Showing posts with label private stage 1. Show all posts
Showing posts with label private stage 1. Show all posts

Monday, July 8, 2019

Ground lesson 1 - flight training

  • Introduction to Pilot resources
    • FAR/AIM
      • Federal Aviation Regulation / Aeronautical Information Manual
      • Part 61 - Certifications: pilots, flight instructors, and ground instructors 

        • 14 CFR subpart C - Student pilot
          • § 61.81 – Applicability.

        • 14 CFR Subpart E - Private Pilots
          • § 61.102 – Applicability.

      • Part 91 - General operating and flight rules


    • Role of the FAA
      • National authority with powers to regulate all aspects of civil aviation

    • Fixed base operators
      • Organization granted the right by an airport to operate at the airport and provide aeronautical services such as fueling, hangaring, tie-down and parking, etc.

    • Eligibility requirements for student pilots
      • Part 61.83
      • At least 16 years of age.
      • Be able to read, speak, write, and understand the English language.

    • Eligibility requirements for private pilots
      • At least 17 years of age.
      • Be able to read, speak, write, and understand the English language.
      • Receive a logbook endorsement from an authorized instructor who:
        • Conducted the training or reviewed the aeronautical knowledge areas listed in 61.105.

      • Pass the required knowledge test on the aeronautical knowledge areas listed in 61.105(b)
      • Receive flight training and a logbook endorsement from an authorized instructor who:
        • Conducted the training in the areas of operation listed in 61.107(b)
        • Certify that the person is prepared for the practical test

      • Meet the aeronautical experience requirements of this part that apply to the aircraft rating before applying for the practical test.
      • Pass the practical test on the areas of operations listed in part 61.107(b)
      • Hold a student pilot certificate. Sport pilot certificate, or recreational pilot certificate.

    • Types of training available
      • Part 61 or Part 141
        • Ground training
        • Flight training

    • Phases of training
      • Pre solo → 1st solo → Cross country → Practical test preparation

    • Private pilot privileges and limitations - FAR 61.113
      • Privileges
        • Act as PIC
        • Share expenses

      • Limitations
        • May not carry passengers or property for compensation or hire
        • In the FAR there are some exceptions

    • Aircraft requirements
      • ARROW
        • Airworthiness certificate - (FAR 91.203)
        • Registration (state / federal) - (FAR 91.203)
        • Radio license
        • pOh - (FAR 91.9)
        • Weight and balance - (FAR 23.1589)

    • Student pilot requirements - FAR 61.51 (i)
      • Smile
        • Student certificate
        • Medical certificate
        • ID
        • Logbook
        • Endorsements

    • Maintenance requirements
      • AVIATES
        • Annual inspection (FAR 91.409)
        • VOR check (30 days)
        • I00 hour inspection (for hire or flight instruction - FAR 91.409(b))
        • Airworthiness Directives (FAR part 39)
        • Transponder (24 months - FAR 91.413)
        • ELT (12 months - 

          FAR 91.207

           )
        • Static and Altimeter inspection  (24 months - FAR  91.411)

    • VFR requirements Day and Night
      • TOMATOFLAMES  –––––––––––––––––––––––––  FLAP

Airspeed indicator
Fuses (spares) or circuit breakers
Tachometers 
Landing light (if for hire)
Oil pressure
Anti Collision lights
Manifold pressure
Position lights
Altimeter 
Source of electricity
Temperature sensor (liquid-cooled)

Oil temperature (air cooled)

Fuel gauge

Landing gear position

Anti collision lights

Magnetic compass

ELT

Seat belts




    • Medical Certificate -

      FAR 61.23



       
  • Introduction to human factors
    • Aeronautical decision making
      • Pilot decisions and/or actions while flying
      • 75% of accidents are human factor related
      • Usually not a single decision, but a chain of events triggered by a number of factors
      • Decision making process
        • First step →  Problem definition
          • Recognizing that a change has occurred, or that an expected change did not occur

        • Second step → evaluate the need to react
          • Determine the action to resolve the problem in the time available
          • After the decision has been made, evaluate the outcome and see if additional steps must be taken
      • Decide model
        Detect
        Changes in the condition of flight
        Estimate
        The need for correction action 
        Choose
        Desired outcome of corrective action 
        Identify
        Corrective action needed for the situation 
        Do
        The necessary action 
        Evaluate
        The effect of the action 
      • PPP model
        Perceive →  Given set of circumstances 
        Process → By evaluating their inspection on flight safety
        Perform → Implementing the best course of action 
    • Crew resource management (CRM)
      • Team work
      • Use all resources available
      • Ask copilot for help
      • Try to stay 5 minutes ahead of the aircraft

