BRM BRISTELL ELSA Operation Instructions Manual Download

Page: 103 / 116

9-4

Date of Issue: 11/2017

Document No.:

ELSA-AOI-2-1-0-US

Revision: -

Maximum Takeoff Weight Limitation.
600 kg (1320 lb) limit for Light sport
aeroplanes.
Located on the instrument panel or
fuselage side.

Summary of Contents for BRISTELL ELSA

Page 1: ...O s r o LETECK 255 686 04 KUNOVICE CZECH REPUBLIC Phone 420 773 984 338 E mail info brmaero com www brmaero com Kit builder INSERT HERE A PHOTO OF THE AIRPLANE Sport Flying USA Services 500 Airport Rd...

Page 2: ...engine and Fiti 3LR 158 on ground adjustable propeller The Sections paragraphs to be updated at least Title page picture of the airplane builder s name Section 6 Weight and balance 7 12 Miscellaneous...

Page 3: ...ment No ELSA AOI 2 1 0 US Revision Registration N312LM Serial Number 312 2018 This airplane must be operated in compliance with information and limitations contained in herein This AOI must be availab...

Page 4: ...ii Date of Issue 11 2017 Document No ELSA AOI 2 1 0 US Revision INTENTIONALLY LEFT BLANK...

Page 5: ...0 1 Date of Issue 11 2017 Document No ELSA AOI 2 1 0 US Revision SECTION 0 0 Technical Information 0 1 Record of revisions 0 2 List of effective pages 0 3 Table of contents...

Page 6: ...manual except actual weighing data cockpit description and list of instruments and avionics must be recorded in the following table Revision No Affected Section Affected Pages Date of Issue Approved...

Page 7: ...1 2017 2 5 11 2017 0 0 1 11 2017 2 6 11 2017 0 2 11 2017 2 7 11 2017 0 3 11 2017 2 8 11 2017 0 4 11 2017 2 9 11 2017 0 5 11 2017 2 10 11 2017 0 6 11 2017 0 7 11 2017 0 8 11 2017 3 3 1 11 2017 1 1 1 11...

Page 8: ...2017 5 5 11 2017 5 6 11 2017 5 7 11 2017 5 8 11 2017 5 9 11 2017 4 4 1 11 2017 5 10 11 2017 4 2 11 2017 4 3 11 2017 4 4 11 2017 4 5 11 2017 4 6 11 2017 4 7 11 2017 6 6 1 11 2017 4 8 11 2017 6 2 11 20...

Page 9: ...17 6 13 11 2017 8 2 11 2017 6 14 11 2017 8 3 11 2017 6 15 11 2017 8 4 11 2017 6 16 11 2017 9 9 1 11 2017 9 2 11 2017 9 3 11 2017 7 7 1 11 2017 9 4 11 2017 7 2 11 2017 9 5 11 2017 7 3 11 2017 9 6 11 20...

Page 10: ...0 6 Date of Issue 11 2017 Document No ELSA AOI 2 1 0 US Revision INTENTIONALLY LEFT BLANK...

Page 11: ...Section TECHNICAL INFORMATION 0 GENERAL INFORMATION 1 OPERATING LIMITATIONS 2 EMERGENCY PROCEDURES 3 NORMAL PROCEDURES 4 PERFORMANCE 5 WEIGHT AND BALANCE 6 AIRPLANE AND SYSTEMS DESCRIPTION 7 AIRPLANE...

Page 12: ...0 8 Date of Issue 11 2017 Document No ELSA AOI 2 1 0 US Revision INTENTIONALLY LEFT BLANK...

Page 13: ...eneral Information 1 1 Introduction 1 1 1 Certification 1 2 Warnings cautions and notes 1 3 Descriptive data 1 3 1 Aircraft description 1 3 2 Power plant 1 3 3 Aircraft dimensions 1 3 4 Aircraft layou...

Page 14: ...te the aircraft with respect to the procedures and limitations provided in this manual It is the owner s operator s responsibility to have the aeroplane registered and insured according to country spe...

Page 15: ...that the non observation of the corresponding procedure leads to an immediate or important degradation of the flight safety i e to injury or death of persons CAUTION Means that the non observation of...

Page 16: ...The standard power plant is composed of ROTAX 912 ULS 98 6 hp 4 cylinder 4 stroke engine and FITI three blade ground adjustable propeller BRISTELL ELSA S N 312 2018 is fitted with Rotax 912 ULS 2 FIT...

