1st progress check ground Flashcards
main parts
fuselage, wings, power plant, tail assembly, landing gear
flight controls/surfaces
primary: ailerons, elevator, rudder. secondary: flaps, trim.
6 pack
attitude indecator, heading indecator, turning coordinator,airspeed indicator, altimeter, vertical speed indicator.
engine gauges
tachometer, ammeter, volts meter, vacuum gauge, fuel flow, oil pressure gauge, oil tempeture gauge, fuel quantity
scan
regularly scanning your surroundings and interments checking for traffic and any abnormal indications.
ARROW
A-airworthyness certificate, R- registration certificate, R-radio operations, O- operation limitations, W-weight and balance.
AAVIATE
A- airworthiness directives, A- annual/ every 12 calendar months, V-VOR/ every 30 days, 1- done every 100 hours (based off the tach time), A- altimeter pitot static system/ done every 24 calendar months, T-transponder/done every 24 calendar months, E- ELT/ done every 12 calendar or whe 50% of batterie life has expired or 1hr of use.
91.205
ATOMATOFLAMES.
A- airspeed indecator
T-tachometer per engine
O-oil pressure gauge
M-manifold pressure gauge
A-altimeter
T-temp gauge for liquid cooled engine
O-oil temp gauge for air cooled engine
F- fuel gauge
L-landing gear position lights
A-anti collision lights
M-magnetic direction indicator
E-ELT (emergency location transponder)
S-safty belts
4 forces
thrust, drag, weight, lift.
3 axes
vertical/yaw axes, lateral, longitudinal.
when do you use rudder
using rudder allows you to centralize and coordinate the forces affecting you in turns
when do you use flaps
using flaps allows for a steeper decent angle at the same speed
AOA
(angle of attack), the angle at which the chord of your wing meets relative wind.
SRM
(single pilot resource management), situational awareness, risk management
effective use of all available resources 
situational awareness
Monitoring all available sources of information about the aircraft and aircraft around you.
risk management
And minimizing the risks presented to you both on the ground and in the flight.
PAVE
P-pilot :IMSAFE
A-aircraft :ARROW,AAVIATE
V- enverment: NWKRAFT
N-notice to airmen
W-weather
K-know ATC delays
R- runway lengths
A-alternantes available
F-fuel requirements
T-takeoff and landing destinies
E-external pressures: Everything else
aeronautical decision making
decide model, the 3 p’s:
It is the process of making decisions in flight to reduce the risks of anything or eliminate a hazard
what class airport are we
we are a class E airport but below 700ft AGL we are class G
controlled flight into terrain
unintentional collision with terrain
cloud clearances
152: 3 SM visibility, 1000 above, 2000 around, 500 below
the left turning tendencies
p-factor, spiraling slip stream, torque, gyroscopic precession.
gyroscopic precession
an inherent quality of rotating Bodies, which causes an applied force to be manifested 90 degrees in the direction of the rotation from the point where the force was applied.
p-factor
a tendency for an aircraft to yaw to the left due to the descending propeller blade on the right producing more thrust than the ascending blade on the left. this occurs when the aircrafts longitudinal axis is inn a climbing attitude in relation to the relative wind. the p-factor would be to the right if the aircraft had a counterclockwise rotating propeller.
spiraling sliptream
the slipstream of the propeller-driven airplanes rotates around the airplane . this slipstream stricks the left side of the vertical fin causing the airplane to yaw to the left.
torque
a. resistance to Turning or twisting or rotating motion in an airplane the tendency of the aircraft to turn(roll) in try opposite direction of rotation of the engine and props.newtons 3rd law of motion
PARE
P-power idle
A-ailerons neutral
R-rudder in the opposite direction
E-elevator briskly through neutral
