Private Pilot Notes
Traffic pattern
Upwind to crosswind turn
if staying in pattern, 700ft agl (1700 msl)
if leaving the pattern 500agl (1500msl)
Downwind
Stay at pattern altitude (2000) and at 90kts along with 2300rpm
once parallel with landing point (numbers or 1000ft markers), begin configuring
Should remain 1 mile parallel from runway
The wingtip should be just touching the runway (though, better closer than farther)
Downwind to base turn
configure
is setting rpm to 1600-1700rpm
Flaps 10 (first click)
80 knots
At this point, hold pitch and let it naturally descend to 800ft agl (1800ft msl)
Make the turn when wing hits at a 45 degree angle with the runway (practice in msfs)
Base
should have naturally decelerated to 800ft agl at this point, at 70 knots
Final
A whole lot more than I can put here
Power idle when runway is made
Standard temperature is 15º C/ 59º F
Standard Pressure is 29.92 inHg / 1013 mb
The Aircraft
PA-28-161
N84400
N25510
V speeds
Vr - 60
Vy - 79 - rate
Vx - 63 -angle
Va -89 to 111
Vne - 160
Vno - 126
Vg - 73
Vfe - 103
Vs - 44
Vso - 50
Engine
Lycoming 0320
0 - carburetor (float type)
320 - size of the engine (cubic inches)
Lycoming 0320
Horizontally opposed cylinders
Air cooled
Naturally aspirated
Direct drive
fixed pitch and prop is directly connected to crankshaft
2 mags
Mags generate electricity for the spark plugs (there are two for redundancy)
8 sparkplugs
2 per each cylinder
Necessary instruments
Altimeter
Tachometer
Oil pressure gauge
Manifold pressure gauge (if applicable)
Airspeed indicator
Temperature gauge (for liquid cooled, or oil temperature for air cooled engine)
Oil temperature gauge
Fuel level gauge
Landing gear position indicator (for retractable gear aircraft)
Anticollision lights (for aircraft certified after March 11, 1996)
Magnetic compass
ELT (Emergency Locator Transmitter)
Safety belts/shoulder harnesses
(only applicable at night)
Fuses
Landing lights
Anti-collision lights
Position lights
Source of electricity
Fuel system
Fuel Tanks: Each tank holds 24 usable gallons.
Fuel Selector: Fuel from each tank flows to the fuel selector.
Strainer: From the selector, fuel goes to a strainer.
Fork in the System: After the strainer, the fuel path divides:
Priming Path: Fuel proceeds to the primer, which delivers fuel to cylinders 3 cylinders (which ones, who knows?)
Main Engine Fuel Path:
Electric fuel pump.
Engine-driven fuel pump.
Fuel pressure gauge.
Carburetor (float type).
Required maintenance
Annual
12 calendar months
VOR check
30 days
100 hours
commercial aircraft
Altimeter and static port
24 calendar months
Transponder
24 calendar months
ELT
TO REPLACE
1 hour of use / use half of battery
TO CHECK
12 calendar month
Necessary documents (plane)
Airworthiness certificate
indefinite if compliant
Registration
7 years
Radio operating license
only necessary if flying internationally
Operating handbook (pilot operating handbook)
Weight and balance (calculations)
Technical information of plane
76 inch Sensenich propellor
Fixed pitch (highest pitch is at hub of prop, lowest at tip)
Fixed tricycle landing gear
Brakes are on main gear
hydraulically actuated disk brakes
Minimum 6 quarts of oil
cleans
seals cylinder wall & pistons
cools
lubricates
OLEO struts
filled with hydraulic fluid and nitrogen
12V battery with a 14 volt system
if voltage is abnormally above, something is wrong with the reader
60 Amps
0-60 normally
Avionics
G5 - EFD
G430 - nav and transponder
Ram air at tip of pitot tube
aneroid wafer expands and contracts based on air pressure, to show altitude on the altimeter
Kollsman window is where the pressure is seen
Pilot Information
Necessary documents
Govt issued photo ID
Pilots license
Medical
logbook (if student pilot is soloing)
Safety Checklist
Illness
Medications
Stress
Alcohol
below .04
Fatigue
Eating/drinking
General checklist for safe flight
Pilot
Airplane
EnVironment
External factors (Weather, TFR, etc.)
Concepts
Adverse Yaw
Per say in a left turn, the left aileron raises reducing its lift and drag. The right aileron raises and gains lift. Because its gaining lift, it must therefore gain more drag.
