|
AirFrame
|
|
|
Fusulage Construction
|
Semimonocoque |
|
Airframe Material
|
All-Metal |
|
Number of Doors
|
2 |
|
Wing
|
|
|
Wing Location
|
Bottom Wing |
|
Wing Construction
|
Full Cantilever |
|
Wing Rib Material
|
Sheet Metal |
|
Wing Skin Material
|
Aluminum |
|
--Aileron
|
|
Aileron Type
|
Differential |
Aileron Trim
|
Manual |
Aileron Control System
|
Pully and Cable |
--Flap
|
|
Flap Type
|
Plain |
|
Wing Flap Actuation
|
Manual |
|
Empennage
|
|
|
Empennage Type
|
Conventional |
|
Empennage Rib Material
|
Sheet Metal |
|
Empennage Skin Material
|
Aluminum |
|
Rudder Trim
|
Cable Link Trim Tab |
|
Yaw Trim Actuator
|
Manual |
|
Yaw Control System
|
Cable and Pully |
|
Pitch Trim
|
Cable Link Trim Tab |
|
Pitch Control System
|
Cable and Pulley |
|
Pitch Trim Actuator
|
Manual |
|
Landing Gear
|
|
|
Landing Gear Type
|
Tricycle |
|
Retractable
|
No |
|
Retraction System
|
N/A |
|
Emergency Extension
|
N/A |
|
Ground Steering
|
Rudder Pedals |
|
Shock Absorbtion Main Gear
|
Oil/Air Strut |
|
Shock Absorbtion Other Gear
|
Nosewheel Air/Oil Strut |
|
Brake Type
|
Hydraulic Actuated Brake Disc |
|
Brake Controls
|
Toe Brakes |
|
Cabin
|
|
|
Instrument Panel
|
IFR non Glass |
|
Flight Control
|
Ram Horn Yoke |
|
Number of Seats
|
6 |
|
Heating
|
Engine Exhaust Shroud |
|
Window Defrost
|
Ducted Hot Air |
|
Cooling
|
Ducted Ram Air |
|
Profiles
|
|
|
Normal Climb Profile Speed (KIAS)
|
91-100 |
|
Maximum Climb Profile Speed (KIAS)
|
82 |
|
|
Engine
|
|
|
Number of Engines
|
1 |
|
Engine Manufacturer
|
Lycoming |
|
Engine Model
|
IO-540-K1A5 |
|
Engine Type
|
Normally Aspirated Piston |
|
Geared
|
Direct Drive |
|
Cooled
|
Air Cooled |
|
Fuel/Air Mechanism
|
Fuel Injected |
|
Number of Cylinders
|
6 |
|
Max HP
|
300 |
|
Starter System
|
Electric Starter |
|
Propeller
|
|
|
Propeller Manufacturer
|
Hartzell |
|
Propeller Model
|
|
|
Number of Blades
|
3 |
|
Minimum Diameter
|
|
|
Maximum Diameter
|
80 |
|
Propeller Type
|
Constant Speed |
|
Propeller Governor
|
Oil Pressure |
|
Fuel System
|
|
|
Fuel System Type
|
Fuel Pump |
|
Approved Fuel Type 1
|
100LL |
|
Approved Fuel Type 2
|
100/130 |
|
Approved Fuel Type 3
|
|
|
Fuel Capacity (G)
|
84 |
|
Tank Type 1 Location
|
Left Wing |
|
Tank Type 1 Capacity (G)
|
42 |
|
Tank Type 2 Location
|
Right Wing |
|
Tank Type 2 Capacity (G)
|
42 |
|
Usable Fuel (G)
|
83.5 |
|
Oil Capacity (Quarts)
|
12 |
|
Electrical System
|
|
|
Power Source
|
Engine Driven Alternator |
|
Power Storage
|
Battery |
|
System Voltage
|
12V |
|
Alternator Amp
|
60amp |
|
Battery Voltage
|
12V |
|
Battery Amp/Hour
|
|
|
Limitations
|
|
|
Maximum T/O Weight (lbs)
|
3400 |
|
Maximum LDG Weight (lbs)
|
3400 |
|
Standard Empty Weight (lbs)
|
1968 |
|
Useful Load (lbs)
|
1432 |
|
Station 1 Baggage Location
|
178.7 |
|
Max Weight Station 1 (lbs)
|
100 |
|
Station 2 Baggage Location
|
42 |
|
Max Weight Station 2(lbs)
|
100 |
|
Station 3 Baggage Location
|
|
|
Max Weight Station 3(lbs)
|
0 |
|
Wing Loading (lbs/sq.ft)
|
19.5 |
|
Vne (KCAS)
|
184 |
|
Vno (KCAS)
|
146 |
|
Va(Max Gross) (KCAS)
|
129 |
|