    • Workload management
      • Stay ahead of the aircraft
      • Doing as much as possible in advance will reduce stress during high workload situations
      • Prioritize
      • ANC → aviate, navigate, communicate

    • Resource use
      • Be familiar with the aircraft equipment
      • Use any available resource provided in the aircraft

    • Pilot in command responsibilities - FAR 91.3/91.7/91.107
      • Directly responsible and final authority as to, the operation of the aircraft
      • In an in-flight emergency requiring immediate action, the pilot in command may deviate from any rule of this part to the extent required to meet that emergency 
      • Each pilot who deviates from a rule shall upon request of the administrator, send a written report of that deviation to the administrator.


    • Communication
      • Radio technique 
        • Proper communication is critical in IFR flight
        • Work on effective listening 
        • Watch out for similar call signs
        • Question anything you find confusing or unclear
        • Listen before you transmit to not step over other people 
        • Think before you transmit 
        • Read back frequency change , runway numbers
        • State altitude on initial contact 
          • ATC can compare reported altitude with transponder

      • Standard phraseology 
        • Immediately → execute without delay
        • “Climb at pilot's discretion “ → start/rate/temporarily level off is at your discretion 
          • Once an altitude is left, you may not return to that altitude


        • “When able” → pilot can delay, but should seek first opportunity to comply 
        • “Cruise 5000” → you can climb/descend and level off between MDA and 5000’
          • If you report leaving an altitude, you cannot return to that altitude


        • “Resume own navigation” → resume your own navigation responsibilities


    • Situational awareness
      • Know your position 
      • Know positions of other aircraft's 
      • Know the terrain
      • Pay attention to ATC
      • Keep track of weather and wind
      • Know your aircraft
      • Keep an eye out for other factors that can affect your flight


    • Alcohol, drugs, and performance - FAR 91.17
      • Illness and disease may affect your performance, as can the drug meant to fight them
      • Consider the illness you are treating, and the side effects of the drug you are taking
      • No person may act or attempt to act as a crew-member of a civil aircraft
      • Within 8 hours after the consumption of any alcoholic beverage
      • While under the influence of alcohol
      • While using any drug that affects the person's faculties in any way contrary to safety 
      • While having an alcohol concentration of 0.04 or greater in a blood or breath specimen


    • Aviation physiology
      • Performance and limitations of the body in the flight environment 
      • Pressure effects
        • As the aircraft climbs and descends, outside air pressure changes
        • Pressure can be trapped in the ear, teeth, sinus cavities, and others, causing pain


      • Motion sickness

      • Stress 
      • Fatigue


    • Fitness for flight
      • I.M.S.A.F.E
        • Illness/ medication/ stress/ alcohol/ fatigue/ eat, emotion.



.

Ground lesson 2 - Airplane systems & flight inst

  • Airplane
    • Fuselage
      • Houses the cabin/cockpit
      • Semi Monocoque structure
      • Strong but can't tolerate dents



    • Wings
      • When air flows around the wings, it generates lift
      • Attached to the wings you have ailerons and flaps
        • Ailerons
          • Move in opposite directions to allow the aircraft to turn

        • Flaps
          • Move simultaneously to increase the lift force for takeoff, landings, and maneuvers.


    • Empennage
      • Typically consists of vertical stabilizer, rudder, horizontal stabilizer, and the elevator
      • They help steady the aircraft
      • The rudder can be used to move the nose left and right
      • The elevator can be used to move the nose up and down


    • Landing gear
      • Absorbs landing loads and supports the airplane on the ground
      • Attached to the strut which absorbs impacts


    • Engine/propeller
      • Primary function of the engine is to provide power to the propeller
      • The propeller translates the rotating force of the engine into a forward acting force called thrust.


    • POH
      • Most of the pertinent info about a particular make and model of airplane can be found in the POH




  • Powerplant and related systems
    • Reciprocating engines (piston)
    • Four stroke cycle
      • Intake (fuel/ air)
      • Compression
      • Ignition
      • Exhaust


  • Cessna 152 engine
    • Engine Manufacturer
      • Avco Lycoming.
Image result for cessna 152 engine diagram
    • Engine Model Number
      • O-235-L2C.


