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CESSNA172R-SET2
1.
During cold weather operations time required for oil pressure to get registered is
a) 30 seconds
b) 45 seconds
c) 60 seconds
d) 90 seconds
2.
Propeller ground clearance for C172R is
a) 11”
b) 11.25”
c) 12”
d) 12.5”
3.
In event of alternate static door open ASI and altimeter error are:
a) ASI: 9 KIAS Altimeter: 30 feet
b) ASI: 6 KIAS Altimeter: 15 feet
c) ASI: 20 KIAS Altimeter: 60 feet
d) ASI: 15 KIAS Altimeter: 50 feet
4.
Minimum turning radius from pivot point to outboard wing tip is
a) 36 feet 6 inches
b) 30 feet 0 inches
c) 27 feet 5.5 inches
d) 28 feet 6 inches
5.
Abrupt use of flight controls is prohibited beyond
a) 129 KIAS
b) 85 KIAS
c) 99 KIAS
d) 103 KIAS
6.
Yellow arc range on the ASI is from
a) 33 KIAS to 85 KIAS
b) 129 KIAS to 163 KIAS
c) 44 KIAS to 129 KIAS
d) 20 KIAS to 33 KIAS
7.
Minimum oil pressure is
a) 20 psi
b) 50 psi
c) 14 psi
d) 10 psi
8.
During preflight inspection which annuciator should not be displayed
a) Low vacuum annunciator
b) Oil pressure annunciator
c) Low Fuel L and Low Fuel R annunciator
d) All the above
9.
Proper action to be taken in case of voltmeter reading in excess of 31.5 volts is
a) Switch off Master Switch (Alt. and Bat.) and land as soon as practical
b) Switch off Master Switch (Alt. only ) and land as soon as possible
c) Switch off Master Switch (Bat. only) and land as soon as possible
d) Switch off Master Switch (Alt. only) and land as soon as practical
10.
In event of alternator failure
a) Direction Indication Gyro may show error of more than 25o
b) Magnetic Compass may show error of more than 25o
c) Standby attitude indicator may not be relied upon
d) ASI may show error upto 6 KIAS
11.
For maximum cabin heating
a) Cabin heat knob fully out and cabin air knob fully in
b) Cabin Heat knob fully in and cabin air knob fully in
c) Cabin Heat knob fully out and cabin air knob fully out
d) Cabin Heat knob fully out and cabin air knob fully out
12.
Attitude indicator bank markings are
a) 10o, 15o, 30o, 45o and 90o
b) 10o, 20o, 30o and 60o
c) 10o, 15o, 30o, 60o and 90o
d) 10o, 20o, 30o, 60o and 90o
13.
Direction Indicating Gyro (DGI) shall be periodically aligned with magnetic compass to compensate for
a) Slip error
b) Precession Error
c) Vacuum error
d) Instrument Error
14.
Audible stall warning comes
a) 5-10 knots below stall speed
b) 5-10 knots above stall speed
c) 5 knots below stall speed
d) 5 knots above stall speed
15.
Maximum allowable speed for opening the window is
a) 163 Knots
b) 129 Knots
c) 110 Knots
d) 85 Knots
16.
Maximum slip-skid duration when flying on one tank dry is
a) 20 seconds
b) 30 seconds
c) 45 seconds
d) 60 seconds
17.
Unusable fuel quantity in each tank is
a) 3.0 gallons
b) 2.0 gallons
c) 1.5 gallons
d) 1.0 gallons
18.
Maximum oil pressure is indicated by lower end of upper red arc, in psi it is
a) 115
b) 120
c) 125
d) 130
19.
Fuel grade and color approved for use in Cessna 172 are
a) 100LL Green and 100 Blue
b) 100LL Blue and 100 Green
c) 100 Green only
d) 100LL Blue only
20.
Minimum oil quantity used for extended operations is
a) 3 quarts
b) 5 quarts
c) 6 quarts
d) 8 quarts
21.
Which engine oil is recommended for use after 50 hrs operations when oil consumption has stabilized
a) MIL – L 22851 or SAE J1899
b) MIL – L 6082 or SAE J1966
c) SAE J1966 only
d) MIL – L 6082 only
22.
Permitted concentration of fuel additive DiEGME is
a) 1 % to 1.5 %
b) 0.1% to 0.15 %
c) 0.01 % to 0.05 %
d) none of the above
23.
Maximum deflection of nose gear on ground is
a) 10o with rudder, 15o with rudder and brake
b) 10o with rudder, 20o with rudder and brake
c) 10o with rudder, 30o with rudder and brake
d) 10o with rudder, 40o with rudder and brake
24.
Flaps are equipped with mechanical stops at following extensions
a) 10o, 15o and 20o
b) 10o, 25o and 30o
c) 20o, 30o and 40o
d) 10o, 20o and 30o
25.
Landing gear shock absorption on C-172 are
a) Nose Gear: Air/Oil Strut; Main Gear: Tubular Spring
b) Nose Gear: Tubular Spring; Main Gear: Air/Oil Strut
c) Nose Gear: Tubular Spring;; Main Gear: Tubular Spring
d) Nose Gear: Air/Oil Strut; Main Gear: Air/Oil Strut
26.