Relative wind is the direction of wind relative to aircrafts flight path
AoA is the difference between chord line and relative wind
Angle of Incidence is the angle between the chord line and longitude axis
The idea of excess thrust allows for continuous motion @ the same airspeed (NOT inertia
Gyroscopic instruments
Heading indicator
rigidity in space
Attitude indicator
rigidity in space
turn coordinator
precession
Pitot-static instruments
Airspeed indicator
Altimeter
Vertical Speed Indicator
delay of 6-9 seconds
Region of reverse command
casued by a dramatic increase in Induced drag
in high draghigh lift environments (slow flight, landing), the flight controls reverse:
pitch for airspeed
power for altitude
Left turning tendencies
Spiraling Slipstream
The air displacement caused by the propellor rotating spins around the plane and hits it on the left side
Gyroscopic precession
In the air, the planes engine acts as a gyroscope, and therefore has all the gyroscopic properties: rigidity and in space and precession. Therefore when the force is applied, aka the elevator, it takes a full 90º for said force to be felt, which causes the aircraft to want to turn left
P-factor
In high angle of attack situations, the right side of the blade (or the falling side) takes more air than the ascending side. t
Torque effect
Types of drag
Parasitic
caused by any object moving through air
Form drag - based on the shape of the aircraft
Interference drag - any point of opposing airflow (corners, wings, etc.)
Skin friction - friction caused by friction between air and the planes surface
Induced
A byproduct of the creation of lift (wingtip vorticies)
Slow
Clean
Drag
Maneuvers
Clearing turns
Reference
Airspeed/altitude
Configuration
Steep turns
put plane in 45º bank angle and make full 360º turn to original reference heading (without loosing altitude)
add power because your’e losing vertical lift
watch out for climbing
Power on stalls
takeoff configuration
fuel pump on / mixture rich / landing light on
aim for 79 then pitch up until you stall
S-turns
pick a line ground reference point
fly over the line and when its in your 45º rear, make a standard rate turn, and when the turn rounds out, one should be back over the line - repeat
straight and level
fly without gaining any airspeed or altitude
slow flight
put full flaps in, slow to 55, and attempt to hold altitude and airspeed
for climbs, full power will often be necessary
for descents, be weary of overshooting altitude
turns around a point
pick a point and attempt to make a perfect circle 360º turn around said point
The Airport
KPDK
21R is right traffic, 21L is left traffic
3L is left traffic,
3R is right traffic
Solo
3 full stop taxi backs at PDK
Add student solo at the end of first call
Peachtree ground warrior 84400 at clairimont with E requesting pattern work with full stop taxibacks student solo
If I get lost, request progressive taxi
Maneuvers and checkride notes
CRAAAAAAAAAAAC
There is no time limit for checkrides, so bug EVERYTHING (altitude and airspeed). CRAC before all maneuvers
mentally remind whenever approachign taxiway/runway do clear left, clea center, and clear right. also, remind oneself that we’re clear to cross a runway if assigned
study cloud types
Startup
lean out mixture until engine slows, then add a little bit, setting a new equillibrium
Passenger Breifing
Follow SAFETY and DEMONSTRATE each item in the checklist
Seatbelts: unbuckle and buckle must be on during takeoff, taxi, and landing.
Air vents: open and close and show direction of movements
Fire extinguisher/flight controls: point to it and say if they get to it first thats fine. Explain a positive three way exchange of controls.
Emergency: explain emergency procedures and that we have 1 door. Physically show how to open the door (2 latches)
Talking/Traffic: Explain to limit talking during critical stages of flight (Taxi, takeoff, landing). Explain what sterile cockpit is and that its basically an aviation euphemism of shut up. Explain if you see anything outside (planes, birds, etc.) let me know because 4 eyes are better than two.
Y: Questions?
Taxi to run up
perform brake check immediately
call out anticipated taxi breifing, mention hot spots
mention obstructions and potential engine failures. predict how the plane might climb based on density altitude.
remember crosswind taxi correction
Run up
Go through full checklist, bug runway heading, yadayada.
