Checkride Prep Taken From Notes Flashcards

And a cumulative deck from notes taken in weaknesses.

1
Q

Systems: Type of Engine

A
F-Fuel injected
L-Lycoming
H-Horizontally Opposed
A-Air Cooled
N-Naturally Aspirated
D-Direct Drive
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2
Q

Engine Oil

A

15/50
It:
Cools, lubricates,reduces friction, seals, cleans

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3
Q

Oil System

A
Sump to
Strainer
Oil Pump
Bypass Valve (or if hot to oil cooler)
Filter
Pressure Relief Valve
Residual back to sump
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4
Q

The gyroscopic flight instruments

A

Turn coordinator
heading indicator
attitude indicator

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5
Q

Fundamental properties of gyroscopic action

A

Rigidity in space

Precession

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6
Q

What is rigidity in space as it pertains to gyroscopes

A

Refers to the principle that a gyroscope remains in a fixed position in the plane in which it is spinning

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7
Q

What is precession as it pertains to gyroscopes

A

Procession is a tilting or turning of a gyro in response to a deflective force, this Force when applied occurs at a 90° point later in the direction of rotation

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8
Q

Two types of turn indicators

A

Turn and slip indicator

Turn coordinators

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9
Q

Turn and slip indicator general function

A

Rotates in the vertical plane corresponding to the aircraft longitudinal axis.Uses a pointer call the turn needle to show the direction and rate of turn.

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10
Q

Turn coordinator general functions

A

The gimbal and a turn coordinator is canted therefore it’s gyro can sense both rate of roll and rate of turn.

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11
Q

Inclinometer general functions

A

Used to depict aircraft yaw. during coordinated straight and level flight, the force of gravity causes the ball to rest in the lowest part of the tube centered between the reference lines.

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12
Q

Attitude indicator general principles of function

A

Depicts miniature aircraft as in relation to the horizon. The gyro is mounted in a horizontal plane, the bar is fixed to the gyro and remains in horizontal plane as he aircraft is pitched or banked about its lateral a longitudinal axis. The aircraft actually rotates around the spinning gyro.

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13
Q

Diluted demand oxygen system

A

supply oxygen only when the user inhales through the mask. Can mix cabin air an oxygen or supply 100% oxygen. Tight seal and can be used up to 40,000 ft

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14
Q

Pressure demand oxygen system

A

Similar to diluted except the oxygen is supplied to the mask under pressure at cabin altitudes above 34000 ft. Oxygen tight seal positive pressure which allows a uses lungs to be pressurized with oxygen. Safer at altitudes above 40000 feet.

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15
Q

Continuous Flow oxygen system

A

Usually provided for passengers. Typically has a reservoir bag that collects oxygen from The continuous Flow oxygen system. Ambient air headed to the supplied oxygen during lesion after reserve back oxygen is depleted.

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16
Q

Electric pulse demand oxygen system

A

Deliver Oxygen by detecting the individuals inhalation effort. Only provide oxygen during initial portion of inhalation. Can reduce the amount of oxygen needed by 50 to 85% since oxygen is not wasted.

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17
Q

A narrower than usual runway illusion

A

Can create an illusion that the aircraft is higher than it actually is leading to a low approach.

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18
Q

A wider than usual runway illusion

A

Can create an illusion that the aircraft is lower than it actually is leading to a higher approach.

19
Q

A downsloping runway illusion

A

Can create the illusion that the aircraft is lower than it actually is leading to a higher approach

20
Q

Upsloping runway illusion

A

Can create the illusion that the aircraft is higher than it actually is leading to a lower approach

21
Q

Featureless terrain illusion

A

Can create an illusion that the aircraft is at a higher altitude than it actually is

22
Q

Haze illusion

A

Can create an illusion of being at a greater distance and height from the runway

23
Q

Fog illusion

A

Can create an illusion of pitching up

24
Q

Federal aviation regulations pertaining to drugs

A

61.53

Prohibited acting as pic four non medical conditions or taking medication or receiving another treatment whichresults in the person being unable to meet the requirements for the medical certificate necessary for the pilot operation

91.17

prohibits the use of any drug that affects the person’s faculties in any way contrary to safety

25
Q

Actions during a decompression sickness emergency

A

Put on oxygen if available switch to 100%
Being an emergency descent and landing soon as possible even if the symptoms disappeared during descent
If one of the symptoms of joint pain keep the affected area still
Apollo landing seek medical assistance from an FAA medical officer a m a military flight surgeon or a hyperbaric medicine specialist
Treatment may involve the use of a hyperbaric chamber

26
Q

Wait times after scuba diving

A

Altitudes of up to 8,000 feet is 12 hours after diving that does not require controlled ascend, and at least 24 hours after diving that does require controlled descent.

