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PAVE
PILOT IMSAFE
AIRCRAFT AAVIATE, Weight and Balance, Walkaround/Preflight, ARROW
ENVIRONENT NWKRAFT
EXTERNAL PRESSURES
IMSAFE
Illness Medication Stress Alcohol Fatigue Emotions/eating
AAV1ATE
Airworthiness Directives
Annual Inspection - 12 CM (Every Plane)
VOR Check - 30 Days (IFR Only)
100 Hour - Compensation or Hire
Altimeter and Pitot Static System - 24 CM
Transponder - 24 CM
ELT - 1 hr of use, half of the battery life, 12 CM
Airframe and Powerplant Mechanic/with an Inspectors Authorization (A and P/APIA)
A and P - 100 hour
APIA - Annual
ARROW
Airworthiness - Doesn't expire as long as AD's are complied with
Registration - 7 yrs
Radio Operating License - International Only
Operation Limitations - POH
Weight and Balance - POH
NWKRAFT
NOTAMS
Weather
Known ATC Delays Runway
Lengths and Widths
Alternates Fuel Req
Takeoff and Landing Distance
4 Stages of an Engine
Intake - Air comes in (suck)
Compression - Air is compressed (squeeze)
Combustion - Fuel and Air mix then ignite (bang)
Exhaust - Fumes leave the cylinder (blow)
ATOMATOFLAMES (DAY VFR REQ) 91.205
Airspeed Indicator
Tachometer Oil
Pressure Gauge (each engine)
Manifold Pressure Gauge (each engine)
Altimeter
Temperature Gauge (each LIQUID COOLED engine)
Oil Temperature Gauge (each engine)
Fuel Gauge (each fuel tank)
Landing Gear Position Indicator
Anti Collision Lights Magnetic
Compass
ELT
Safety Belts
FLAPS (NIGHT VFR REQ + DAY)
Fuses (circuit breakers)
Landing Light
Anti-Collision Lights
Position
Lights Source of Electricity
SAFETY
Seat Belts
Air Vents
Fire Extinguisher
Exit Door(s)
Talking Your Questions
p100i Avionics
G3X - PFD
G5 - Standby Instrument
GNX375 - Transponder
Pitot Static Systems
Pitot - Airspeed Indicator
Static - Airspeed Indicator, Vertical Speed Indicator (VSI), Altimeter
Airspeed Indicator (ASI)
Pitot and Static ports
Pitot tube connect to the diaphragm type balloon (ram air pressure)
Static port provides air pressure to the rest of the empty space (static pressure)
Altimeter (ALT)
Works similarly to the airspeed indicator
However, the diaphragm in the altimeter is pre-sealed and is referred to as an Aneroid Wafer
After we set the pressure in the kollsman window, the rise and drop in the air pressure applies a varying force upon the aneroid wafer, and depending on the expansion or contraction of the wafer inside of the altimeter, it gives us the proper reading
Vertical Speed Indicator (VSI)
Compares static air pressure to a change in static air pressure
Two lines of static pressure are connected to the VSI and the change in static pressure is measured by a "Calibrated Leak"
As we ascend or descend, higher pressure air always wants to go from low to high, same applies here
Clogged Pitot Tube
Only the airspeed indicator will be affected
No ram air pressure is being sent to the diaphragm
The diaphragm will cease to expand and contract with airspeed changes
Making the airspeed indicator act like an altimeter
Note: if the pitot tube has a drain hole that is unclogged, the ASI will drop to zero
Clogged Static Port (ASI)
The static port gets clogged while flying at 5,000' MSL
This would trap 5,000' air in the static area of the airspeed indicator and cause the diaphragm to expand and contract incorrectly at higher and lower altitudes
Clogged Static Port (ALT)
The altimeter will freeze at the altitude where the clog occurred
No changing static pressure inside the instrument casing
No expanding and contracting of the pre-sealed aneroid wafer
Clogged Static Port (VSI)
No static pressure change in the diaphragm or in the pressure flowing out of the calibrated leak
Therefore, the VSI will drop to a 0 indication and freeze there
Vacuum System
The aircraft's vacuum system is typically run via a vacuum pump connected to the aircraft's engine
The vacuum pump sucks air through the vacuum system to power the vacuum associated instrument gauges
Gyroscopic Instruments
Attitude Indicator
Heading Indictor
Turn Coordinator (electrically powered)
Rigidity in Space
