TL Ultralight TL-3000 Sirius Flight And Operational Manual Download Page 31 | Manualshive

Page: 31 / 64

background image

Flight

and

operational

manual

TL

3000

SIRIUS

Page

30

6.

Tail

‐

plane:

Surface

inspection

Attachment

inspection

Tailplane

and

rudder

swivel

pins

clearance

inspection

controls

inspection

7.

Airframe

left

hand

side:

The

same

as

for

the

airframe

right

hand

side.

8.

Left

wing:

The

same

as

for

the

right

wing

Pitot

tube

–

cleanliness

of

the

openings

9.

Cabin:

Ignition

–

switched

off

Main

switch

–

switched

on

Instruments

inspection

Steering

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

procedures

and

action

list

4.3.1.

Cockpit

post

‐

boarding

actions

1.

Foot

controls

clearance

inspection

2.

Hand

controls

clearance

inspection

3.

Balancing

freedom

of

action

4.

Gas

lever

freedom

of

action

5.

Fuel

tap

closed

6.

Fuel

level

indicators

fuel

level

check

7.

Instruments

status

inspection

8.

Ignition

switched

off

9.

Main

switch

switched

off

10.

Other

switches

switched

off

11.

Activation

handle

check

12.

Activation

handle

fuse

remove

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Summary of Contents for TL-3000 Sirius

Page 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...

Page 2: ......

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

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