213AF

AIRCRAFT	213AF
Year	1975
Model	150M
Engine Horsepower	100hp
Va-Max Wt	97 kts
Vx-Sea Level	56 kts
Vy-Sea Level	68 kts
Cruise Climb	65-75 kts
Land - 0 Flaps	60-70 kts
Land - Full Flaps	50-60 kts
Vlo/le	- -
Vs	47 kts
Vso	42 kts
Vfe	85 kts
Vno	107 kts
Vne	141 kts
Maximum Glide	60 kts
Max T/O Weight	1600 lbs
Empty Weight	1163 lbs
Useful T/O Load	437 lbs
(Note: Full oil is included in all aircraft empty weights)
Oil Capacities
Max	6 qts
Min	4 qts
Usable Fuel	22.5 gal
Rudder Trim	No
Avionics Cooling	No
POH Required	No
STC Required	No
Red Electrical	Over Voltage
Malfunction Light	Alternator
Indicates	Faulty