A gyroscope (when spinning) tends to resist the motion of the aircraft in flight
It is able to maintain its position in space due to rotational velocity
This is because more "G-Forces" are pulling out on the gyroscope than are pulling down on the gyroscope
Precession
Because of the rotational velocity of the gyroscope, precession states that : The resulting force will take place 90 degrees ahead of the applied force in the direction of rotation
p100i Electrical System
Alternator/Generator - 28 Volts, 70 Amps Battery - 24 volts Master/Battery Switch Alternator/Generator Switch Bus Bars Fuses or Circuit Breakers Voltage Regulator - 28 Volts Ammeter or Loadmeter Associated Electrical Wiring
Parasite Drag
Drag not associated with the product of lift
Form Drag - engine cowling, antennas
Interference Drag - wing root meets fuselage
Skin-friction Drag - paint chips
Induced Drag
Bi product of Lift
4 Left Turning Tendancies
P-factor - Descending blade take a "bigger bite" of air creating more thrust than the ascending blade
Spiraling Slipstream
Gyroscopic precession - a force applied is felt 90 degrees in the direction of rotation
Torque - Newtons 3rd
Adverse Yaw
Turn left = right, vise versa, caused by drag created by the deflection of the ailerons
Category
Airplane Glider Rotorcraft
Class
SEL MEL SES MES
Type
a380 p28 b747
Engine Out
Airspeed - 76 Best place to land Checklist, fuel tanks, fuel pump on, full rich, alt air open, ELT on, cycle mags Declare emergency - squawk 7700
E Decend
power idle 30 degrees of bank away from fire lights off if needed pitch for top of green arc land asap
Engine Fire
fuel selector off fuel pump off mixture leaned e descent
Airspace (91.155)
Alpha Bravo Charlie Delta Echo Golf
Class Alpha
18000 to FL600 29.92 NO WEATHER MINIMUMS
Class Bravo
Blue solid lines "Big" INTL airports Entry req - Clearance, mode-C transponder and ADSB-Out, PPL or proper endorsements Weather minimums - 3 SM Vis and Clear of Clouds
Class Charlie
Magenta solid lines "Crowded" airports Lower shelf (core) 5 SM radius, up to 1200 AGL Upper shelf - 10 NM, up to 4000 AGL Entry Req - two way coms, mode-C transponder and ADSB-Out Weather minimums - 3-152
Class Delta
Dashed blue lines "Dialogue" Surface to 2500 AGL, 4 NM radius Entry Req - two way com Weather minimums - 3-152
Class Echo
Almost "everywhere" 3 different floors going to the underlying airspace 700 AGL 1200 AGL Weather minimums - below 10k MSL - 3-152 Above 10k - 5-111 SM
Class Golf
UNCONTROLLED airspace Any airspace thats not ABCDE Surface to overlying airspace
Day
10K MSL - 5-111 1200-10000 - 1-152 <1200 AGL - 3-152
Night
10K MSL - 5-111 1200-10000 - 3-152 <1200 AGL - 3-152
Special Use Airspace
Military Operating Area (MOA) Controlled Firing Area Prohibited Area - X Restricted Alert Area Warning Area National Security Area - X
Standard day
15 degrees C 29.92 In Hg
Standard Lapse Rate
2 degrees C per 1000' -1 In Hg
Coriolis Force
Air is deflected due to the rotation of the earth
Northern Hemisphere - 90 degrees to the right
Southern Hemisphere - 90 degrees to the left
The friction of the earth tends to slow the moving air and diver it from its original path
“H” - High pressure system
outward, downward, clockwise
anti-cyclonic
calm, clear, dry
“L” - Low pressure system
inward, upward, counterclockwise
cyclonic
cloudy, rainy, stormy
Convective Currents
Convection is vertically moving air
Wind is horizontally moving air
Turbulance
Uneven heating of the surface
Virga
Precipitation evaporates before hitting the ground
Wind Shear
Sudden change in the direction or velocity of wind
This can create updrafts, downdrafts, and change the horizontal movement
Low Level Wind Shear
Surface level wind shear
EXTREMELY DANGEROUS
Micro Burst
Convective activity
Indicated by rain or virga at the base of the cloud
Life span - 5-15 min
Down drafts up to -6k ft per min and headwind loses from 30-90 KTS
Dry Adiabatic Lapse Rate
3 degrees C per 1k ft
Temp Inversion
When climbing air gets warmer
Smooth stable air
Humidity
