Ultra Start KE-6 Wartungshandbuch

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T L U L T R A L I G H T
Dobrovského 734
500 02 Hradec Králové
tel/fax 049 5613378
tel +42049 5618910
tel +42049 5611753
www.tl-ultralight.cz
T L - 96 STAR
F l i g h t a n d o p e r a t i o n a l m a n u a l
Published in December 2000
Serial number: Imatriculation:
1
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1 2 3 4 5 6 ... 47 48

Inhaltsverzeichnis

Seite 1 - T L U L T R A L I G H T

T L U L T R A L I G H TDobrovského 734500 02 Hradec Královétel/fax 049 5613378tel +42049 5618910tel +42049 5611753e-mail: [email protected]

Seite 2

1.4.Detecting the center of gravity position, allowed and measured valuesObservance of the center of gravity is decisive for the stability and managea

Seite 3

1.4.3. Measured values of the center of gravity for the airplane TL-96 Star before test flyingSeriál.number: Measured value Unit

Seite 4

2.Operating restrictions2.1. Restriction of the speed of the flight and reparation of position fault of air-speed recorderPresented speeds of the flig

Seite 5 - TL Ultralight

Indicated Actual Indicated Actual I ndicated Actual 60 58 110 103 160 14870 67

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Engine restrictions for engines Rotax 912 and 914, for the 912S are the same values as for engine 912.Minimum temperature of air when taking off in Ce

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2.4.1.Fuel supplyTotal volume of tanks 67litresUnexhaustible supply

Seite 8

The restriction of the airplane UL in the view of allowed maneuvers is determinated by the requirements of the rule UL2 part 2. which allows for this

Seite 9 - 1.3.Layout of the airplane

Second condition is not to overpass the maximum total weight of the airplane 450kg. The observance of this condition is for the airplane to have the a

Seite 10

The age of the pilot is not confined in any way and is derived of the requirements of the minimum age of the pilot or piloting learner by the rule UL3

Seite 11

Operating restrictions of the airplane in the way of meteorological conditions in cooler weather are determinated mostly by the possibility of ice for

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1. General information 1.1. Important information 1.2. Description of airplane 51.2.1. Airframe 51.2.2. Fuelsystem 61.2.3. Airscrew 6

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3.Emergency process3.1.Misfire of the engineThe procedure while failure of the engine differs due to the time we have to solve the situation, so the h

Seite 14

The airplane signalize the vibrations in pilotaging the airplane with approaching stalling speed, this is the consequence of beginning breaking of th

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When the airplane is dropping steadily, the airplane is in the position wheel down. It is necessary to count with a damage of the airplane when fallin

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4.Normal processes4.1.Starting up the engineTasks which need to have be done especially before first startup of the engine in the flight day, or in t

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-do the test of ignition at the revolutions of 4000/min, the drop of the revolutions for each circuit can not be higher than 300 revolutions per minut

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4.4.TaxyingMaximum speed of taxying is 4km/h. There is a very good view from the airplane while taxying but be careful for barriers in front of the ai

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4.7.Flight at the flight levelAt flight at the flight level it is necessary to count with big sensitivity of controlling agents and the reactions to t

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Consecutive slight speed increase will enable to keep the direction of landing because the rudder is still adequately effective. If you will be coming

Seite 21

If your airscrew is adjustable, set it on a smaller incidence angle and fly with higher revolutions of the engine, you will have the dispos

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5.Output5.1.Condiotions for output assessmentLower introduced values are valid only by the conditions of MSA at the sea level and for a steady flight

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3.4. Undercarriage failure 203.4.1. Main undercarriage failure 203.4.2. Proe undercarriage failure 203.5. Using the saving systém 204. N

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When using other than introduced airscrew, especially 3blade is the real gliding range by no load engine slightly higher / principle of bigger tension

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Table of optimal speed at setting the blades from the smallest, which is 12 degrees, to the biggest, which is 22 degrees. Engine with the reductor at

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5.9. Flying rangeThe flying range initiated in steady speed 170km/h, on the land by adjustable three blade airscrew FITI and again recounted to

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6.4.Assembly and disassembly of the planeAssembly and disassembly of the plane could be done only by trained persons. Assembly and disassembly is reco

Seite 28

-wash and rub off the blades of the aircrew from the sedentary dirt-wash, rub off and furbish the glass parts of the cabin, use only one bucksin leath

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Check possible fouling of the fuel filter, change it if necessary. If you recognize the fuel filter fouling in the engine space, perform extraordinary

Seite 30

Screw connections, hinges, springs6.7. Filling the fuelDue to the composite construction of the airplane, increasing occurrence of the static electric

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7.Service life of airplane and maintenance periodicity Regular and careful proceeding of the maintenance is the principle of reliable and safe operati

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7.2.1.Lubricant plan and lubricant preparationFor lubricating the engine, use only the oil prescribed by the engine producer and introduced in the mai

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7.2.3.Disassembly of the front wheelThe disassembly demands the cooperation of two persons. Prepare the bracket under the support points by the point

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7.2. Workaday maintenance 367.2.1. Lubricant plan and lubricant preparation 377.2.2. Blocking, raising and jogging along preparation 377.2.3. D

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7.2.6.Electrical system voltage Basic electrical installation on the plane is with the voltage of 12V and two wire conductors. The electrical installa

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ATTENTION!Perform the filter change on a cool engine onlyThe progress while changing the fuel filter:-close the fuel delivery-take out the upper cover

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7.3.Contract revisionIntroductory revision is made after first 25 flight hours by the producer in his service center. Performing this revision by the

Seite 38

-revision after 100hours-taking off the airscrew and the engine-revision of the construction-revision of the interior of the body and the cabin-the ou

Seite 39

-the label indicating used engine oil is on the control tap of the upper cover of the engine8.Airplane repairs8.1.Repairs of connection screwIn case

Seite 40

8.6.Engine repairsAll reparation of the engine and its aggregates can be performed only the service center of the producer. These types of faults c

Seite 41

9.Engine Rotax 912/912S maintenanceThere are most information and derection needed for the operating of the engine Rotax 912/912S in the handbook for

Seite 42

9.4.Service life of the plane, revisions and inspection of the engineUse the liquid with anti corrosive ingredients prescribed for the block of engi

Seite 43

ATTENTION!The engine producer prescribes after every exchange of the filter to cut the old filter, it should be taken out, unfolded and looked throug

Seite 44

Dear airplane holder, I would like to compliment you on the purchase of the ultra light airplane TL-96 Star which is the result of many years of

Seite 45

1.General informationIn case that this guidebook reveals to the rule UL1, UL 2 or UL 3, it is only a calling off corresponding rule of Letecké amatérs

Seite 46

The cabin is arranged with seats next to each other, it is covered with large either clear or with darker toned cover, which provides an exceptional v

Seite 47

1.2.5.Meaning of movement of control component units Foot pilotage:Pushing on the left foot pedal, the airplane turns to the left if on land or in the

Seite 48 - Natural BA 95

1.3.Layout of the airplaneThere are all the drawn dimensions in the layout. 1.4. recalls to this layout.9

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