine wear manifold pressure and RPM should be reduced after take-off to
- A.
25 " and 2500 RPM
- B.
23” and 2450 RPM
- C.
21" and 2450 RPM
- D.
23" and 2500 RPM
- 8.Approach speed with full flaps
- A.
70 mph
- B.
80 mph
- C.
85 mph
- D.
90 mph
- 9.Fuel capasity is
- A.
79 gallons usable and 2 gallons unusable
- B.
79 gallons usable and 1.5 gallons unusable
- C.
77 gallons usable and 1.5 gallons unusable
- D.
77 gallons usable and 2.0 gallons unusable
- 10.Prolonged uncoordinated flight, such as slips or skids can cause engine stoppage
- A.
If fuel pump is not being operated
- B.
If there is less than 1/4 of fuel in the tanks
- C.
If there is less than 1/3 of fuel in the tanks
- D.
If fuel selector should be selected for either left or right tank
- 11.Which is correct regarding the fuel system
- A.
Fuel from each wing taken is drawn by aid of fuel pump to a selector valve. From there it flows through a fuel strainer and carburetor to the engine manifold.
- B.
Fuel from each wing taken flows by gravity to a fuel strainer. From there it flows through a selector valve and carburetor to the engine induction system.
- C.
Fuel from each wing taken flows by gravity to a selector valve. From there it flows through a fuel strainer and carburetor to the engine manifold.
- D.
Fuel from each wing taken flows by gravity to a selector valve. From there it flows through a fuel strainer and carburetor to the engine induction system.
- 12.Fuel tank selector must be selected for
- A.
Both tanks
- B.
The left tank
- C.
The right tank
- D.
The fullest tank
- 13.Electrical system is
- A.
14 volt and storage battery is 12 volt
- B.
24 volt and storage battery is 22 volt
- C.
12 volt and storage battery is 14 volt
- D.
24 volt and storage battery is 20 volt
- 14.During engine start puffs of black smoke from the exhaust stack indicate
- A.
A too weak mixture
- B.
Water in the fuel
- C.
Worn piston rings
- D.
Over priming or flooding
- 15.During magneto check on the ground
- A.
RPM must drop but should not be more than 50 RPM
- B.
RPM should not drop more than 50 RPM
- C.
RPM must not increase more than 50 RPM
- D.
RPM must drop by 50 RPM
- 16.Vx is (IAS in mph)
- 17.Vy is (IAS in mph)
- 18.For short field take-off which of the following flap settings should be used
- A.
10°
- B.
20°
- C.
30°
- D.
40°
- 19.Load factors are
- A.
+4.4 to -1.52
- B.
+4.4 to –1.76
- C.
+3.8 to -1.76
- D.
+3.8 to -1.52
- 20.Vne is (IAS in mph)
- 21.Vno is (IAS in mph)
- 22.Vfe is (IAS in mph)
- 23.Va is (IAS in mph)
- 24.Minimum oil quantity in quarts
- 25.Vs1 is (IAS in mph)
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