Waiting time before going to flight altitudes above 8000 feet should be at least 24 hours after scuba

27
Q

Pave checklist is for?

A

Hey wait a mitigating risk

28
Q

P in the pave checklist

A

Pilot am I ready for this trip in terms of experience recency currency physical and emotional condition
Go through I’m safe checklists

Illness
Medication
Stress
Alcohol (less then .04%bac or 8 hours bottle to throttle)
Fatigue
Emotion
29
Q

A in the pave checklist

A

You asked yourself:

Right aircraft for the flight
Familiar and current in the circuit
Remember performance figures based on new aircraft
is the aircraft equipped for the flight? instruments? lights navigation and communication equipment?
Can this aircraft use a runway available for the trip?
Can the aircraft carrier the plan load?
Can the aircraft operate at the altitudes required?
Does this aircraft have sufficient fuel capacity for the legs planned?
Does the fuel quantity delivered match the fuel quantity ordered?

30
Q

V in pave checklist

A

Environment like weather

Sky conditions:
Ceiling and visibility, winds at airport being used with crosswind component
Thunderstorm present or forecast?
Forecasted/current or possibility of icing?
Temperature/dew point spread

Terrain
Is a terrain mountainous?
Day or night flight
VFR IFR
Safe altitude on charts
Know your maximum elevation figures

Airport
Know the lights available at your destination and alternate airports
VASI/PAPI
No the instrument approaches available
Check notices to airmen foreclosed runways or airports and taxiways
Choose flight route wisely

Airspace
Survival gear for remote area flying or flying over water
check the air space and temporary flight restrictions along the route of flight

Nighttime
Be prepared to fly IFR
Will the flight conditions allow a safe emergency landing at night
check all aircraft lights interior and exterior for night flight carry two flashlights one fixture pre-flight and smaller when they can be dimmed and kept nearby

31
Q

E in the pave checklist

A

External pressures

Is someone winning at the airport for flights arrival
A passenger the pilot does not want to disappoint
Desire to demonstrate public qualifications
Impress someone
Get home-itis get there-is and let’s go-its

32
Q

5 hazardous attitudes and their antidotes

A

Anti-authority “don’t tell me”
Antidote: follow the rules they are usually right

Impulsivity “do it quickly”
Antidote: not-so-fast thing first

Invulnerability “it won’t happen to me”
Antidote: it could happen to me

Macho “I can do it”
Antidote: taking chances is foolish

Resignation “what’s the use”
Antidote: I’m not helpless I can make a difference

33
Q

How are the electric circuits applied

A

Supplied through a split primary busbar
Busbar 1
Busbar 2

34
Q

Primary bus 1

A
Turn coordinator 
Nav& control wheel 
map lights 
strobe/taxi lights
pitot heat
Avionics bus 2
Avionics fan 
GPS 
nav/com 1 
auto pilots 
ADF
35
Q

Primary bus 2

A
Instrument and ignition switch 
fuel pump (electric) 
landing lights 
flashing beacon 
flaps
Avionics bus 1
HSI and Gyro 
autopilot nav 2 
transponder 
navcom 2
36
Q

Essential cross-feed bus

A

To the various annunciators
glareshield interior instrument lights
to master switch

37
Q

Annunciator panel

A
Inputs come from
Fuel transmitter 
low oil pressure switch 
vacuum transducer 
alternator control unit ACU
38
Q

Engine instruments

A

Oil pressure / oil temperature
tachometer
exhaust gas temperature EGT
+ the oil pressure annunciator (on below 20psi)

39
Q

Lubrication system

A

Full pressure wet sump with aviation grade oil 8 quarts capacity ( 5-8 quarts operating range)

40
Q

Oil route through engine

A

Oil drawn from sump
to strainer
To engine driven oil pump
to bypass
Hot oil to oil cooler, then oil filter
Cold oil directly to full flow oil filter
To pressure relief valve (excess pressure routed back to sump)
To engine
Oil returns to sump by gravity

41
Q

Ignition and starting

A

2 engine driven Magneto’s two spark plugs per cylinder

42
Q

Fuel system

A
2 vented fuel tanks 1 per wing 5 drains per tank.
To fuel selector valve (1 drain here)
Fuel reservoir (1 drain here)
Auxillary fuel pump
Fuel shut off valve
Fuel strainer (1 drain here)
Engine driven pump
Fuel/air control unit
Fuel distribution valve
43
Q

Low voltage annunciator

A

Activate when voltage falls below 24.5 volts