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TL Ultralight TL-3000 Sirius, Руководство по эксплуатации и полетам


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Flight

 

and

 

operational

 

manual

 

TL

 

3000

 

SIRIUS

  

 

                                                                                                    

Page

  

44

                         

 

 

 

Section

 

7

 

Aircraft

 

and

 

aircraft

 

systems

 

description

 

 

 

 
 

 

7.1

 

Introduction

45

 

7.2

 

Airframe

 

45

 

7.2.1

 

Fuselage

 

45

 

7.2.2

 

Wing

 

45

 

7.2.3

 

Horizontal

 

tail

 

plane

 

(VOP)

 

45

 

7.2.4

 

Vertical

 

tail

 

plane

 

(SOP)

 

45

 

7.3

 

Cockpit

 

controls

 

–

 

instrument

 

board

 

46

 

7.4

 

Undercarriage

 

47

 

7.5

 

Steering

 

47

 

7.6

 

Seats

 

and

 

safety

 

belts

 

48

 

7.7

 

Luggage

 

compartment

 

48

 

7.8

 

Cockpit

 

door

 

48

 

7.9

 

Power

 

plant

 

48

 

7.10

 

Fuel

 

system

 

48

 

7.11

 

Electrical

 

system

 

49

 

7.12

 

Pitot

 ‐ 

static

 

system

 

49

 

7.13

 

Rescue

 

system

 

49

 

 

 
 
 
 
 
 
 
 
 
 

Содержание TL-3000 Sirius

Страница 1: ...type Flight and operational manual Registration T L 3 0 0 0 S I R I U S TL Ultralight s r o Airport building 84 503 41 Hradec Kralove Czech Republic Tel 420 495 211 753 420 495 218 910 Tel Fax 420 49...

Страница 2: ......

Страница 3: ...Flight and operational manual TL 3000 SIRIUS Page 2 0 List of changes Change amendment serial number Bulletin number Changed pages New page release or change date Execution date and signature...

Страница 4: ...rational limitations 11 21 Section 3 Emergency procedures 22 26 Section 4 Normal procedures 28 34 Section 5 Performances 36 39 Section 6 Weight and gravity centre position 41 43 Section 7 Aircraft and...

Страница 5: ...nual TL 3000 SIRIUS Page 4 Section 1 General information 1 1 Introduction 5 1 2 Certification attest 6 1 3 Abbreviations and definitions 7 1 4 Warnings notifications and notes 8 1 5 Technical data 8 1...

Страница 6: ...al manual is divided by topics into several sections that are split into paragraphs according to the significance and importance of their subject matter In case of page replacement amendment or handwr...

Страница 7: ...tification attest This aircraft has been approved by the Amateur Light Aircraft Association of the Czech Republic in accordance with the regulation Ultralight Aircraft Airworthiness Requirements The t...

Страница 8: ...meter system error o 1 2 o air specific weight at the see level air specific gravity at given altitude ISA International standard atmosphere MAC Mean aerodynamic chord VNE Maximum never exceed speed V...

Страница 9: ...ut a special point that is not directly related to the flight safety but is important or unusual 1 5 Technical data TL 3000 Sirius ultra light aircraft is a two seat classical design high wing monopla...

Страница 10: ...tyres 2 0 kPa Nose wheel rebound Coil spring Main undercarriage rebound Tyres undercarriage leg resilience Brakes Hydraulic disc brakes Fuel tank volume 130 litres Empty aircraft weight kg Wing mean a...

Страница 11: ...Flight and operational manual TL 3000 SIRIUS Page 10 1 6 Three view drawing...

Страница 12: ...12 2 3 Speed indicator 13 2 4 Power plant 13 2 5 Power plant instruments markings 15 2 6 Other instruments markings 16 2 7 Weight 16 2 8 Centre of gravity position 17 2 9 Approved manoeuvres 19 2 10 F...

Страница 13: ...o not exceed this speed in any flight regime VH Maximum speed of horizontal flight at max steady engine power 226 Engine RPM 5400 per min VOPT Optimal cruising speed 178 Engine RPM 4500 per min VA Des...

Страница 14: ...formed with caution and only in a calm atmosphere Radial red line 230 Maximum speed in all flight phases 2 4 Power plant Engine manufacturer BOMBARDIER Rotax GmbH Austria Engine model Rotax 912UL Rota...

Страница 15: ...ating maximum 0 15 0 4 bar 2 2 5 8 psi 0 4 bar 5 8 psi Fuel European norm EN 228 super min 90 octanes EN 228 super min 95 oct Oil According to API SG or higher Castrol GTX 3 Minimum engine starting te...

Страница 16: ...0 5800 Fuel pressure 0 0 7 0 7 2 5 2 5 5 8 5 8 6 5 6 5 7 3 Filling pressure INHG 0 31 31 32 32 33 3 Oil pressure PSI 0 15 15 20 20 90 90 95 95 99 Oil temperature C 0 50 50 90 90 110 110 140 Cylinder t...

