Section 1 - General Flashcards
1
Q
Elevator span
A
11’4”
2
Q
Wing span
A
36’1”
3
Q
Propeller diameter
A
75 inches max
4
Q
Aircraft length
A
27’2”
5
Q
Aircraft height
A
8’11’’
6
Q
Wheel base
A
65”
7
Q
Propeller ground clearance
A
11.25 inch
8
Q
Wing area
A
174 sq. Ft.
9
Q
Minimum turning radius
A
27’5.5”
10
Q
Engine description
A
Single engine by textron lycoming
IO-360-L2A
160 BHP at 2400 RPM
11
Q
Propeller description
A
Manufactured by McCauley propeller systems
1c235/LFA7570 2 blades fined pitch max diameter 15”
12
Q
Fuel grade
A
Avgas 100
Avgas 100LL
13
Q
Additives in fuel
A
Isopropyl alcohol 1%
Diegme 0.10% to 0.15 %
14
Q
Fuel capacity
A
56 USG total 53USG usable
15
Q
Oil used
A
Mil-l-6082 mil-l - 22851
