Baron 58 Cockpit Simulator

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FOR FLIGHT SIMULATION USE ONLY

AIRSPEED INDICATOR MARKINGS*
AIRSPEED LIMITATIONS

Speed IAS / kts
Maneuvering (Va)   156
Maximum Flap Extended Speed (Vfe) Approach (15) 152
Full Down (30) 122
Maximum Structural Cruising (Vno)   195
Never Exceed (Vne)   223
Maximum Landing Gear Operating/Extended( Vlo/Vle)   152

    POWER PLANT LIMITATIONS

   NUMBER OF ENGINES

    Two

   ENGINE MANUFACTURER
   
Teledyne Continetal Motors Corp. (Mobile, Alabama)

   ENGINE MODEL NUMBER
   
IO-550-C

   ENIGINE TYPE
   
Normally aspirated, fuel-injected, direct-drive, air-cooled,
   six-cylinder, horizontally opposed, 550-cubic-inch
   displacement, 300 hp.

   HORSEPOWER RATING
   
300 H.P.

   NUMBER OF PROPELLERS
   
Two

   PROPELLER MANUFACTURER
   
McCauley Propeller (Vandalia, Ohio)

   NUMBER OF BLADES
   
3

   PROPELLER TYPE
   
Constant speed, Hydraulically Actuated

   EINGINE OPERATING LIMITATIONS
   
Take-off and Maximum
   Continuos Power..................................Full Throttle, 2700 rpm
   Maximum Cylinder Head Temperature.........................238C
   Maximum Oil Temperature.............................................116C
   Minimum Take-off Oil Tempreature.................................24C
   Minimum Oil Pressure (idle)...........................................10 psi
   Maximum Oil Pressure.................................................100 psi
   
   STARTERS (Time For Cranking)
   
   Do not operate starter continuously for more then 30
   secounds in any 4-minute period. Allow starter to cool again
   before cranking.


   FUEL LIMITS
   
   APPROVED ENGINE FUELS
   

   100LL (blue)
   100 (green)
   115/145 (purple)
   
   
   FUEL CAPACITY
   
   STANDARD FUEL SYSTEM
   
   
Totlal Capacity.........................................................142 Gallons
   Total Useable...........................................................136 Gallons
   
   OPTIONAL FUEL SYSTEM
   
   
Totlal Capacity.........................................................200 Gallons
   Total Useable...........................................................194 Gallons
   
   
   OIL CAPACITY
   
   12 Quarts (each engine)
   
   
   WEIGHT LIMITS
   
   Maximum Take-off........................................................5500 lbs
   Maximum Landing........................................................5400 lbs
   Maximum Ramp............................................................5524 lbs
   
   Maximum Baggage Compartment Weights
   Maximum Cabin Compartement...................................400 lbs
   Maximum Extended Aft Compartement.......................120 lbs
   Maximum Nose Compartement....................................300 lbs
   
   
   MANEUVER LIMITS LIMITS
   
   This is a noraml catagory airplane. Acrobatic maneuvers,
   including spins, prohibited.
   
   
   FLIGHT LOAD FACTORS (5500 Pounds)
   
   Positive Maneuvering Load Factors
   Flaps Up (0)......................................................................3.8 G
   Flaps Down (30)...............................................................2.0 G
 

 

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