    • Engine Type
      • Normally-aspirated - air intake depends solely on atmospheric pressure
      • Direct-drive - power straight from the engine crankshaft to the prop
      • Air-cooled
      • Horizontally opposed
      • Carburetor equipped
      • Four-cylinder engine with 233.3 cu. in displacement.


    • Horsepower Rating and Engine Speed: HO rated BHP at 2550 RPM.


  • Induction system
    • Air filter
      • Intake air is filtered to prevent the intake from dust and other foreign objects
      • Located below the carburetor


    • Carburetor
      • Air is mixed with vaporized fuel as it passes through a venturi
      • The metered fuel/air mixture is then delivered to the cylinder intake


    • Carburetor ICE
      • Causes
        • Fuel vaporization and decreasing air pressure in the venturi causes a drop in temp.
        • If the air is moist, the water vapor in the air may condense
        • In low power settings, the butterfly valve creates a second venturi, ice is built there
        • Low temperatures ( see POH)

      • Indications
        • Decrease in engine RPM
        • Engine roughness

      • Prevention
        • Carb. heat should be used in low r.p.m settings or when ice is suspected



  • Ignition system
    • Provides the spark that ignites the fuel air mixture in the cylinder
    • 2 magnetos → 2 reasons
      • Redundancy
      • Efficiency
        • Two magnetos are connected in such a way that one drives the top spark plugs and the other the bottom plugs.
        • The magnetos generate power independently of the aircraft electrical system, so that in the event of flat battery during flight the engine will keep running. 


    • 2 spark plugs in each cylinder
      • Two spark plugs and separate ignition circuits are used per cylinder for redundancy, safety and better ignition and combustion of the mixture



  • Fuel system
    • Consists of
      • Fuel tanks
      • Fuel quantity gauge
      • Shut-off valve
      • Fuel filter
      • Fuel line to the engine
      • Possibly a primer and fuel pumps


    • Fuel travels from the fuel tank through a shut-off valve, which provides a means to completely stop fuel flow to the engine in the event of an emergency or fire
    • Primer allows fuel to be pumped directly into the intake port of the cylinders prior to engine startImage result for c152 fuel system

    • Gravity flow fuel system
      • Fuel grade
        • Av gas - 100LL - light blue


    • Fuel tanks
      • 26G total

      • 24.5 G usable
        • Usable fuel
          • Guaranteed to get to your engine anywhere inside your normal operating limits
            • 30 degrees nose up and nose down, 60 degree banks.

        • Unusable fuel
          • Not guaranteed to make it to your engine in those conditions.
          • The fuel pickup is not at the absolute bottom of the tank. Some space is left in case there is some water or sediment.

    • Fuel shutoff valve → enables and disables fuel flow out of the tank


  • Refueling
    • Use a ground wire to reduce static electricity and possible spark between refueling equipment and aircraft.
    • Make sure you are using the proper grade fuel. 


  • Oil system
    • Oil cleans and lubricates(cools) the engine
    • Improves efficiency by provides seal between cylinder walls and piston
    • Oil level
      • Minimum - 4qt
      • Maximum - 6qt


    • Gauges
      • Temperature gauges
        • If oil temp. to low
          • Not enough lubrication
          • High oil pressure


        • If oil temp to high
          • Oil loses the capability of lubrication
          • Low oil pressure


  • Cooling system
    • The combustion process that takes place in the engine produces intense heat
    • Excessively high engine temp. can result in loss of power, high oil consumption, and engine damage.
    • Outside air usually enters the engine compartment through an inlet behind the propeller hub




  • Exhaust system
    • Vent burned gas
    • Provide cabin heat
    • Defrosting the windscreen


  • Propellers
    • Provides thrust
    • Speed varies along the propeller blade span
    • Blade twist allows more uniform thrust throughout most of the length of the blade
    • There are Fixed pitch propeller and constant speed propellers


  • Propeller hazards
    • Provide your passenger with a thorough briefing so they stay clear of the propeller


  • Electrical system
    • Battery
      • 24V/ 25A
      • Needed to start engine
      • Provides backup power