Страница 17: ...ent markings Fuel level indicator Minimum start fuel volume 10 litres Inexhaustible volume 2x1 litres 2 7 Weight Maximum take off weight 472 5 kg Maximum fuel weight 93 5 kg Maximum one seat load 90 k...

Страница 18: ...fuel on the graduated scale 2 Sum up so determined increments and add them to the empty aircraft centring 3 The total gives the aircraft centre of gravity position at the chosen payload of each item...

Страница 19: ...Flight and operational manual TL 3000 SIRIUS Page 18...

Страница 20: ...alling over the horizon and sharp turns up to6O tilt WARNING This aircraft category is allowed only for non acrobatic operations Intended spins and drops are forbidden 2 10 Flight multiples 2 11 Crew...

Страница 21: ...nstruments manometer thermometer tachometer a fuel level indicator for each fuel tank 2 13 Fuel This aircraft is equipped with 2 fuel tanks one tank in each wing Each fuel tank volume is 65 litres The...

Страница 22: ...Flight and operational manual TL 3000 SIRIUS Page 21...

Страница 23: ...tion 3 Emergency procedures 3 1 Introduction 23 3 2 Engine failure 23 3 3 In flight engine restart 24 3 4 Engine on fire smoke in the cabin 24 3 5 Descending flight 25 3 6 Emergency landing 25 3 7 Uni...

Страница 24: ...e run 2 Brake intensively 3 Ignition switch off 3 2 2 Engine failure during the flight at the altitude up to 200m 1 Speed glide at the speed of 120 km h 2 Altitude up to 50 m land in the take off dire...

Страница 25: ...gine on fire smoke in the cabin 3 4 1 A fire on the ground with the engine running 1 Fuel tap close 2 Gas lever full throttle 3 Ignition 2x switch off 4 Main switch switched off 5 Leave the aircraft a...

Страница 26: ...arriage leg failure land on the undamaged leg side hold the aircraft on this side above the ground as long as possible by using the elevators 2 In case of nose gear damage hold the fuselage front elev...

Страница 27: ...with the lowest vibration level 2 Landing at the closest airfield or emergency landing according to paragraph 3 6 1 3 8 3 Carburettor icing 1 Airspeed 140 km h 2 Gas lever set to of the throttle 3 Ic...

Страница 28: ...list 30 4 3 1 Cockpit post boarding actions 30 4 3 2 Pre start actions and starting up 31 4 3 3 Engine test 31 4 3 4 Taxiing 32 4 3 5 Pre takeoff actions 32 4 3 6 Take off 32 4 3 7 Climb 32 4 3 8 En r...

Страница 29: ...that nothing is omitted It is recommended to conduct inspection as shown in the picture and further according to the procedure hereunder The inspection starts with the engine and continues clockwise...

Страница 30: ...both ignition circuits and main switch are switched off 3 Undercarriage Dismounting the aerodynamic cover lower part and nose gear inspection Inspection of the main undercarriage wheels self fusing nu...

Страница 31: ...ing correct function and clearance inspection Mutual flaps lifting inspection Cleanliness inspection Remove or fix the loose objects Safety belts inspection Door and locking inspection 4 3 Normal proc...

Страница 32: ...r check clearance 8 Starter push 9 After start up idle run 10 Other instruments switch on 11 Choke push in 12 Engine heating see paragraph 4 3 3 Caution Continue starting during maximum 10 sec cool do...

Страница 33: ...4 3 5 Pre takeoff actions 1 Brakes brake 2 Balancing on the centre 3 Flaps Level 1 10 5 4 Instruments at operating values 5 Safety belts buckled and fastened 4 3 6 Take off 1 Brakes release 2 Gas lev...

Страница 34: ...2 Balancing equilibrate 3 Airspeed 150 km h 4 Instruments at the operating values CAUTION To prevent engine overcooling when descending from higher flight levels do not decrease to idle run but descen...

Страница 35: ...s possible The nose wheel will ground by itself at the speed of 60 km hour 4 3 12 Repeated landing 1 Gas lever full throttle 2 Flaps grade 1 10 5 3 Balancing equilibrate 4 Airspeed 130 km h 5 Flaps re...

Страница 36: ...mances 5 1 Introduction 36 5 2 Specified data 36 5 2 1 Airspeed indication system error correction 36 5 2 2 Stall speed 37 5 2 3 Take off 37 5 2 4 Landing 37 5 2 5 Climb 38 5 2 6 Cruising flight 38 5...

Страница 37: ...otherwise the performances presented in this section are valid for the aircraft maximum take off weight and calculated for the conditions of the International Standard Atmosphere ISA 5 2 Specified val...

Страница 38: ...n be resumed without a significant altitude loss 5 2 3 Take off Take off run distance m Take off distance over a 15 metre obstacle m Grass 103 283 NOTE The take off distance stated in the table above...

Страница 39: ...mum permanen Maximum Take off Time limitation unlimited unlimited 5 minutes max Engine rotations 4500 5500 5800 Flight altitude ft IAS km h IAS km h IAS km h 2000 178 22 227 4000 181 22 228 5000 180 2...

