Semminole Flashcards
structure type
semi-monocoque
semi-tapered
what kind of flaps
slotted
tail design
t tail
- hard to recover if stall
rudder trim tab
anti servo tab
engine
lycoming 4 cylinder direct drive horizontally opposed
cowl flaps
located bottom of engine cowling
controls engine heating & cooling
- increases form drag
prop feathering
turn 90 degree intowind for less drag
props
can change AOA
feathering
counterrotating
- downward blade has most power
Fuel quantities
55 x 2
110T
108 usable
why oil change
visocitiy, temp, acidity changes oil
battery
1 each engine
12V, 35A
14V system
alternators
2 belt driven
14V, 70A, do not exceed 60A
6 electrical buses
battery container vents
acid drain
prop govenor
controls prop blade angle
situated on each engine to control propeller blade angle for constant RPM
constant speed propeller
tach - prop rpm
mp - power
landing gear
hydraulically actuated and fully retractable
3 gears
safety squat switch
ground
- switch is open, preventing electrical current from reaching hydraulic pump
airbourne
- strut fully extended, closing switch allowing current to reachhydaulic pump
Vs1
Vs0
VMCA
Vx
Vy
vyse
stalling speed clean 57
stalling speed landing 55
Vmca min control airspeed 56
vx 82
vy 88
vyse one eng inop aoc 88
Vne
Vlo down
Vlo up
Va 3800
Va 2700
Vne 202
Vlo down 140
Vlo up 109
Va 3800 135
Va 2700112
