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Flight and Operational Manual 

TL- 96 STAR                                                                                s/n 99 S 25 

Notice! The information contained in this document is for reference and information only. 

The pilot is the final and only responsible party for the safe operation of this aircraft. 

 

 

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5.3.Rate of climbs and height loss from the beginning of stalling 

The values of rate of climbs are valid for maximum weight of the airplane-450kg with maximum 

steady  output  of  the  engine  and  after  the  recount  to  the  zero  height  by  the  MSA.  With 

increasing height the rate of climb expressively decreases.  

Rate of climb for the engine Rotax 912                4,6m/s 

Rate of climb for the engine Rotax 912S              4,8m/s 

 

The  loss  of  height  from  the  beginning  of  stalling  in  direct  flight  till  reinstatement  of  the 

horizontal flight using the common procedures is 15m. 
The loss of height by stalling in strictly flying turn at the bank of 30 degrees from the beginning 

of stalling till reinstatement of the horizontal flight is 20-25m. 

 

  

5.4.Ceiling 

Practical ceiling is 6500m with the airplane with engine Rotax 912 and 912S with the maximum 

taking off weight. Practical ceiling means the height of the airplane when it is able to be rising 

with the speed at least 0.5m/s. 

 

5.5.Gliding range 

Introduced value of the gliding range is valid for wooden 2blade airscrew and the speed of the 

flight 130km/h. 

Gliding range with no load engine                               16.8 
Gliding range with turned off engine                           15.2 

 

When  using  other  than  introduced  airscrew,  especially  3blade  is  the  real  gliding  range  by  no 

load  engine  slightly  higher  /  principle  of  bigger  tension/.  and  with  turned  off  engine  slightly 

lower / the principle of higher aerodynamic force / 

 

5.6 Length of start 

Introduced  length  of  start  is  prescribed  for  the  maximum  weight  450kg,  by  dead  calm,  dry, 

straight and shortly cut lawn, with the position of lifting flaps prescribed for the start. There is 

prescribed the value of sticking off the launching area and for reaching the height of 15m. 

 

Engine                 After sticking off                  Across the obstruction at the height of 15m 
912                                       90m                                             290m 

912S                                     75m                                             250m 

 

5.7.Landing length 

Introduced length of landing is prescribed for the maximum weight of 450 kg, by dead calm, 

dry  and  straight  and  short  cut  lawn  and  with  the  position  of  lifting  flaps  prescribed  for  the 

landing. There is a value for maximum effective braking / without blocking the wheels / and for 

the landing without using the brakes. 

The length of landing with using the brakes                 100m 

Length of landing without using the brakes                  300m 

 

Do not forget  the landing length will expressively elongate, if you try to land with wind in the 

back. If it is only possible, land always against the wind.  

 

 

Summary of Contents for TL-96 STAR

Page 1: ...responsible party for the safe operation of this aircraft 1 T L U L T R A L I G H T Leti t 515 Pouchov 503 41 Hradec Kr lov tel fax 049 5213378 tel 42049 5218910 tel 42049 5211753 info tl ultralight c...

Page 2: ...light and reparation of position fault of airspeed indicator 11 2 1 1 Airspeed ind data reparation regarding the position fault of Pitot tube 12 2 1 2 Reparation table of real and indicated air veloci...

Page 3: ...id 23 4 9 Landing 23 4 10 Tasks after landing 23 4 11 Pilotage in lateral wind 23 4 12 Flight in turbulent atmosphere 24 4 13 Standing up to the lane 24 5 Output 24 5 1 Conditions for output assessmen...

Page 4: ...7 2 12 Changing the fuel filter in the engine area 34 7 2 13 Maintenance of airscrew SR 2000 xa 35 7 3 Contract revision 35 7 4 Periodical revision after every 50hours 35 7 5 Periodical revision afte...

Page 5: ...flying with TL 96 Star is much economical and its maintenance is also much easier I believe that the aircraft will operate for your enjoyment for very long time and it will satisfy you Also this Fligh...

Page 6: ...holder TL 96 Star are put into effect These changes are gradually paginated and they contain removable pages Respective pages should be changed in the guidebook If there is no page with such number ne...

Page 7: ...the supply is ensured electrically The fuel tank is equipped with lockable lid placed on the front right side of the fuselage The producer of the fuel system is also the company TL Ultralight 1 2 3 P...

Page 8: ...both top parts of pedal both wheels of main undercarriage are braking Lifting flaps Compressing the button on the hand lever between the seats and snapping this bar up we can rebuilt the lifting flap...

Page 9: ...rmation contained in this document is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 9 1 3 Layout of the airplane There ar...

Page 10: ...ith a pilot with the lowest allowed weight there can not be any load on the plane the fuel tank must be empty at the weighing machines under the main undercarriage deduct the data of the weighing mach...

Page 11: ...ictions 2 1 Restriction of the speed of the flight and reparation of position fault of air speed recorder Presented speeds of the flight applies to the maximum take off weight of 450kg and at the cond...

Page 12: ...the mistake is increasing For security reasons not extending the maximum allowed speeds we choose the type of lower real calibrated speed than the indicated speed All speed limits introduced in this g...