Page 17: ...1 5 Date of Issue 11 2017 Document No ELSA AOI 2 1 0 US Revision 1 3 4 Aircraft layout...

Page 18: ...cation transmitter EFIS Electronic Flight Instrument System ELT Emergency Locator Transmitter EMS Engine Monitoring System ft foot feet ft min feet per minute GPS Global Positioning System hp power un...

Page 19: ...d per square inch pressure unit rpm revolutions per minute sec second US gal volume unit VA maneuvering airspeed VFE maximum flap extended speed VFR Visual Flight Rules VMC Visual Meteorological Condi...

Page 20: ...Vy 920 fpm at 133 km h IAS 840 fpm at 65 KIAS 920 fpm at 72 KIAS Stall speed VS1 flaps retracted 83 km h CAS 45 KCAS Stall speed VS0 flaps fully extended 71 km h CAS 38 KCAS Total fuel capacity 120 li...

Page 21: ...rspeed indicator markings 2 4 Power plant 2 4 1 Engine operating speeds and limits 2 4 2 Fuel 2 4 3 Oil 2 4 4 Coolant 2 5 Power plant instrument markings 2 6 Miscellaneous Instrument Marking 2 7 Weigh...

Page 22: ...rational significance are shown below Speed IAS km h KIAS Remarks VNE Never exceed speed 290 157 Do not exceed this speed in any operation VNO Max structural cruising speed 240 129 Do not exceed this...

Page 23: ...their color code significance are shown below Marking IAS value or range Significance km h Knots White arc 71 139 38 75 Flap Operating Range Green arc 83 240 45 129 Normal Operating Range Yellow arc 2...

Page 24: ...ines S N without Suffix 01 Minimum 50 C 122 F Maximum 135 C 275 F conventional coolant permanent monitoring of coolant temperature and CHT is necessary Waterless coolant permanent monitoring of CHT is...

Page 25: ...2 5 Date of Issue 11 2017 Document No ELSA AOI 2 1 0 US Revision 2 4 2 Fuel Fuel volume Wing fuel tank volume 2x60 l 2x16 US gal Unusable fuel quantity 2x0 5 l 2x0 13 US gal...

Page 26: ...ssue 11 2017 Document No ELSA AOI 2 1 0 US Revision 2 4 3 Oil NOTE Type of oil used by aircraft manufacturer is shown in Section 10 Supplement No 2 Oil volume Minimum 3 2 l 0 856 US gal Maximum 3 6 l...

Page 27: ...f Issue 11 2017 Document No ELSA AOI 2 1 0 US Revision 2 4 4 Coolant NOTE Type of coolant used by aircraft manufacturer is shown in Section 10 Supplement No 2 Coolant liquid volume It is about 2 5 l 0...

Page 28: ...ion Range yellow arc Maximum Range red line Engine speed RPM 1400 1400 5500 5500 5800 5800 Oil Temperature 50 C 122 F 50 110 C 122 230 F 110 130 C 230 266 F 130 C 266 F Exhaust Gases Temp EGT 800 850...

Page 29: ...lb Maximum baggage weight Baggage compartment behind seats 15 kg 33 lb Wing lockers optional 20 kg 44 lb each Front locker optional 10 kg 22 lb 2 8 Center of gravity Operating C G range 25 to 35 of M...

Page 30: ...tted Day VFR flights Night VFR flights and IFR flights under VMC are permitted if the aeroplane is appropriately equipped e g FAR 91 205 and when the pilot has appropriate rating WARNING IFR flights u...

Page 31: ...4 3 Fire during take off 3 4 4 Fire in flight 3 4 5 Fire in the cockpit 3 5 Glide 3 5 1 Emergency descent 3 6 Landing Emergencies 3 6 1 Emergency landing 3 6 2 Precautionary landing 3 6 3 Landing wit...

Page 32: ...3 2 Date of Issue 11 2017 Document No ELSA AOI 2 1 0 US Revision 3 8 7 Overvoltage 3 8 8 Inadvertent icing encounter 3 8 9 Loss of primary instruments 3 8 10 Loss of flight controls...

Page 33: ...is section should be considered and applied as necessary to correct the problem 3 2 Engine Failure 3 2 1 Engine failure during take off run 1 Throttle reduce to idle 2 Ignition switch off 3 Apply brak...

Page 34: ...ke off direction over 150 ft choose a landing area 4 Wind find direction and velocity 5 Landing area choose free area without obstacles 6 Flaps extend as needed 7 Fuel Selector shut off 8 Ignition swi...