Takeoff brief
explain runway lengths, emergency procedures, yadayada
Takeoff and climb
Dont drift, and assign a point on the horizon to use as extended centerline
Climb checklist when load dies down
Simulated IFR
Declare an emergency and broadcast mayday mayaday mayday on 121.5
Make an immediate 180 turn
VOR tuning
VOR radials are coming FROM the vor. So if asked to fly the 300º radial, one would tune to the 300 degree mark then fly until you intercept it
Make sure nav 1 is on during testing
Unusual attitude
Blue power through (when pitched up, wings level and push nose down as applying power)
Brown power down (when pitched down, wings level, then pull power and lift nose up)
CRAAAAAAAAAAAC
Slow flight
Landing configuration (full flaps, mixture rich, landing light/fuel pump on)
Speed you tell the dpe is 50 but youre actually flying 55. This gives ±5 buffer. do NOT fly over 60
be precise on entry with alt/heading/spd
Power off stalls
Simulating a landing when someone flares too much too high
landing configuration (full flaps, mixture rich, landing light/fuel pump on)
Pull power for 66 knots and get in a stabilized descent of -500fpm
pull power to idle, and slowly pull up into first indication of a stall. Hold it level and bleed off the airspeed
Aim not to descent (so dont crash into ground)
dont dump last 2 notches of flight until positive rate is established
Power on stall
over rotation on takeoff
Clean configuration (no flaps, mixture rich, fuel pump on, landing light on)
push down and build airspeed
biggest concern for power on stall is a spin because of left turning tendencies
keep nose at 20º
Steep turn
cruise configuration
hold 45 degrees of bank
95 knots
Maintain the entry altitude ±100 feet, airspeed ±10 knots, bank ±5°, and roll out on the entry heading ±10°.
dont overcontroll, keep it at 45 and let the power setting (2300) and pitch (5º) do the rest
Simulated engine failure
Airspeed - 73
Best place to land - likely a field
Checklist - emergency landing checklist
Declare emergency - 121.5 mayday mayday mayday
ELT
Emergency descent
pitch for 125 and maintain 35 degrees in the turn
throttle idle, mixture cut, fuel valve off
checklist
Diversions
Short field landing
full flaps and approach speed of 72 kias
If anything go LONG
As soon as touchdown, youre adding max breaks, and do max aerodynamic breaking
flaps are secondary to aerobreaking and breaks
Short field takeoff
hold max breaks and max power on centerline at start of runway count to 3
roatate at 55, climb at 63, clear 50ft obstacle, then climb out at 79
2 notches of flaps
Soft field landings
come in on mains softly, then hold the nose up for as long as possible at that attitude
come in a little faster - 72ish knots. Flare at 66
When holding flare, should be idle
Soft field takeoff
keep rolling with minimum breaking, and full power onto runway. then stay in ground effect until 63. climb to 63, clear obstacle, then climb to 79
add max back pressure, then RELEASE SLOWLY, lifting off at around 55ish then staying in ground effect until 63, climbing out at 63, clearing obstacle, then climbing out at 79
2 notches of flaps
Go Around
full power, flaps retracted, radio going around
S turns
enter on downwind leg with a tail wind
Clean configuration (no flaps, mixture rich, fuel pump on, landing light on)
right after crossing the road, start turn
Turns around a point
enter on downwind leg, ideally with a tailwind
Clean configuration (no flaps, mixture rich, fuel pump on, landing light on)
maintain uhhh good distance yk
slips
slip into the wind
full flaps
Oral Notes
acronyms
Pilot
IMSAFE
SAFETY
AIIMR
HASH
Aircraft
AVIATE
ARROW
ATOMATOFLAMES FLAPS
UNOS/ANDS
LHAND
EnVironment
NWKRAFT
PARE
TTMPRAWNS
External factors
PPPPP
Engine
Lycoming
Horizontally opposed
Air cooled
Naturally aspirated
Direct drive
Altimiter
Tachometer
Oil pressure gauge
Manifold pressure gauge
Airspeed indicator
Temperature gauge (liquid cooled engines)
Oil temperature gauge
Fuel gauge
Landing light
Anti collision lights
Magnetic compass
ELT (replace after 1 hour of cumulative use or 50% battery | check every 12 cal months)
Seatbelts (required during critical stages of flight)
Fuses
Landing light
Anti collision light
Position lights
Source of electricity
Pilot
Plane
Plan
Programming
Passengers
Hypoxic hypoxia - lungs
Anemic hypoxia - blood loses ability to carry o2 to brain (CO2 poisoning)
Stagnant hypoxia - high Gs
Histotoxic hypoxia - drugs/alc
Anti authority
Impulsivity
Invulnerability
Mmacho
Resignation
Seat belts
Air vents
Fire extinguisher
Emergency exits
Talking/traffic
Y - questions?