Amount of vapor present in the atmosphere
Relative Humidity
Actual amount of moisture in the air compared to the total amount of moisture the air could hold at that temperature
Cloud Formation
Adequate water vapor
Condensation Nuclei
A method by which air may be cooled
When air cools and reaches its saturation point, the invisible water vapor changes into its visible state
Low Clouds
Surface to 6500 AGL
Stratus
Nimbostratus
Stratocumulus
Middle Clouds
6500 to 20000 AGL
Alto
Altostratus
Altocumulus
High Clouds
>20k AGL
Cirrus
Cirrostratus
Cirrocumulus
Clouds with vertical development - Anvil Tops
Cumulus
Cumulonimbus
Fog
A cloud that is on or within 50 ft of the surface
Temperature near the ground is cooled to the airs dew point
Radiation Fog
Forms on clear nights with little to no wind
Ground cools rapidly due to the terrestrial radiation
Surrounding air temp reaches dew point
Low lying areas
Advection Fog
Forms when a layer of smooth warm air moves over a cold surface
Winds required - up to 15 KTS
Coastal areas
Upslope Fog
Forms when moist stable air is forced upsloping mountains
Requires wind to develop
Persists for days
Mountains
Steam Fog
Forms when cold dry air moves over warm water
As water Evaporates it rises
Over water during cold times of the year
Ice Fog
Forms in very cold weather
Must be -25 F or colder
Water vapor turns into ice crystals instantly
Arctic regions
Fronts
The boundary layer between two types of air masses
Warm Front
Warm mass of air advances and replaces a body of colder air
Slow moving (10-25 MPH)
High humidity
Good weather
Cold Front
Cold dense air replaces a body of warm air
Fast moving (25-30 MPH)
Bad weather
Stays close to the ground, acting like a snow plow
Stationary Front
When the forces of two air masses are equal
Mixture of warm and cold fronts
Can last for days, even weeks
Occluded Front
Occurs when a fast moving cold front catches up to a slow moving warm front
Very dangerous
Warm front weather prevails but immediately followed by cold front
Thunderstorms
Should be avoided by 20 NM, ideally 50-60 NM
Cumulus Stage
Lifting action begins
Strong updrafts
Present rain
Mature Stage
Most violent
Rain starts
Up and down drafts
Dissipating Stage
Down drafts
TS Ingrediants
Unstable air
Uplifting action
Visible moisture
Squall line
Narrow band of thunderstorms
Isobars
black lines
Lines of equal pressure
When close together = stronger winds
Trough
Orange/brown lines
Area of elongated low pressure
Ridge
Yellow lines
Area of elongated high pressure
Icing
Disturbs the smooth airflow over the wing, prop, and tail
Clear Ice
Most dangerous
Supercooled water droplets freeze slowly over a surface
Smooth and hard to see
Rime Ice
Supercooled water droplets freeze instantly
Rough texture and white
Ingredients of Icing
Surface of the airplane needs to be below freezing
Visible moisture
METAR
Aviation routine weather report
Observation of current weather
Reported in a standard format
Typically updated on an hourly basis
Can be updated more frequently (SPECI)
PIREPS
Actual Inflight conditions by other pilots, can confirm height of bases and top of clouds
Icing
UA - NON URGENT
UUA - URGENT
TAF
Terminal aerodrome forecast
Excepted weather for a 5 SM vicinity
Valid for 24 hrs, issued every 6 hrs
Airmets
Inflight weather advisories
Issued every 6 hrs as needed
Considered potentially hazard to light aircraft
Sierra
IFR conditions
Mountain obscuration
Tango
Light to moderate turbulance
Zulu
Light to moderate icing
Sigmets
Valid for 4 hrs
Extremely dangerous
Severe icing not associated with TS
Severe or extreme turbulence
Dust, sandstorms, or volcanic ash
Convective Sigmet
Valid for 2 hrs
Associated with TS
Issued for severe TS
Surface winds of >50 KTS
Hail ¾ in or >
Tornadoes
Micro bursts
Inversion
Climb-Level out-tumble backwards
Vestibular
Corriolis
Quick head movement
feels like you are spinning everywhere
Vestibular
Elevator
Up and down drafts
Somatosensory
False Horizon
Self explanatory
Leans
Turn
Fluid equalizes
New straight and level
Tighten bank
Opposite direction
Vestibular