Page 35: ...ot do it 3 4 2 Fire on ground with engine running 1 Heating close 2 Fuel selector close 3 Throttle full power 4 Ignition switch off 5 Leave the airplane 6 Extinguish fire by a fire extinguisher if ava...

Page 36: ...ose of area heading to the nearest airport or choose emergency landing area 7 Emergency landing perform according to 3 6 8 Leave the airplane 9 Extinguish fire by a fire extinguisher if available or c...

Page 37: ...exceed this speed except in smooth air and then only with caution VNE 157 KIAS 290 km h Do not exceed this speed in any operation Steep spiral dive with max 60 bank may be used however be carefull to...

Page 38: ...ying over the runway threshold and touch down at the very beginning of the chosen area 7 After stopping the airplane switch off all switches shut off the fuel selector lock the airplane and seek for a...

Page 39: ...ollable tendency of the airplane to enter into a spin provided the normal piloting techniques are used Unintentional spin recovery technique 1 Throttle idle 2 Lateral control ailerons neutralized 3 Ru...

Page 40: ...ower gradually up to cruise conditions after 1 2 minutes If you fail to recover the engine power land on the nearest airfield if possible or depending on the circumstances perform a precautionary land...

Page 41: ...ts is indicated by Low Volt warning lamp on the instrument panel or on EFIS display If the alternator fails then the instruments are supplied by onboard battery for a limited period of time around 30...

Page 42: ...conditions change altitude or turn back 3 Carb heat pull knob to ON 4 Cockpit heating pull knob to ON 5 Up Down knob pushed forward UP to defrost windshield 3 8 9 Loss of primary instruments If prima...

Page 43: ...vator control Engine power may be used to pitch up Before landing when the airplane will enter ground effect will be needed to apply a slight nose up pitch as the airplane enters ground effect Small s...

Page 44: ...3 14 Date of Issue 11 2017 Document No ELSA AOI 2 1 0 US Revision INTENTIONALLY LEFT BLANK...

Page 45: ...starting 4 4 3 Engine warm up Engine check 4 4 4 Taxiing 4 4 5 Before take off 4 4 6 Take off 4 4 7 Short field take off 4 4 8 Soft field take off 4 4 9 Climb 4 4 10 Cruise 4 4 11 Descent 4 4 12 Befo...

Page 46: ...es manual 4 3 Pre flight Inspection Carry out the pre flight inspection every day prior to the first flight or after airplane assembly Incomplete or careless inspection can cause an accident Carry out...

Page 47: ...4 3 Date of Issue 11 2017 Document No ELSA AOI 2 1 0 US Revision The manufacturer recommends carrying out the pre flight inspection as follows...

Page 48: ...f surface Engine mount and exhaust manifold condition Oil and coolant quantity check Visual inspection of the fuel and electrical system Fuel system draining Other actions according to the engine manu...

Page 49: ...take off to make sure you have sufficient fuel for the planned flight CAUTION In case of long term parking it is recommended to turn the engine several times Ignition LANE A B OFF by turning the prope...

Page 50: ...because returning fuel will overpressure left tank and fuel will leak from fuel tank air vent tube at the wing tip 4 Electric fuel pump ON only for cold engine 5 Choke cold engine pull to open and gr...

Page 51: ...magneto switched off should not over 300 rpm The Max engine speed drop difference between circuits A and B should be 115 rpm NOTE Only one ignition should be switched on off during ignition circuit c...

Page 52: ...e right tank if the left one is full because returning fuel will overpressure left tank and fuel will leak from fuel tank air vent tube at the wing tip 7 Ignition A B ON 8 Electric fuel pump ON 9 Wing...

Page 53: ...rpm increase 9 Accelerate and pull control stick aft to lift off the nose wheel as soon as possible 10 As aircraft becomes airborne level off in ground effect to accelerate to No obstacle Vy best rat...

Page 54: ...0 ft 4 4 9 Climb 1 Speed Best rate of climb speed Vy 72 KIAS 133 km h Best angle of climb speed Vx 60 KIAS 111 km h 2 Throttle Max take off power max 5800 rpm for 5 minutes Max cont power 5500 rpm 3 T...

Page 55: ...65 70 KIAS and check that the engine instruments indicate values within permitted limits 4 4 12 Before landing 1 Approach speed 120 km h 65 KIAS 2 Throttle as needed 3 Electric fuel pump s ON 4 Wing...

