TL Ultralight TL-96 STAR Flight And Operational Manual Download Page 17

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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2.7.Maximum flight height 

From technical view the airplane is able to rise into such height, when it is permanently able to 

be rising with the speed of 0.5m/s at the speed of flight 130km/h / practical ceiling/. Factually 

this  technical  ability  depends  on  actual  weight  of  the  airplane,  conditions  of  engine,  the 

airscrew output, meteorological conditions and etc.  

In the way of legislative, the height of the flight is influenced by many restrictions which can  

change in course of time. Meantime, these restrictions are introduced for example in the rule 

UL1,  head  2.,  point  2.7.  make  sure  you  get  to  know  these  conditions  in  its  full  length.  We 

roughly introduce for orientation, these restrictive conditions: 

-with ULLa it is possible to fly only at conditions VFR during the day, and only to the flight level 
f FL 205, it means 6.250m MSL 

-within its borders of the height limit FL 205 it is necessary to respect the conditions laying the 

flight in single forms of the aerial area / flying schedule, radiolink, responder.../ 

 

 

2.8.Meteorologic condition restriction 

Operating  the  airplane  is  restricted  on  meteorological  conditions  and  also  on  constitution  of 

valid  rules  for  the  performance  of  the  flight  /keeping  the  meteorological  minimums  and  the 

rules of flights in single forms of the aerial area – see the rule LAA ČR UL1 /, also technical 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 side component of wind                                3m/s 

Maximum speed of the wind in the direction of taking off           1m/s 

 

Operating restrictions of the airplane in the way of meteorological conditions in cooler weather 

are determinated mostly by the possibility of ice formation. Keep away from flight in conditions 

which increase the probability of its formation.  

 

 2.9. Carriage of baggage restriction  

Transport of load is restricted by the valid rules and also by the technical possibility. 

Valid  flying  rules  prohibit  the  transport  of  some  kinds  of  loads,  for  example  weapons, 

explosives, volatile and caustic agents and etc.  

In the way of technical possibility the airplane is able for transportation in its cabin only at these 
conditions: 

-maximum weight of the airplane can not be overpassed 

-the  load  can  be  transferred  only  if  it  does  not  influence  controllability  of  the  pilot,  the 

movement and the view of the pilot in any way, also the load must be mounted to the seat 

-small sized things can be conveyed in side pockets of padding 

-at the put off area in the back under the overlap of the cabin behind the seats there can be 

conveyed only such things, when the center of gravity will be ensured. At the same time, the 

load must be kept the way not to terminate the pilot´s view and controllability even in worse 

flying conditions / for example flying into the turbulence / 

 

2.10.Types of airport traffic 

Flying rule and the equipment of the airplane terminate the operating with the airplane only for 

flights under the conditions VFR during the day. Other flights are strictly prohibited. 
 

 

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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