Section 1 - General Flashcards
Elevator span
11’4”
Wing span
36’1”
Propeller diameter
75 inches max
Aircraft length
27’2”
Aircraft height
8’11’’
Wheel base
65”
Propeller ground clearance
11.25 inch
Wing area
174 sq. Ft.
Minimum turning radius
27’5.5”
Engine description
Single engine by textron lycoming
IO-360-L2A
160 BHP at 2400 RPM
Propeller description
Manufactured by McCauley propeller systems
1c235/LFA7570 2 blades fined pitch max diameter 15”
Fuel grade
Avgas 100
Avgas 100LL
Additives in fuel
Isopropyl alcohol 1%
Diegme 0.10% to 0.15 %
Fuel capacity
56 USG total 53USG usable
Oil used
Mil-l-6082 mil-l - 22851
Oil capacity
8 qts sump
9 QTs total
Ramp weight normal category
2457 lbs
Ramp wt utility category
2107 lbs
T/0 wt normal category
2450 lbs
T/0 wt utility category
2100 lbs
Standard empty weight
1639 lbs
Max useful load (normal)
818 lbs
Max useful load (utility)
468 lbs
Wing loading
14.1 lbs/sq ft
Power loading
15.3 lbs/hp