Systems Flashcards

(39 cards)

1
Q

The Cessna 172S Skyhawk is powered by a…

with a ____ ________ lubricating system

A

Lycoming
Horizontally opposed
Air cooled
Naturally aspirated
Direct drive
Engine

wet sump

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2
Q

The engine is a Lycoming model ___-_____-____.

It is rated at ____ horsepower at ______ RPM.

A

IO-360-L2A

180
2700

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3
Q

Major accessories of the engine include a…

A

-starter and belt-driven alternator
-dual magnetos
-vacuum pumps
-engine driven fuel pump
-full flow oil filter mounted on the rear of the engine accessory case

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4
Q

The Skyhawk is equipped with what type of propeller?

It is _______ and it is ___ inches in diameter.

A

Two-bladed, fixed pitch, one piece forged aluminum alloy propeller

anodized

76

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5
Q

The Shyhawks landing gear is of the _______ type. It has a steerable _____ ______ and two main wheels.

Shock absorption is provided by the tubular ______ ______ main landing gear struts and the ___/___ nose gear shock strut.

A

tricycle
nose wheel

spring steel
air/oil

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6
Q

Each main gear has a __________ actuated brake on the _______ side of each wheel

A

hydraulically
inboard

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7
Q

Slips with full flaps should be avoided to avoid ________ _______.

A

elevator flutter

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8
Q

The Skyhawk is equipped with _______ driven vacuum pumps.

Analog avionics have ____ vacuum pumps.
G1000 avionics have ____ pump.

A

engine

two
one

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9
Q

The vacuum pumps are ___________, allowing a _____ ____ with a reduced chance of failed components from the pump fouling the ____________.

A

downstream
fail safe
gyroscopes

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10
Q

Skyhawks equipped with the NXi version of the G1000 ___ _____ have a vacuum system if the standby instrument is a….

A

do not
self contained electronic unit

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11
Q

The pitot-static system supplies ram air pressure to the ________ ________ and static pressure to the…

A

airspeed indicator

airspeed indicator, vertical speed indicator, and altimeter.

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12
Q

When using the alternate static source, the windows and cabin vents must be _______ to reduce the pressure differential between the cockpit and the atmosphere, reducing pitot-static _______.

A

closed
error

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13
Q

What kind of gas does the Skyhawk use?

What color is it?

A

100 Low Lead AVGAS

Blue

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14
Q

The Skyhawk has two ___ gallon vented fuel tanks.

How much is usable?
How much is unusable?

A

28

26.5 gallons
1.5 gallons

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15
Q

The fuel system consists of…

The engine-mounted portion of the fuel system consists of the…

A

Two vented fuel tanks
3 position selector valve
Fuel reservoir tank
Auxiliary fuel pump
Fuel shutoff valve
Fuel strainer

Engine driven fuel pump
Fuel/air control unit
Fuel flow transducer
Fuel distribution valve
Fuel injection nozzles

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16
Q

The auxiliary fuel pump is __________ driven.

17
Q

The Skyhawk is equipped with a ____ volt ________ ________ electrical system, powered by a ____-amp, engine driven alternator and a ____ volt battery.

A

28
Direct Current
60
24

18
Q

Power is supplied to most electrical circuits through a _____ primary bus bar, with an _________ bus wired between the two primaries to provide power to the…

A

split
essential

master switch
annunciation circuits
interior lighting

19
Q

An annunciation panel is located on the left side of the instrument panel and provides _______ caution messages and _____ warning messages for selected portions of the airplane systems.

The annunciation is designed to flash for ___ seconds before remaining _______ to gain the attention of the pilot.

A

amber
red

10
steady

20
Q

The BAT side of the MASTER switch controls the _________ and the ALT side controls the _________.

A

battery
alternator

21
Q

The Skyhawk is equipped with a _________ type stall warning system. The warning horn will result at ___ to ___ knots above the stall speed in all flight configurations

A

pneumatic
5 to 10

22
Q

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 _____ and _____ MHz, and may be checked in the first ___ minutes past the hour for no more than ___ sweeps.

A

121.5 and 243.0
5
3

23
Q

What are the 4 functions of engine oil?

A

-Engine lubrication
-Engine cooling
-Engine cleaning (removes sediment and debris)
-Seals the piston in the cylinder

24
Q

The engine should not be operated on less than ___ quarts of oil.

25
In the event that the alternator and main battery have failed the _________ _________ is available to supply power to the _________ bus.
standby battery essential
26
If the alternator has failed and the main battery runs out of power you will lose primary bus 1 and 2 and be using the standby battery and essential bus. What do you lose when the primary buses go offline?
12v cabin power Flaps Auxiliary fuel pump Pitot heat Interior lights Exterior lights
27
What runs off the essential bus?
PFD ADC, AHARS COMM 1 NAV 1 Standby indicator lights
28
The fuel/air control unit…
meters fuel flow in proportion to induction air flow.
29
What kind of flaps does the 172 have?
Slotted flaps
30
The fuel return system is designed to… Metered fuel is taken from the ____-____ _________ _____ and routed through the _____ ________ _____ to the _____ __________ _____. This results in ______ fuel operating temperatures, which minimizes the amount of fuel ______ generated in the fuel lines during ____ weather operations.
improve engine operation during extended idle operation in hot weather. fuel-air control unit fuel return line fuel reservoir tank lower vapor hot
31
G1000 The magnetometer provides ________ data to the AHRS.
heading
32
G100 If both GIA 63 (Integrated Avionics Units) fail, the AHRS and ADC still provide _____ to the displays but ___ navigation or communication capabilities are available.
data no
33
G1000 The ADC receives _____ and _______ system inputs as well as _____ input
pitot and static OAT
34
G1000 If your ADC fails you will see red ___ for…
airspeed altitude vertical speed OAT true airspeed
35
G1000 If your ADC fails, your transponder will no longer have what capability?
Altitude reporting capability
36
G1000 The AHRS provides what data to the PFD? What does the magnetometer do? What data does the magnetometer provide to the AHRS for display on the PFD?
Attitude Turn-rate Measures the vertical and horizontal components of the earth’s magnetic field Magnetic heading data
37
G1000 If the AHRS fails all attitude indications are replaced by a large, red ___ and the words…
X Altitude Fail
38
G1000 If the magnetometer fails, what data will you lose?
Heading data
39
Transformer Rectifier Units (TRUs) convert… Inverters convert…
AC generator output to DC. DC output to AC.