Semminole

Question 1

structure type

Answer 1

semi-monocoque
semi-tapered

Question 2

what kind of flaps

Answer 2

slotted

Question 3

tail design

Answer 3

t tail
- hard to recover if stall

Question 4

rudder trim tab

Answer 4

anti servo tab

Question 5

engine

Answer 5

lycoming 4 cylinder direct drive horizontally opposed

Question 6

cowl flaps

Answer 6

located bottom of engine cowling
controls engine heating & cooling
- increases form drag

Question 7

prop feathering

Answer 7

turn 90 degree intowind for less drag

Question 8

props

Answer 8

can change AOA
feathering
counterrotating
- downward blade has most power

Question 9

Fuel quantities

Answer 9

55 x 2
110T
108 usable

Question 10

why oil change

Answer 10

visocitiy, temp, acidity changes oil

Question 11

battery

Answer 11

1 each engine
12V, 35A
14V system

Question 12

alternators

Answer 12

2 belt driven
14V, 70A, do not exceed 60A
6 electrical buses

Question 13

battery container vents

Answer 13

acid drain

Question 14

prop govenor

Answer 14

controls prop blade angle
situated on each engine to control propeller blade angle for constant RPM

Question 15

constant speed propeller

Answer 15

tach - prop rpm
mp - power

Question 16

landing gear

Answer 16

hydraulically actuated and fully retractable
3 gears

Question 17

safety squat switch

Answer 17

ground
- switch is open, preventing electrical current from reaching hydraulic pump
airbourne
- strut fully extended, closing switch allowing current to reachhydaulic pump

Question 18

Vs1
Vs0
VMCA
Vx
Vy
vyse

Answer 18

stalling speed clean 57
stalling speed landing 55
Vmca min control airspeed 56
vx 82
vy 88
vyse one eng inop aoc 88

Question 19

Vne
Vlo down
Vlo up
Va 3800
Va 2700

Answer 19

Vne 202
Vlo down 140
Vlo up 109
Va 3800 135
Va 2700112