Operation of Systems Flashcards
Describe Flight Controls (Primary and Secondary)
Primary:
Pitch: Stabilator - pulleys/cables to yoke.
Roll: Ailerons - pulleys/cables to yoke.
Yaw: Rudder - pulleys/cables to pedals.
Secondary:
Trim
Flaps
Power-plant
Lycoming IO-360-C
200hp @ 2700rpm
Fuel injected
Airframe
Aluminum Semi-monocoque
Stabilator
incorporates anti-servo tab
Ailerons & Rudder
Interconnected bus springs to help with adverse yaw
Flaps
Slotted.
Manual 4-position handle with push button on end to unlock:
F0 - 0°
F1 - 10°
F2 - 25°
F3 - 40°
Cowl flaps
Manual levers below throttle (don’t confuse with alternate air)
3-position:
- closed (up)
- intermediate
- open (down)
Alternate air
Manual 2-position levers immediately below pwr quadrant: closed (up) and open (down).
Air filter bypass
Heated by exhaust tube
Max CHT and Oil T
475°
245°
How to cool an overheated engine
v Pitch (reduce); ^ Airspeed (increase)
v Pwr (reduce)
^ Mix (enrich)
v open cowl flaps
Propellers
Counter rotating (left vs right engine)
Constant-speed / controllable pitch
Full feathering
How to Feather Propeller
Move Prop Control - FULL AFT
> 800 rpm
How is the propeller pitch controlled?
Controlled via the prop control lever adjusting the governor that control oil pressure to the prop hub.
High RPM / Low Pitch
- Oil pressure from governor (prop control)
- Aerodynamic force
Low RPM / High Pitch
- Counter weights
Anti-feathering lock
Centrifugal anti-feathering lock
- prevents feathering
impossible to feather < 800rpm
feather before 800rpm
Landing gear
- configuration
- retractable
- how is it held up/down
- actuation
Tricycle
Retractable - electric hydraulic pump
- Held up with hydraulic pressure
- naturally wants to come down due to gravity, aerodynamics, and spring assist
- held down with spring loaded hooks