Systems Flashcards
Type of fuselage
Semi-monocoque structure
Type of wing
NACA 652-415
How are the wings attached
The insertion of the butt ends of the spar in to a spar box carry-through.
Continuos main spar
Purpose of the Anti-Servo Tab
Improves longitudinal stability and provides longitudinal trim
Direction the Anti-Servo Tab moves
Same direction as the stabilator but with increased travel
Engine Type
IO-360-C1C6
Direct drive
Horizontally opposed
Fuel injected
Engine horsepower
200 Hp @ 2700 RPM
Rated output of the Alternator
60 amp
14 volts
Engine furnishings
Starter Alternator Ignition Vacuum pump drive Fuel pump Propeller governor Dry automotive type induction air filter
Type of propeller
Constant speed controllable pitch
How are cabin heat and windshield defrosting accomplished?
A heater shroud around the muffler
Oil cooler and air inlet location
Oil cooler- Forward lower right side of the firewall
Air inlet- Right side of the bottom cowling
Principle behind the fuel injector
Differential pressure which balances air pressure against fuel pressure
What is the airframe made of
Aluminum Alloy
Annunciator panel
Alternator
Low oil pressure
Low Vaccum
How are the Landing Gear actuated?
Hydraulically actuated by an electrically powered reversible pump
How long does it take to cycle the landing gear?
7 seconds
Manual gear extension process
Emergency gear lever held down
Releases the hydraulic pressure
Gear free falls
How does the nose gear extend during a manual gear extension?
Free falls
Spring assisted
Gear warning horn conditions
Gear up Power less than 14”
Gear up WOW throttle retracted
Gear up Flaps beyond 10*
Main gear strut extension
2.75” +/-.25
Nose gear strut extension
2.5” +/-.25
Difference between gear horn and stall horn
Gear horn- 90 hertz beeping sound
Stall- continuous tone
Nose gear turning radius
30*
