Beechcraft Baron 58: Reference

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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.........................238°C
Maximum Oil Temperature.............................................116°C
Minimum Take-off Oil Tempreature.................................24°C
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