Specifications Flashcards
1
Q
Engine
A
200HP - 2700 rpm
Teledyne Continental IO-360-ES
Fuel injected-Air cooled
Horizontally opposed 6 cylinder
2
Q
Propeller
A
Hartzell two blade 76”
Constant speed
3
Q
Fuel
A
60.5
56 gal usable
100LL
4
Q
Oil
A
8 Quarts
SAE 15W-50 or 20W-50
5
Q
Weights
A
3000 max Takeoff
2900 max Landing
2160 Empty
504 useful load at full fuel
6
Q
Max Baggage Weight
A
130lbs
7
Q
Max Oil Temp & Pressure
A
240 degrees F
100 PSI
8
Q
Takeoff runway length
A
2500ish ft
(To clear a 50’ obstacle)
Refer to poh
