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FOR
FLIGHT SIMULATION USE ONLY
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AIRSPEED INDICATOR
MARKINGS*
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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)
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152 |
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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
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