Page 13: ...al requirement for protecting the propeller against all winds effects for all types of delivered propeller Covers for your airscrew blades were delivered together with your airscrew and please use the...

Page 14: ...is enclosed in the instruction for maintenance for the engine Also used airscrew expressively influences the consumption Positioning the angle of incidence of the airscrew blades can be a compromise...

Page 15: ...prohibited 2 5 1 Allowed turns non acrobatic operations in sense of definitions proposed at the top by the rule UL2 sharp turns are not recommended at lower speed than 130km h use maximum 1 3 of full...

Page 16: ...ULLa is on board the pilot can have the qualification of learner ULLa piloting learner ULLa can be on board alone when he is taken aback by the valid training program in such part when he is able to o...

Page 17: ...and flying attributes need to be considered There are these restrictive conditions Maximum outside temperature 45 degrees of Celsius Minimum outside temperature 15 degrees of Celsius Maximum vertical...

Page 18: ...of the engine failure perform these tasks bring you airplane to gliding make sure the ignition is on check the fuel status try to launch the engine If the engine is not able to start up proceed by th...

Page 19: ...plane is equipped with the saving system you have received with handed documentations Guidebook for assembling and using the saving system elaborated by the producer Go through this guidebook in its f...

Page 20: ...f the engine is not started let the starter cool down for about 2 minutes and then repeat the starting Overheated starter loses its output very quickly and the engine is hard to start with it because...

Page 21: ...the check up consists of these activities while taxying try the function of the brakes and pilotage of the front wheel maximum speed of taxying is 4km h slow walk set the altitude meter check the gas...

Page 22: ...d speed when taking off is enclosed at the point 2 9 Meteorological restrictions 4 6 Tasks after reaching the flight level trim the regime of the engine to travel regime in case of adjustable aircrew...

Page 23: ...s task Consecutive slight speed increase will enable to keep the direction of landing because the rudder is still adequately effective If you will be coming to landing with too low speed even though s...

Page 24: ...g in turbulence Be ready to quickly add and detract the gas The flight in turbulence is stressing for the pilot and also for the airplane If it is possible you can mount to higher flight level where m...

Page 25: ...ntroduced value of the gliding range is valid for wooden 2blade airscrew and the speed of the flight 130km h Gliding range with no load engine 16 8 Gliding range with turned off engine 15 2 When using...

Page 26: ...gest effectiveness Lower there is a table for the airscrew SR 2000xa Table of optimal speed at setting the blades from the smallest which is 12 degrees to the biggest which is 22 degrees Engine with t...

Page 27: ...cabin with suitable cover 6 2 Anchorage of the airplane Anchore the airplane to sufficient strong anchore screw anchor is recommended with cables and straps Anchore the airplane at these places screw...

Page 28: ...out the elevator to the back 6 4 2 Assembly of the plane The assembly of the plane should be performed by to persons in reversed order than the disassembly of the plane ATTENTION All self stop hunts...

Page 29: ...he screw of the dashpot stirrup check up the spring integrity of the exhaust stroke piping check the tightness of oil cooler and the cooling liquid cooler Check the untightness of the sparks which cou...

Page 30: ...as in the space between the elevator and the rudder from top nuts screws possible flaws in the varnish Left side of the body the same as the right side locking the assembly hole the rudder Left wing t...

Page 31: ...high lawn which can expressively take the trouble on the airscrew Regular conservation with high quality car vosk expressively terminates aging of the varnish Park the airplane in covered hangar if po...

Page 32: ...riage leg plastic lubricant once a year Aileron hang ups transmission oil after 50 hours Upper and bottom rudden hang up transmission oil after 50 hours Elevator hang up weighting transmission oil aft...

Page 33: ...the inside braking plate to the direction down and take it out of the brake valve take out the brake valve from the braking disk by compressing to back screw out the inside nut of the hinge of the wh...

Page 34: ...rea We can not say how often the fuel filter should be changed because it depends on how well you filter the fuel while filling the tanks That s why use fuel filters with clear housing only you can se...

Page 35: ...ance of the airplane otherwise the revision is made in the service center of the producer The revision consists of these tasks the before flight revision in its full length revision of all screw and h...

Page 36: ...the low part of the engine hood Do not forget about ensuring the wheels of the main undercarriage by the wedges on both sides while supporting the airplane on these points The jacking points prescrib...

Page 37: ...ion of the pilotage flight test with a probationary pilot must be done 8 4 Airframe repair The damaged surface should be cemented rubbed and varnished when it is damaged slightly When perforation of n...

Page 38: ...ur airplane Keep the engine in cleanness and watch out incidental leakage of oil which can signalize the necessity of expert maintenance of the engine We introduce only the basic tasks for the mainten...

Page 39: ...id leak out after letting it out put the pipe back on the cooler and tighten the buckle carefully While exchanging the refrigerating liquid it is also necessary to exchange the tamping under the low t...

Page 40: ...ENTION Condition for incidental successful reclamation of the engine faults is keeping prescribed revision and work on the engine only the way the producer of the engine prescribed or by the authorize...

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