Page 56: ...ing light s ON 10 Flare minimum float 11 After touchdown stick forward Retract flaps Maximum braking 4 4 16 Soft field landing 1 Fuel selector select proper tank 2 Safety harness check that tightened...

Page 57: ...r switch switch off 7 Switch box turn key to switch off 8 El pump off 9 Fuel Selector off CAUTION Rapid engine cooling should be avoided during operation This happens above all during aircraft descent...

Page 58: ...r at low temperatures of ambient air do not use parking brake but use the wheel chocks instead NOTE Use anchor eyes on the wings and fuselage rear section to fix the airplane Move control stick forwar...

Page 59: ...1 Introduction 5 2 Performance 5 2 1 Airspeed indicator system calibration 5 2 2 Stall speeds 5 2 3 Take off performance 5 2 4 Landing distances 5 2 5 Climb performance 5 2 6 Cruise 5 2 7 Endurance a...

Page 60: ...formation The presented data has been computed from actual flight tests with the aircraft and engine in good conditions and using average piloting techniques If not stated otherwise the performance st...

Page 61: ...65 65 70 70 VFE 75 75 80 80 85 85 90 90 VA 96 96 100 100 105 105 110 109 115 114 120 119 125 124 VN0 130 129 135 134 140 139 145 144 150 149 VNE 157 156 IAS km h CAS km h 65 66 VS0 70 71 80 81 VS1 82...

Page 62: ...Conditions Wing IAS CAS KIAS KCAS Altitude loss Max takeoff off weight 600 kg flaps pos km h km h at recovery Engine idle run ft Wing level stall 0 82 83 44 45 100 20 78 79 42 43 120 30 70 71 37 38 16...

Page 63: ...istance over 50 ft obstacle ft Takeoff Run ft Distance over 50 ft obstacle ft 0 ft ISA 35 0 95 750 1720 1050 2010 2000 ft ISA 31 0 88 850 1930 1190 2270 4000 ft ISA 27 1 81 960 2180 1340 2560 6000 ft...

Page 64: ...t Distance over 50 ft obstacle ft Landing Run ft Distance over 50 ft obstacle ft 0 ft ISA 35 0 95 320 1020 390 1090 2000 ft ISA 31 0 88 340 1080 410 1160 4000 ft ISA 27 1 81 360 1150 430 1230 6000 ft...

Page 65: ...g speed Vy for best rate of climb Rate of climb Climbing speed Vx for best angle of climb Rate of climb IAS km h KIAS fpm IAS km h KIAS fpm 0 ft ISA 133 72 920 111 60 840 2000 ft ISA 130 70 810 109 59...

Page 66: ...100 knots 112 knots KIAS 74 knots 86 knots 91 knots 103 knots KCAS 76 knots 88 knots 92 knots 104 knots KTAS 81 knots 93 knots 98 knots 110 knots KIAS 69 knots 81 knots 86 knots 98 knots KCAS 71 knots...

Page 67: ...nots KCAS 76 knots 88 knots 92 knots 104 knots KTAS 81 knots 93 knots 98 knots 110 knots Fuel consumption 3 7 USgal h 4 9 USgal h 5 4 USgal h 6 6 USgal h Endurance 8 28 6 23 5 47 4 45 Range 680 NM 590...

Page 68: ...Max permitted head wind velocity for take off and landing 20 m s 40 knots Max permitted cross wind velocity for take off and landing Average pilots 8 m s 15 knots Skilled pilots 11 m s 22 knots 5 2 9...

Page 69: ...nd Balance Report 6 2 1 1 Empty Aircraft Weight and CG 6 2 1 2 Loaded Aircraft Weight and CG 6 2 1 3 Weight and CG Blank Form 6 3 Permitted payload range 6 4 Operational Weight and Balance Computation...

Page 70: ...This section contains the payload range within which the BRISTELL ELSA may be safely operated Procedures for weighing the aircraft and the calculation method for establishing the permitted payload ra...

Page 71: ...tinuous history of changes of equipment affecting weight and balance 312 2018 Basic weight of empty airplane Moment lb in Weight lb Weight change Removed Moment lb in Arm in Weight lb Added Moment lb...

Page 72: ...EFT MAIN WHEEL WL 310 LL 27 6 ML 8543 3 NOSE WHEEL WN 161 LN 29 7 MN 4779 3 CG in 15 83 WE 786 CG MAC 29 4 MT 12445 12 Serial No 312 2018 Date 0 1 1900 By 0 WEIGHT lb ARM in MOMENT WEIGHT x ARM lb in...

