1st progress check ground

Question 1

main parts

Answer 1

fuselage, wings, power plant, tail assembly, landing gear

Question 2

flight controls/surfaces

Answer 2

primary: ailerons, elevator, rudder. secondary: flaps, trim.

Question 3

6 pack

Answer 3

attitude indecator, heading indecator, turning coordinator,airspeed indicator, altimeter, vertical speed indicator.

Question 4

engine gauges

Answer 4

tachometer, ammeter, volts meter, vacuum gauge, fuel flow, oil pressure gauge, oil tempeture gauge, fuel quantity

Question 5

scan

Answer 5

regularly scanning your surroundings and interments checking for traffic and any abnormal indications.

Question 6

ARROW

Answer 6

A-airworthyness certificate, R- registration certificate, R-radio operations, O- operation limitations, W-weight and balance.

Question 7

AAVIATE

Answer 7

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.

Question 8

91.205

Answer 8

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

Question 9

4 forces

Answer 9

thrust, drag, weight, lift.

Question 10

3 axes

Answer 10

vertical/yaw axes, lateral, longitudinal.

Question 11

when do you use rudder

Answer 11

using rudder allows you to centralize and coordinate the forces affecting you in turns

Question 12

when do you use flaps

Answer 12

using flaps allows for a steeper decent angle at the same speed

Question 13

AOA

Answer 13

(angle of attack), the angle at which the chord of your wing meets relative wind.

Question 14

SRM

Answer 14

(single pilot resource management), situational awareness, risk management

effective use of all available resources 

Question 15

situational awareness

Answer 15

Monitoring all available sources of information about the aircraft and aircraft around you.

Question 16

risk management

Answer 16

And minimizing the risks presented to you both on the ground and in the flight.

Question 17

PAVE

Answer 17

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

Question 18

aeronautical decision making

Answer 18

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

Question 19

what class airport are we

Answer 19

we are a class E airport but below 700ft AGL we are class G

Question 19

controlled flight into terrain

Answer 19

unintentional collision with terrain

Question 20

cloud clearances

Answer 20

152: 3 SM visibility, 1000 above, 2000 around, 500 below

Question 21

the left turning tendencies

Answer 21

p-factor, spiraling slip stream, torque, gyroscopic precession.

Question 22

gyroscopic precession

Answer 22

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.

Question 23

p-factor

Answer 23

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.

Question 24

spiraling sliptream

Answer 24

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.

Question 25

torque

Answer 25

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

Question 26

PARE

Answer 26

P-power idle
A-ailerons neutral
R-rudder in the opposite direction
E-elevator briskly through neutral