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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. 

 

 

- 23 - 

4.8.1.Sideslid 

the slip should be performed at the speed between 120 to 130km/h. 

 

4.9.Landing 

Set  the  airscrew to  small angle  of incidence  if your airscrew is adjustable,  in  case    having  to 

repeat the landing, your engine would have the full disposal of output.  

Set the weighing of the airplane slightly heavy on the tale and fasten your seat belts.  

After  third  round  turn  shift  out  the  flaps  at  the  speed  125-130km/h.  After  fourth  round  turn 

slightly snap and shift the flaps to the 2

nd

 grade.  at the speed of 105-110km/h. After shifting 

out, increase the speed snapping to 115-120km/h, and go to landing with this speed till long 
wind. The way you are losing the long wind, wind down the speed. Thank to the down-to-earth 

lifting  force  you  will  be  bearing    relatively  slow,  on  the  main  undercarriage  it  will  be  around 

75km/h. With sequent snapping of the gas lever keep the airplane as long as possible only on 

the main undercarriage. The proe wheel will lay on the ground on itself with the speed around 

60km/h.  

Remark:  Shifting  especially  the  2

nd

  grade  flaps  at  slightly  lower  speed  than  is  the  maximum 

allowed speed for the 2nd grade speed expressively descent the power, which is necessary for 

this 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 still with the backup against the stalling speed / you will find out, that the effectiveness 
of the rudder is descending and you will have more work with keeping the direction. 

 

4.10.Tasks after landing 

rom the place of landing taxy to the place of parking 

urn off all appliances, respectively horizon 

urn off the main switch 

lose the fuel supply to the engine with the fuel tap 

eave the lifting flaps shifted off on 2

nd

 grade / this task seems to not be logical because 

we  shift  the  flaps  on  the  1

st

  grade  before  the  start,  but  its  purpose  is  to  restrain  the 

possibility of stepping of you own or your fellow-traveller while getting off the plane. The 

flap  is  fully  shifted  off  and  is  expressively    bended,  the  possibility  of  stepping  on  it  is 

smaller / 

fter the airscrew stops, lock off the overlap of the cabin, release the seat belts and lift 

off  the  cabin.  The  airplane  should  stand  against  the  wind  when  lifting  the  cabin.  The 

overlap of the cabin has pretty big size and rapid wind directing to the overlap from the 

back could damage the hung up of the overlap of the cabin 

while parking the airplane, the cabin must be closed so the side or back wind would not 

apply load in the hung up of the cabin 

ATTENTION!

  do  NOT  leave  aircraft  canopy  opened  againts  the  sun,  the  plexy  canopy   

will function as magnifying glass and will brun the top upholstary 

ATTENTION!

 Before leaving and locking the cabin lock and lock in the saving system 

 

 

 
 

 

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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