2008 POH

KCAS

Calibrated Airspeed is the indicated airspeed corrected for position and instrument error and expressed in knots.

KIAS

Indicated Airspeed is the speed shown on the airspeed indicator and expressed in knots.

KTAS

True Airspeed is the airspeed expressed in knots relative to undisturbed air, which is KCAS: corrected for altitude and temperature.

VA

Design maneuvering speed

VC

Design cruising speed

VFE

Maximum Flap Extended Speed is the highest speed permissible with wing flaps in a prescribed extended position.

VH

Max Speed in level flight with Max continuous power

VLO

Lift off speed- is the speed at which the aircraft generally lifts off from the ground.

Section 3- CG locations

For: 20% MAC (Mean Aerodynamic Chord) 72.5 in

Aft: 33% MAC (Mean Aerodynamic Chord) 79.5 in

VNE

Never Exceed Speed is the speed limit that may not be exceeded at any time.

VNO

Maximum Structural Cruising Speed is the speed that should not be exceeded except in smooth air, then only with caution.

VS

Stalling Speed or minimum steady flight speed flaps retracted

VS0

Stalling speed or minimum steady flight speed in landing configuration

VS1

Stalling speed in clean configuration (flap 0°)

VX

Best Angle-of-Climb Speed is the speed, which results in the greatest gain of altitude in a given horizontal distance.

VY

Best Rate-of-Climb Speed is the speed, which results in the greatest gain in altitude in a given time.

VR

Rotation speed: is the speed at which the aircraft rotates about the pitch axis during takeoff

RPM Revolutions Per Minute

is the number of revolutions per minute of the propeller, multiplied by 2.4286 yields engine RPM.

1.3.1.1 Wing-wing span

29.5 ft

1.3.1.1 Wing-aspect ratio

6.7 ft

1.3.1.1 Wing-chord

4.5 ft

1.3.1.2 Fuselage length

22.7 ft

1.4.1 Engine-Manufacturer

Bombardier-Rotax GmbH

1.4.1 Engine- Model

914 UL-

UL = Ultralight (Non-Type Certified)

1.4.1 Engine- Certification

ASTM 2339 LSA

1.4.1 Engine- type

4-stroke carburetor engine

1.4.1 Engine- max power

113 hp at 5800 rpm

1.4.1 Engine- max can't power

98.5 ph at 5500 rpm

1.4.2. Propeller

Fixed ground adjustable 3-blade Sensenich manufacturer 68 inches and no reductions permitted (No shortening the propeller)

1.4.3. OIl System

Forced dry sump system

1.4.3 Oil Capacity

Max 3.2 qt and minimum 2.1 qt- SB says 2.6 qts

1.4.4. Cooling

Air and liquid-cooled

1.4.5. Fuel types that can be used

100 LL, AKI 91 PRemimum USA, EN 228 Premium and Premium Plus

1.4.5. Fuel capacity

15.8 gal, 31,7 gal (1.1 unusable)

1.5.1 Max take-off and landing

1320

1.5.1 Max baggage

44 lb

1.8.1 The dual ignition system

is a solid state, breakerless, capacitive discharge, interference suppression system instead of a mechanical magneto system. Each ignition system is powered by individual and totally independent AC generators which are not dependent on the aircraft battery.

1.8.1 The dual carburetors are

constant depression carburetors that automatically adjust for altitude.

1.8.1 Two electric fuel pumps feed the engine. When do they turn on

One is automatically switched ON when the engine is running; the auxiliary one is controlled by the pilot.

1.8.1 Cooling system is designed for liquid cooling of

the cylinder heads and ram-air cooling of the cylinders. The liquid system is a closed circuit with an overflow bottle and an expansion tank.

1.8.1 The coolant flow is forced by

a water pump, driven from the camshaft, from the radiator to the cylinder heads.

1.8.1 From the top of the cylinder heads the coolant passes on to the

expansion tank. Since the standard location of the radiator is below engine level, the expansion tank, located on top of the engine, allows for coolant expansion.

The engine uses a reduction gearbox with a gear reduction ratio of

2.4286 to 1.

1.9 Electrical system

12 volt DC circuit controls by master switch

1.9 Generator info

AC generator

1.9 battery

12 volt

2.1.1 VNE

Never exceed speed 145 Never exceed this speed in any operation

2.1.1 VNO

Maximum Structural Cruising Speed 113 Never exceed this speed unless in smooth air, and then only with caution

2.1.1 VA

Maneuvering speed 98 Do not make full or abrupt control movements above this speed as this may cause stress in excess of the limit load factor

2.1.1 VFE

Maximum flap extended speed 71 Never exceed this speed for any given flap setting

2.1.1 VH

Maximum speed 120 Maximum speed in level flight at max continuous power (MSL)

2.1.1 VX

Best Angle Climb 65 The speed which results in the greatest gain of altitude in a given horizontal distance

2.1.1 VY

Best Rate Climb 78 The speed which results in the greatest gain of altitude in a given time

2.1.2 White Arc

40-71- flap operating rang at max weight

2.1.2. Green Arc

48-113- Normal operating range

2.1.2 Yellow Arc

113-145 only in smooth air

2.1.2 Red line

Max speed

2.1.4 Max Cylinder Head temp

135C

2.1.4 Max Coolant temperature

120 C

2.1.4 min/max oil temperature

50/130 C

2.1.4 Oil normal operating temperature

90-110C

2.1.5 Oil Pressure

Minimum: .8 Bar below 35 RPM

2.1.5 OIl Pressure MInimum

2-5bar above 35 RPM

2.1.6 Operating and starting temperature range

-25 to 50

Admissable pressure for a cold start is

7 bar for short periods

2.1.7 Fuel Pressure

Min .15 Bar and .35 Bar Max

9.1.12 Prolonged use of Aviation Fuel Avgas 100LL results in

greater wear of valve seats and greater combustion deposits inside cylinders due to higher lead content.

2.1.17 Approached maneuvers

Any maneuver pertaining to normal flight, stalls (except whip stalls), Lazy 8s, Chandelles, Turns in which the angle of the bank is not more than 60, and acrobatic maneuvers are not approved.

2.1.18 Maneuvering load factor limits

4 to -2 0 degrees of flaps, landing flaps is +2 to 0.

2.1.23 IFR

Not allowed

2.1.24 Max Cross wind

15 kts

2.1.25 Service Ceiling

16,000' the altitude at which an aircraft can no longer climb faster than a specified rate

3.2.1 Datum location

Propeller Support flange w/o spacer

4.6 Stall recovery with less than 30 banks

200ft

Tire inflation

32 PSI nose and 40 PSI main

Shut down the engine if the oil doesn't

Rise within 10 seconds

Starter duty cycle

10 seconds with 2 minutes cool down

Optimal touchdown speed

45

KOEL-per the G3X

Magnetic direction indicator; ELT; Strobe lights; G3X Touch suite: Airspeed indicator; Altimeter; RPM indicator; Oil pressure indicator; Oil temperature indicator; Cylinder Head Temp. Indicator (or Coolant Temp. indicator); Fuel quantity indicator.

KOEL- per G3X-night

instrument lights and position (nav) lights

Operating Limitations of Autopilot

1,000 feet in cruise, must not be used for final approach procedure, can't use with flaps extended more than T/O, A/P master must be off during TakeOff and Final Approach,

Glide Ratio

Glide ratio is 12.8 therefore with 1000 ft of altitude; it is possible to cover ~2 nautical miles in zero wind conditions.