TFR - no
TRSA - legacy airspace that usually surrounds class D and grants greater assists without the strict, mandatory participation rules of Class C
MOA - you can fly through without permission, but probably not a good idea. call first
Controlled firing - good to fly through
Prohibited - no flying
Restricted - ask permission to fly in
Alert - high volume of traffic
Warning - can fly through but strongly discouraged
National security - no
SFRA - only with permission, depends on the airspace
Illness
Medication
Stress
Alcohol
Fatigue
Eating
Airspeed
Best place to land
Checklist
Declare emergency on 121.5 and squack 7700
ELT
Undershoot
North
Overshoot
South
Accelerate
North
Decelerate
South
Airworthiness - doesnt expire
Registration - every 7 years
Radio operating license - if flying intl.
Operating handbook
Weight and Balance
Power Idle
Ailerons neutral
Rudder opposite
Elevator foward
Annual - 12 cal months
VOR - IFR only - 30 days
100 hour - every 100 hours for commercial aircraft
Airworthiness Directives - active compliance
Transponder - 24 cal months
ELT - 12 cal months to check, 50% battery or 1 hour of cumul. use to replace
Static system and altimeter - 24 cal months and ifr only
Notams
Weather
Known ATC delays
Runway lengths
Alternates
Fuel
TO/LD distances
General notes to remember
16 volt alternator, 14 volt battery - constant charge
Wind flows paralell to isobars and is caused by the uneven heating of the earths surface
TAFs and METARs are a 5nm radius
Pilotage is using visual landmarks, and Ded reckoning is time + GS
Clear ice is most dangerous bc is most dense/heavy and hardest to see
Chart Supplements update every 50 days
Warm front/high pressure associated with steady continuous precipitation
Spacial disorientation
visual - eyes
vestibular - ear pressure
somatosensory - G forces
water is 8.34 pounds, oil is 7.5 pounds, fuel is 6 pounds
2 electrical buses on the aircraft
a bus is a central conductor where electricity is stored and distributed
Avionics and Main bus (Batt/starter)
plane uses anti servo trim
slotted, manual flaps
voltage regulator controls how much energy goes to the battery from the alternator (to deal with the asymmetry of power produced by the engine vs what the battery needs
30 days to notify the FAA after moving
magnetos go to the leads (wires) then go to the sparkplugs
primer injects fuel into the intake ports
Pressure altitude is Field elevation + (29.92-CA) x 1000
Density altitude is PA + [120 x (OAT-ST)]
types of airspeed
IAS - indicated airspeed, noncorrected
CAS - calibrated airspeed for instrument and position error
TAS - calibrated airspeed adjusted for temperature and pressure
GS - TAS corrected for wind
types of altitude
Indicated altitude - what we see
pressure altitude - corrected for nonstandard pressure, middleman to density alt.
density altitude - corrected for nonstandard temp and pressure (what the airplane feels)
true altitude (MSL) - physical height above sea level
absolute altitude (AGL) - height above ground
Left turning tendencies
P-factor - descening blade catches more air than ascending blade in high AoA scenarios, creating asymetrical thrust, turning the aircraft left
spiraling slipstream - air wraps around the plane and hits the left side of the vertical stabilizer, yawing the plane left
torque effect - prop tuens clockwise, so plane wants to turn ccw (left)
gyroscopic precession - the plane functions as a gyro, and precession states that a force is felt 90º late on said gyro, this (minorly) causes the plane to go left
Stability
static - at a moment
positive - wants to return to orignial position
neutral- wants to stay in altered position
negative - wants to continue deviating
dynamic - over time
positive - wants to return to orignial position
neutral- wants to stay in altered position
negative - wants to continue deviating
Drag
parasitic
form drag - The shape of the plane moving through the air and the friction is causes (wood block vs bullet)
skin friction - the microscopic impact of the wind against the surface of the object, and the drag it creates (walking area of wing vs smooth)
interference - the intersection of parts of the plane (wing with fuselage)
Induced
A byproduct of the creation of lift (wingtip vortices and such)
As airspeed increases, induced drag decreases and parasitic drag increases
L/D Max is Vglide and where the curve of induced and parasitic drag intersects
Slower than LD max is the region of reversed command.
