SPECIFICATIONS:  

 

 

Aircraft Dimensions
Wing span 46'  .48"
Length 47' 3.24"
Height 13' .90"

 

Weight and Balance
Empty weight 7,200 lb.
Maximum Takeoff Weight (MTOW) 11,600 lb.

 

Engine
Manufacturer Pratt & Whitney 
Type Turboprop
Model PT6A-66
Horsepower (ea.) 850 @ 2,000 RPM
Fuel Jet A

 

Propeller
Manufacturer Hartzell Propeller, Inc.

Hub Model

   Left

   Right

 

HC-E5N-3A CW Rotating

HC-E5N-3AL CCW Rotating

Number of Blades

5

 

Altitude Limits
Maximum Approved Altitude 38,000 ft..
Ceiling 41,000 ft.

 

Temperature Limits

 

 

Interstage Turbine Temperature (ITT)

 

 

     Green Arc (Normal Operating Range)

200-830C

 

     Radial Red Line (Maximum)

830C

 

Oil Temperature

 

 

     Green Arc (Normal Operating Range)

20-110C

 

     Radial Red Line (Maximum)

. 110C

 

Pressure Limits

 

Oil Pressure

 

 

     Radial Red Line (Minimum) (Idling)

60 PSI

 

     Green Arc (Normal Operating Range)

90-135 PSI

 

Hydraulic Pressure

 

 

     Normal Operating Range

1000-3000 PSI

 

     Radial Red Line (Maximum)

3000 PSI

 

 

Airspeed Limitations
VA Maneuvering Speed 199 KIAS
VFO Max Flap Operating Speed
  UP to MID
  MID to DN
 
170 KIAS
150 KIAS
VMCA Air Minimum Control Speed
  Autofeather system operating
  Propeller windmilling
 
100 KIAS
128 KIAS
VFE

Flaps Max Extend Speed

   MID          

   DN

 

180 KIAS

175 KIAS

VLO Landing Gear - Operation 180 KIAS
VLE Landing Gear - Max speed when extended 185 KIAS

 

Fuel Limitations
Fuel Capacity (U.S. gal.)  
     Main Tank (x 2)                160.0
     Aux. Tank (x 2)      51.0
     Total (all tanks)                   422.0