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Cessna 172 SOP Infinity Flight Group Questions With Complete Solutions $12.99   Add to cart

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Cessna 172 SOP Infinity Flight Group Questions With Complete Solutions

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Cessna 172 SOP Infinity Flight Group Questions With Complete Solutions

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  • September 3, 2024
  • 26
  • 2024/2025
  • Exam (elaborations)
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  • Cessna 172
  • Cessna 172
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Cessna 172 SOP Infinity Flight Group Questions With
Complete Solutions

Define and identify Va speed Correct Answers Maneuvering
speed. 99-105 KIAS

Define and identify Vfe speed Correct Answers Maximum flap
extended speeds:
10 degrees: 110 KIAS
20 degrees: 85 KIAS

Define and identify Vg speed Correct Answers Best glide
speed. 68 KIAS

Define and identify Vne speed Correct Answers Never exceed
speed. 163 KIAS

Define and identify Vno speed Correct Answers Maximum
structural cruising speed. 129 KIAS

Define and identify Vr Speed Correct Answers Rotation speed
- 55-60 KIAS

Define and identify VS1 speed Correct Answers Stalling speed
or the minimum steady flight speed obtained in a specific
configuration. 48 KIAS

Define and identify VSo speed Correct Answers Stalling speed
or minimum steady flight speed in the landing configuration. 40
KIAS

,Define and identify Vx speed Correct Answers Best angle of
climb speed. 62 KIAS

Define and identify Vy speed Correct Answers Best rate of
climb. 74 KIAS

Describe heater Correct Answers Cabin air knob controls
volume of airflow into the cabin.

Describe the brakes Correct Answers Hydraulically actuated,
main wheel single disc brakes controlled by master cylinders
attached to pedals

Describe the electrical system Correct Answers 28 volt, direct-
current system powered by 60 amp alternator and 24 volt battery

Describe the ELT Correct Answers A remote
switch/annunciator is installed on the top center location of the
co-pilots instrument panel for control of the ELT from the
cockpit.

The ELT emits an omnidirectional signal on 121.5 and 243.0
MHz, and may be checked in the first five minutes past each
hour for no more than three weeks.

Describe the engine Correct Answers Lycoming, horizontally
opposed, air cooled, normally aspirated, direct injected

Major components include: starter, belt driven alternator, dual
magnetos, vacuum pumps, engine driven fuel pump, and a full
flow oil filter

, Describe the flaps Correct Answers The Skyhawks slotted
wings flaps are extended or retracted via electrical power. The
flaps may extend to 10, 20, or 30 degrees.

Describe the fuel system. Correct Answers Uses 100LL avgas,
has two 28 gallon vented integral. Three gallons total unusable.

Describe the landing gear Correct Answers Tricycle Type
Steerable Nosewheel

Describe the pitot static system Correct Answers Pitot tube on
the left wing for ram air, static port on left side (backup static
port in the aircraft), electrically heated

Describe the propeller Correct Answers Two blade, fixed pitch,
one piece forged aluminum alloy propeller. 76 inches in
diameter.

Describe the vacuum system. Correct Answers With the G1000
aircraft, there is only one vacuum pump which provides the
suction required for gyroscopic instruments such as the heading
and attitude indicator.

If an aircraft has a self contained electronic standby instrument
there is no vacuum system.

Describe the warning horn Correct Answers Pneumatic type
stall warning system consisting of an inlet in the leading edge of
the left wing, and an air operate horn near the upper left corner
of the windshield.

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