Instruments
pitot static
Airspeed indicator
Altimiter
VSI
gyroscopic
HSI
turn coordinator
heading indicator
CG effects on performance
Forward CG (weigh concentrated towards center of lift)
highly stable
less efficient - lower cruise speed
higher stall speed, but easier to recover
heavy controls
Aft CG
less stable - very sensitive
lower stall speed, but harder to recover
more efficient and faster at cruise because of decreased induced drag (because the plane is more “balanced,” less lift is needed for level flight)
Magnetic Deviation vs Variation
Variation
Difference between the north and magnetic north
East is least, west is best (subtract east add west)
Deviation
difference between magnetic north and compass needle; caused by electrical systems and is unique to individual aircraft
Magnetic dip
ANDS: on east/west heddings, accelerating turns the compass north, and when decelerating, the compass skews south
UNOS: when turning from north headings, the compass needle will lag, as when turning from south, the compass overshoots
Atmosphere is coposed of 78% nitrogen, 21% oxygen, and 1 percent other gases
wind is caused by the uneven heating of earths surface
The three classiifications are cirrus, alto, and stratus. High to low
Turbulance is the irregular, chaotic, motion of air
light - slight altitude loss
moderate - moderate altitude loss
Severe - momentus loss of control
extreme - structural damage
Unstable atmosphere facilitates vertical motion
fly 20nm away from thunderstorms (at least). If need to fly near fly upwind
Frost forms on wings overnight due to deposition
water vapor turns into ice with full saturation
If encounter icing, decend, turn on carb hear, pitot heat, and advise ATC
Load limits
3.8g and -1.52g
emergency airworthiness directives
immediate action/short time period
AHRS(altitude heading reference system)
provides info to gyroscopic instruments
Vacuum system provides information to gyroscopic information
engine driven pump creates suction and spins rotors
Magnetic oscillation is the combination of deviation and variation
Isogonic lines are the lines of magnetic variation
Oil cleans, cools, seals, and lubricates
Sparkplug fouling is caused by carbon buildup
OLEO struts are oil and (nitrogen)
PGA is the radius of skydivers
The fuses in the PA28161 are the circuit breakers
dont need permission for MoA
low pressure is up, ccw and inward
high pressure is down, cw, and outward
Vglide changes slightly with weight
a ceiling is a large layer of broken or overcast clouds
convective activity is the transfer or energy
from warm to cool and cool to warm
an occluded front is colder air catching up to warmer air
Cyanosis is a symptom of hypoxia
dead reckoning is calculating a current position by advancing a known past position with groundspeed, time, and heading.
5 Cs of being lost
climb
confess
communicate
comply
conserve
GPU is mounted on right side of pa28161
Carb ice generally occurs below 70º F and above 80% humidity
can go as high as 100º F and as low as 50% humidity
FACEPIP
Flight review
flight review/checkride in past 24 cal months
Aircraft docs
ARROW
Currency
3 TO/LD past 90 days (full stop for night) — carrying passengers
E
equipment. 91.213 to KOEL to 91.205 to AD then placard inop and deactivate if possible. ONLY A&P CAN REMOVE
Performance and weather
weight and balance, performance calculations for runway, weather minimums
inspections
Annual (12cal), 100 hr (hire) ELT within 12 cal months (replace if at 50% or used for 1 cumul hour), transponder within 24 cal months, pitot static within 24 cal months for ifr
Pilot
certificates, medical, logbook, photo id,
Airspace
Class B
Solid blue
ADSB, mode C transponder, Two way radio, direct clearance to enter
busiest airports
Class C
Solid magenta
ADSB, mode C transponder, two way radio
Inner ring is 5nm radius with SFC to 1200, outer ring 10nm and 1200 to 4000 (AGL everything)
Class D
Dotted blue
Two way radio
4nm radius, surfact to 2500 agl (depicted in MSL, ex. PDK at [35]
Class E
for ifr traffic, as class E is techincally controlled airspace
no equipment requirements
3152 below 10000
5111 above 10000
normally starts at 1200
dashed magenta means class E begins at surface
magenta vignette class E begins at 700 agl
blue vignette class E begins at 1200
class E teeeechnically starts at 14500, but that blue vignette covers most of the US, so the places to note are the areas where the vignette faces OUT, indicating that the airspace inside the box is actually class G to 14500msl
Class G
uncontrolled airspace
1sm visibility and clear of clouds day vfr
3152 night vfr
normally goes up to 1200
when above 1200 (irregular situation), weather minimums are 1sm of visibility and 152