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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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7.7.Periodical revision after every 300hours 

This revision is made after every 295-305 flight hours  or after three years of operating. The 

diagnostics  of  all  stressed  parts  of  the  construction  is  made  and  also  its  detailed  range  is 

prescribed by the internal rule of the producer by the detected state. We introduce here basic 

tasks for your information: 

 

 
 

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 outer revision of the whole airframe 

pilotage revision 

replacement of intended parts 

flight test by the probationary pilot 

 

ATTENTION! 

This revision is made only by the service center of the producer. 

 
 

7.8.Jacking points on the plane 

The jacking points made by the low inside buckles of the engine bed to the body partition  

are made for lifting the front undercarriage. These jacking points are approachable after taking 

off  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  prescribed  for  the  lifting  are  placed  on  the  low  part  of  the  wings  in  the 

distance of 190cm from the body. The supporting mean must be made of a hard construction, it 

must be at least 100mm wide and 1000mm long. This supporting part, which supports the wing 

must have a soft, 20mm thick felt cover, which enables the weight of the supporting part of the 

airplane to disintegrate to its whole area.  
After interposing the support under the supporting area, we lift the wing on its low end part by 

arms the way to let the lifting force disintegrate on its whole length. 

The main undercarriage wheels can be supported by the low parts of the spring constituting the 

main undercarriage. 

 

7.9.List of labels and their placing 

the producer label of the body is placed on the inner left side of the airplane in the area 

behind the pilot’s seat.  

producer label is placed on the partition behind the seat of the fellow-traveler 

the label introducing the maximum weight of the crew and the load in the dependency 

of filling the fuel tank is sticked inside on the left front part of the cabin 

the  label    indicating  used  engine  oil  is  on  the  control  tap  of  the  upper  cover  of  the 

engine 

 

 

Содержание TL-96 STAR

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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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