Best rate of climb speed at sea level is
a) 65 KIAS
b) 70 KIAS
c) 79 KIAS
d) 80 KIAS
27.
Standard temperature lapse rate is
a) 1o Celsius per 1000 ft
b) 2o Celsius per 1000 ft
c) 3o Celsius per 1000 ft
d) 4o Celsius per 1000 ft
28.
The recommended starter duty cycle is
a) 10 sec. on 20 sec. off for two times then 10 minutes cooling
b) 10 sec. on 20 sec. off for three times then 10 minutes cooling
c) 10 sec. on 10 sec. off for three times then 10 minutes cooling
d) 10 sec. on 20 sec. off for three times then 30 minutes cooling
29.
Until 50hrs of operation, during cruise the max power setting should be
a) 60%
b) 70%
c) 80%
d) 90%
30.
Indication of carburetor icing in a fixed pitch propeller engine system and a constant speed propeller engine system is
a) Drop in rpm and rise in manifold pressure respectively
b) Rise in rpm and rise in manifold pressure respectively
c) Drop in rpm and drop in manifold pressure respectively
d) Rise in rpm and rise in manifold pressure respectively
31.
OAT/Voltmeter gauge may be tested by pushing the select button and holding it for
a) 10 seconds
b) 20 seconds
c) 30 seconds
d) 40 seconds
32.
If the microphone key is keyed in for 33 seconds or more
a) The VHF avionics goes to standby mode
b) The selected COM transmission is discontinued
c) The COM radio goes to low power mode
d) The COM1 radio selection switches to COM2 radio
33.
In the event of pitot tube blockage the ASI will give
a) Aural warning
b) Visual Flag Warning
c) Erroneous Reading
d) Reliable Reading
34.
The fuel filler tabs in the C172 fuel tanks can be used to fill fuel to a lower capacity enabling heavier cabin loading, this lower capacity is
a) 17.5 gallons in both tanks
b) 17.5 gallons in each tanks
c) 30.5 gallons in each tank
d) 18.5 gallons in each tank
35.
Pushing the upper control button on Voltmeter/OAT/Clock changes the display
a) Volts - oF – oC – Volts
b) Volts – oC – oF – Volts
c) Volts - oF – Volts – oC - Volts
d) Volts – oC – Volts – oF - Volts
36.
Indications of over priming are
a) High EGT
b) Puffing black smoke
c) RPM drop
d) Stuck Propeller
37.
Which of the following is acceptable during magneto drop check at 1800 rpm
a) Left: 1680 Right: 1750
b) Left: 1640 Right: 1690
c) Left: 1640 Right: 1640
d) Left: 1750 Right: 1730
38.
Correct procedure for applying parking brakes is
a) Pull parking brake lever and turn it 90 degrees
b) Pull parking brake lever and turn it 180 degrees
c) Press toe brakes and hold them, pull parking lever and turn it 90 degrees, release toe brakes
d) Press toe brakes and hold them, pull parking lever and turn it 180 degrees, release toe brakes
39.
The engine driver vacuum pump provides the suction necessary for operation of
a) Direction Gyro, Attitude Gyro, and Turn Coordinator
b) Direction Gyro, Attitude Gyro, Airspeed Indicator
c) Direction and Attitude Gyros only
d) None of the above
40.
Correct inflation pressures for nose wheel and main wheel are
a) 38 psi, 45 psi
b) 45 psi, 38 psi
c) 34 psi, 29 psi
d) 34 psi, 28 psi
41.
Normal fuel flow range is
a) 0 GPH to 6 GPH
b) 1 GPH to 11 GPH
c) 1 GPH to 6 GPH
d) 0 GPH to 11 GPH
42.
Which of the following is incorrect about ASI markings on C172
a) White arc: 33 – 85 knots
b) Green arc: 44 – 129 knots
c) Yellow arc: 129 – 163 knots
d) Red line: 166 knots
43.
On encountering icing conditions the appropriate course of action is
a) Increase engine power and cruise at airspeed above 110 knots
b) Turn back and change altitude
c) Extend flap to 20 degrees and maintain altitude
d) Declare emergency and land as soon as possible
44.
For best cooling during en-route climbs
a) Climb at Vy
b) Climb at Vx
c) Climb at a speed higher then Vy
d) Climb at 75-85 knots
45.
For easy start during cold weather operations
a) Manually cycle propeller in opposite direction of rotation
b) Manually cycle propeller in normal direction of rotation
c) Use primer pump for 6 seconds
d) Use primer pump for 10 seconds
46.
Operation at peak EGT provides
a) Worst fuel economy
b) Best fuel economy
c) Average fuel economy
d) None of the above
47.
Oil pressure gauge markings are
a) Lower red arc 0-25 psi : Green arc 50-115 psi: Upper red arc psi 115-120 psi
b) Lower red arc 0-20 psi : Green arc 60-115 psi: Upper red arc psi 115-120 psi
c) Lower red arc 0-20 psi : Green arc 50-115 psi: Upper red arc psi 115-120 psi
d) Lower red arc 0-20 psi : Green arc 50-110 psi: Upper red arc psi 110-120 psi
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