    • Alternator
      • 28V/ 60A
      • Driven by the engine
      • Supplies electrical system with power
      • Charges the battery
      • Over-voltage relay → turn off the alternator when it is producing to much power


    • Bus bar
      • Alternator delivers direct current to the bus bar
      • Bus bar distributes the current to various electrical components
      • Ammeter
      • Monitors the electrical current in amperes within the system


    • Master switch
      • Controls entire electrical system.
      • Circuit breakers
      • Used to protect various components from overload or short
      • Circuit will continue to pop out, indicating an electrical problem


  • ISA - International standard atmosphere
    • Used by aviation
      • Calibrate instruments
      • Determine aircraft performance 


    • ISA standard day
      • Based on sea level
        • Temp. is 15ºC
        • Pressure is 29.92 inches of mercury 


    • Standard lapse rate
      • Temp. 2ºC per 1000 feet
      • Pressure 1’’ per 1000 feet


  • Flight instruments
    • Pitot static system
      • Pitot tube
        • Dynamic pressure enters (ram air)
        • Drain hole
        • Some aircrafts have pitot heat
        • Used by airspeed indicator


      • Static port
        • Measures static pressure
        • Used by ASI, VSI, and ALT




    • Airspeed indicator
      • Function
        • Indicates the speed of the aircraft through the air
        • Compares dynamic pressure with static pressure
        • The greater the difference, the greater the speed




      • Different airspeeds
        • Indicated airspeed
          • Reading on the ASI
        • Calibrated airspeed
          • Airspeed corrected for installation and instrument error

             
        • True airspeed
          • Airspeed relative to surrounding air
        • Ground speed
          • Speed over ground
    • Altimeter
      • Function
        • Measures the difference between static pressure and altimeter setting
        • Static port connected to the housing
        • Wafer has set pressure

      • Different altitudes
        • Indicated altitude
          • Reading on the altimeter


        • Absolute altitude
          • Altitude above the ground


        • True altitude
          • Altitude above sea level


        • Pressure altitude
          • Altitude corrected for non standard pressure


        • Density altitude
          • Altitude corrected for nonstandard temperature 


    • Vertical speed indicator
      • Function
        • Displays rate of climb/ descent
        • Measures how fast the static pressure increases and decreases
        • Static pressure enters diaphragm which instantly compresses/ decompresses
        • Static pressure also enters VSI housing through calibrated leak





    • ICING
      • Pitot tube ice
        • Only affects the airspeed indicator
        • Pitot + drain clogged = ASI works as altimeter
          • Higher altitude = higher airspeed


      • Pitot tube ice, drain cleared
        • Drain hole lets the pressure out, airspeed drops to zero


      • Static port ice
        • Affects ASI, ALT, VSI
        • ASI
          • Works normal at altitude it froze at
          • Higher airspeed at lower altitude, lower airspeed at higher altitude 


        • ALT
          • Freezes at current altitude 


        • VSI
          • Shows zero, senses no difference in pressure


        • Alternate static source
          • Break the VSI glass
          • ASI and ALT will show higher than normal



  • Magnetic compass
    • Function
      • Self contained
      • Aircraft rotates around the compass card


    • Magnetic fields of the earth
      • The earth is a huge magnet surrounded by a magnetic field made up of lines of flux
      • These lines leave magnetic north pole and reenter the south pole 


    • Variation
      • Angle between magnetic north and true north


    • Deviation
      • Compass errors caused by magnetic disturbances from electrical and metal components in the aircraft
        • Magnets installed in housing to compensate for the error
        • Correction is placarded on the compass




    • Oscillation
      • Erratic movements of the compass card
      • Turbulence , control inputs 


    • Magnetic dip
      • Tendency of the north seeking needle to deflect downward as it approaches the north pole
      • Flux is Perpendicular at the magnetic north pole
        • Strong deflection 


      • Flux is parallel at the equator
        • No dip error


      • Dip compensating weight at the “south end





    • Dip errors
      • Acceleration / deceleration errors
        • Because of the weight that compensates for magnetic dip
        • Most noticeable on easterly or westerly headings
        • None at north or south headings
        • ANDS
          • accelerate north/ decelerate south





    • Turn errors
      • Most noticeable when turning to/from a north or south heading, none at east/west
      • UNOS
        • Undershoot north, overshoot south
        • When on a south heading and turning north, needle leads