Ultra Start KE-6 Service Manual Page 2

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1. General information
1.1. Important information
1.2. Description of airplane 5
1.2.1. Airframe 5
1.2.2. Fuelsystem 6
1.2.3. Airscrew 6
1.2.4. Engine 6
1.2.5. Meaning of movement of control component units 7
1.2.6. Basic technical data of the airplane 7
1.3. Layout of the airplane 8
1.4. Detecting the center of gravity position, allowed and measured values 9
1.4.1. Weighting the airplane for the the headmost center of gravity 9
1.4.2. Weighting the airplane for the backmost center of gravity 9
2. Operating restrictions 11
2.1. Restriction of the speed of the flight and reparation of position fault of
airspeedrecorder
11
2.1.1. Air-speed recorder data reparation regarding the position fault of Pitot tube 11
2.1.2. Reparation table of real and indicated air-velocity 11
2.2. Weights and loads 12
2.2.1. Maximum and minimum weights 12
2.2.2. Siting of the load 12
2.3. Engine operating restrictions 12
2.4. Air-screw operating restrictions 13
2.4. Fuel and lubricant oil 13
2.4.1. Fuel Tank 14
2.4.2. Consumption of the fuel 14
2.5. Restriction of maneuver 15
2.5.1. Allowed turns 15
2.5.2. Flight multiples 15
2.6. The crew 15
2.6.1. Minimal and maximal weight of the crew 15
2.6.2. Pilot qualification 16
2.6.3. Pilot´s place on the plane, ageof the crew, application of seat belts 16
2.7. Maximum flight height 17
2.8. Meterologic condition restriction 17
2.9. Carriage of goods restriction 18
2.10. Types of airport traffic 18
3. Emergency process
19
3.1. Misfire of the engine 19
3.1.1. Misfire of the engine during the flight to the height 200m 19
3.1.2. Misfire of the engine during the flight above the height 200m 19
3.2. Fire on board of the plane 19
3.3. Vibrations 19
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