Страница 40: ...Flight and operational manual TL 3000 SIRIUS Page 39 5 2 8 Wind effect during the take off and landing Headwind 10 m s Crosswind 5 5 m s Tailwind 2 m s...

Страница 41: ...raft weight and centre of gravity position 6 1 Introduction 41 6 2 Centre of gravity positioning allowed range and maximum take off weight 41 6 3 Empty aircraft centre of gravity determination 41 6 4...

Страница 42: ...safe aircraft operating 6 2 Centre of gravity positioning permitted range and maximum take off weight Aircraft maximum take off weight kg 472 5 Centre of gravity positioning permitted range MAC 22 32...

Страница 43: ...ed by the scale 3 Read the GP and GH values from the scales GH represents the sum of the values indicated by the scales under the wheels 4 Calculate the total empty aircraft weight by using the follow...

Страница 44: ...PAL fuel weight and GZAV luggage weight in the luggage compartment 2 Calculate the empty aircraft centre of gravity for the required configuration by inserting the values derived from the step 1 a 2 i...

Страница 45: ...45 7 2 2 Wing 45 7 2 3 Horizontal tail plane VOP 45 7 2 4 Vertical tail plane SOP 45 7 3 Cockpit controls instrument board 46 7 4 Undercarriage 47 7 5 Steering 47 7 6 Seats and safety belts 48 7 7 Lu...

Страница 46: ...e engine wall The luggage compartment is located behind the pilot seats 7 2 2 Wing The wing is all composite with a single strut consisting of a metal tube and composite coating It is designed as a tw...

Страница 47: ...Flight and operational manual TL 3000 SIRIUS Page 46 7 3 Cockpit controls instrument board...

Страница 48: ...Undercarriage The undercarriage is a nose type with main wheels laminate legs and a spring loaded nose wheel The nose gear is towed and unsteerable The main undercarriage wheels are equipped with brak...

Страница 49: ...y gas operated springs 7 9 Power plant The aircraft is powered with Rotax 912 ULS engine It is a four cylinder four stroke opposite cylinders engine with a central camshaft and OHV distribution Coolin...

Страница 50: ...th the GRS 6 473 rescue system allowing saving the crew up to the speed of 310 km h at the minimum altitude of 80 m above the ground The rescue system consists of the projectile parachute activation h...

Страница 51: ...ating servicing and maintenance 8 1 Introduction 51 8 2 Periodical inspection 51 8 3 Airframe service life 53 8 4 Aircraft modifications and repairs 53 8 5 Aircraft ground servicing 55 8 6 Aircraft gr...

Страница 52: ...ing The guarantee inspection and inspections after 100 300 and 1000 hours are recorded in the aircraft log 8 2 1 Aircraft periodical inspections This paragraph describes the inspection and maintenance...

Страница 53: ...al aircraft service life a every 1000 10 hours of service b 5 years from the production date c 5 years after the last 1000 hour inspection d the date determined by the manufacturer according to his ex...

Страница 54: ...ion as well as the LAA CR before each significant modification or repair influencing airworthiness CAUTION If the modification influences the weight it is necessary to perform a new weighing and empty...

Страница 55: ...ngs struts empennage and fuselage are considered to be the parts of the principal structural elements No intervention in the principal structural elements is allowed by the user without manufacturer s...

Страница 56: ...sult in its damage CAUTION When refuelling use only the containers and filter fillers approved for fuel storing and filling do not use static electricity generating clothes Prevent open fire occurrenc...

Страница 57: ...TION In case of parking outside a hangar it is necessary to anchor the aircraft according to paragraph 8 5 3 in order to protect it against possible wind blast damage 8 5 3 Anchorage It is necessary t...

Страница 58: ...ead area and pushing upwards The rear fuselage portion can be then supported in the rear luggage compartment bulkhead CAUTION When lifting the fuselage rear portion do not push the fuselage pivot poin...

Страница 59: ...sembly do not require a special qualification NOTE After cleaning off the grease all connecting points must be again greased with grease 8 6 2 1 Aircraft disassembly procedure Remove the centroplane i...

Страница 60: ...an To lubricate the engine use only an engine manufacturer prescribed oil according to the engine operating instructions The motor oil exchange frequency is every 100 flight hour For the other lubrica...

Страница 61: ...rst conservation approximately 1 month to let the new painting harden properly Propeller blades and cone Wings and empennage Wing struts Undercarriage Engine cowling suction slots fuselage 8 8 2 Aircr...

Страница 62: ...Flight and operational manual TL 3000 SIRIUS Page 61 Section 9 Amendments 9 1 Introduction 62 9 2 Inserted amendments list 62 9 3 Inserted amendments 63...

Страница 63: ...ntains the amendments necessary for safe and effective the aircraft operating and for the cases of aircraft equipping with different optional systems and equipment not provided within the standard air...

Страница 64: ...Flight and operational manual TL 3000 SIRIUS Page 63 9 3 Inserted amendments...

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