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| 36'-1" with strobe lights installed |
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Lycoming IO-360-L2A:
Normally aspirated
direct drive
air cooled
horizontally opposed
fuel injected
four cylindar engine with 360 cu. in. displacement
180 BHP at 2700 RPM |
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McCauley Propeller Systems
2 blade
76 inch diameter
fixed pitch |
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100LL Grade Aviation Fuel (blue)
100 Grade Aviation Fuel (green)
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Total capacity: 56 gallons
Total usable: 53 gallons
Total capacity each tank: 28 gallons
Toal usable each tank: 26.5 gallons |
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Maximum at sea level: 126 KNOTS
Cruise, 75% power at 8500 feet: 124 KNOTS |
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75% power at 8500 feet: 518 NM
With 53 gallons 4.26 HRS
45% power at 10,000 feet: 638 NM
With 53 gallons 6.72 HRS |
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| RATE OF CLIMB AT SEA LEVEL |
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Ground roll: 960 FEET
Total distance over 50 foot obstacle: 1630 |
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Ground roll: 575 FEET
Total distance over a 50 foot obsticle: 1335 |
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Flaps up, power off: 53 KNOTS
Flaps down, power off: 48 KNOTS |
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Ramp: Normal 2558 POUNDS
Utility 2208 POUNDS
Takeoff: Normal 2550 POUNDS
Utility 2200 POUNDS
Landing: Normal 2550 POUNDS
Utility 2200 POUNDS |
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Normal 895 POUNDS
Utility 545 POUNDS |
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| Knots Calibrated Airspeed- is indicated airspeed corrected for position and instrument error. |
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| Knots Indicated Airspeed- Speed shown on airspeed indicator. |
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| Knots True Airspeed- Airspeed expressed relative to undisturbed air which is KCAS corrected for altitude and temp. |
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Maneuvering Speed- Maximum speed at which full or abrupt contol movements may be used without overstressing the airplane.
2550 POUNDS 105 KNOTS
2200 POUNDS 98 KNOTS
1900 POUNDS 90 KNOTS |
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Maximum Flap Extended Speed- Highest speed permissible with wing flaps in a prescribed exended position.
10 Degrees 110 KNOTS
20-30 Degrees 85 KNOTS |
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Maximum Structural Cruising Speed- Speed which should not be exceeded except in smooth air, then only with caution.
129 KNOTS |
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Never Exceed Speed- Speed limit that may not be exceeded at any time.
163 KNOTS |
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Stalling speed- Minimum speed at which the airplane is controllable.
(given in other cards) |
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Stalling Speed- Minimum speed at which the airplane is controllable in landing configuration.
(given on other cards) |
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Best angle of climb speed- Is the speed which results in the greatest gain of altitude in a givin horizontal distance.
(graph in POH) |
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Best Rate of climb Speed- Is the speed which results in the greatest gain in altitude in a given time.
(graph in POH) |
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| Outside Air Temp.- Free air static temp. |
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| 15 degrees celcius at sea level and decreased bt 2 degrees every 1000 feet of altitude. |
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| The altitude read from an altimeter when the altimeter's barometric scale has been set to 29.92 inches of mercury. |
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| Brake Horsepower- Power developed by the engine. |
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| Revolutions Per Minute- Engine speed |
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| Engine speed during a full throttle run up when the airplane in on the ground and stationary. |
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| Manifold Absolute Pressure- Absoute pressure measured in the engine induction system. |
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| Decreased proportion of fuel in the fuel air mixture. |
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| Increased proportion of fuel in the fuel air mixture. |
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| Mixture control full foward |
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| Is the fuel available for flight planning |
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| Quantity of fuel which cannot be safely used in flight |
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| Gallons Per Hour- Amount of fuel consumed per hour |
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| Nautical Miles Per Hour- the distance which can be expected per gallon of fuel consumed at a specific power setting and/or flight configuration. |
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| Acceleration due to gravity |
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| Compass referance used by the autopilot, along with course deviation. |
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| Imaginary verticle plane from which all horizontal dostances are measured for balance purposes. |
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| A location along the airplane fuselage given in terms of the distance from the reference datum |
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| The horizontal distance from the reference datum to the center of gravity of an item. |
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| product of weight of an item multiplied by its arm |
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| The arm obtained by adding the airplanes individule moments and deviding the sum by the total weight. |
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| the extreme center of gravity locations within which the airplane must be operated at a givin weight. |
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| Weight of a standard airplane including unusable fuel, full operation fluids, and full engine oil. |
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| Is the standard empty weight plus the weight of optional equipment |
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| Diffrence between ramp weight and basic empty weight |
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| Mean aerodynamic chord- The chord of an imaginary rectangular airfoil having the same pitching moments throughout the flight range as that of the actual wing. |
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| The weight of chocks, blocks, stands, ect. used when weighing an airplane and is included in the scale readings. |
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