Oral P.O.H Sect. 1 Flashcards
What kind of Engine do we have?
Textron Lycoming (manufacture)
IO-360-L2A
Fuel Injection
Horizontally Opposed
360 cubic inch of displacement
Accessory Package
What is our Maximum RPM and Horsepower?
180 BHP @2700 RPM
What is the diameter of our propeller?
76 in
What are the three Axis’ that we fly?
Vertical: Pitch
Longitudinal: Roll
Lateral: Yaw
What Flight Controls Affect the Axis’s?
Vertical: Pitch (Elevator)
Longitudinal: Roll (Aileron)
Lateral: Yaw (Rudder)
What is the diameter of the propeller?
76in, minimum 75in
Propeller Type?
Fixed Pitch, the propeller cannot be rotated around their axis
Approved Fuel Grades?
100 LL Grade Aviation Fuel (Low Lead) (Blue)
100 Grade Aviation Fuel (Green)
Fuel Capacity?
Total Capacity: 56
Total Useable: 53
Why can we not use all of the fuel?
There is a lip inside of the fuel tank that sits above the bottom of the tank.
This is so contaminants sink to the bottom and do not get into the fuel system.
What is our Oil Capacity?
Sump: 8 U.S. Quarts
Total: 9 U.S. Quarts
What is our maximum ramp weight?
Why?
Normal: 2558
Utility: 2208
We burn 8lbs of gas while we taxi.
What is the maximum take off and landing weight?
Takeoff and Landing:
Normal: 2550 lbs
Utility: 2200 lbs
Where is Baggage A and Baggage B located?
In the tail storage, A is the main area, B is located behind it and is much smaller.