Page 73: ...UEL TANKS CENTER OF GRAVITY CG in TOW CG MAC MT Max Takeoff Weight 1320 0 lb Serial No 312 2018 CG Range 25 35 Date Forward limit 13 5 in By Rearward limit 18 8 in 15 83 12445 1 WEIGHT lb ARM in MOMEN...

Page 74: ...x Takeoff Weight 1320 lb Serial No 312 2018 CG Range 25 35 Date Forward limit 13 5 in By Rearward limit 18 8 in Max useful load WU lb MTOW WE WU lb 1320 WU lb WARNING DO NOT EXCEED MAXIMUM TAKEOFF WEI...

Page 75: ...MAC 35 0 MAC 34 7 MAC 34 1 MAC 33 4 MAC 32 5 MAC 460 429 399 369 339 298 34 7 MAC 34 0 MAC 33 3 MAC 32 7 MAC 32 0 MAC 31 1 MAC 382 413 383 352 322 282 35 0 MAC 34 7 MAC 34 1 MAC 33 4 MAC 32 7 MAC 31 8...

Page 76: ...crew fuel and baggage 4 Record found moments into the 6 4 1 Airplane Loading Schedule Chart 5 Determine Take off weight of the airplane add together the airplane empty weight crew fuel and baggage an...

Page 77: ...it is necessary to change weight of some of the useful load items crew fuel baggage so that after a repeated computation the intersection of Take off Weight and Total Static Moment will be inside the...

Page 78: ...3 inches Baggage Comp Limit 44 lb Gallons Weight x Arm Moment Basic Weight 772 14 90 11496 84 Pilot 210 23 60 4956 00 Front Passenger 180 23 60 4248 00 Wing Baggage 10 24 80 248 00 Aft Baggage 10 55 1...

Page 79: ...55 1 5 Baggage wing lockers 88 2 88 2 24 8 21 9 24 8 6 Baggage front locker 22 0 22 0 9 8 2 2 9 8 MTOW lb TAKEOFF WEIGHT lb TOTAL MOMENT 100 lb in TAKEOFF WEIGHT lb TOTAL MOMENT 100 lb in sum of weig...

Page 80: ...0 72 1 5 7 12 6 6 30 7 4 6 0 6 240 0 56 7 14 0 84 1 6 6 14 7 7 35 8 7 7 0 7 260 0 61 4 16 0 96 1 7 6 16 8 8 40 9 9 8 0 8 280 0 66 1 18 0 108 2 8 5 18 9 9 45 11 2 9 0 9 300 0 70 9 20 0 120 2 9 5 20 11...

Page 81: ...T 10 0 5 0 0 0 5 0 10 0 15 0 20 0 25 0 0 0 50 0 100 0 150 0 200 0 0 0 20 0 40 0 60 0 80 0 100 0 120 0 140 0 160 0 180 0 200 0 220 0 240 0 260 0 280 0 300 0 320 0 340 0 360 0 380 0 400 0 420 0 440 0 46...

Page 82: ...US Revision 6 4 4 CG Moment envelope SAMPLE AIRCRAFT 600 700 800 900 1000 1100 1200 1300 1400 100 110 120 130 140 150 160 170 180 190 200 210 220 230 240 250 260 LOADED AIRPLANE WEIGHT lb LOADED AIRPL...

Page 83: ...ent No ELSA AOI 2 1 0 US Revision 6 4 5 CG limits SAMPLE AIRCRAFT 600 700 800 900 1000 1100 1200 1300 1400 23 24 25 26 27 28 29 30 31 32 33 34 35 36 LOADED AIRPLANE WEIGHT lb LOADED AIRPLANE C G POSIT...

Page 84: ...r dual brakes 15 Cabin heat 16 Carbon instrument panel 17 Dark Grey interior 18 FFffiti 19 Elevator electric trim 20 ELT Kannad AF Integra 406 MHz 21 RAMI AV 525 VOR LOC GS V Dipole Antenna 22 Garmin...

Page 85: ...9 m with horn balance 50 Middle size instrument panel for G3X 51 Noise insulation on firewall 52 Nose gear doubled flexible rod Teleflex 53 Paint scheme 14 54 Parking brake 55 Pierburg auxiliary fuel...

Page 86: ...g gear 7 5 Seats and safety harness 7 6 Baggage compartment 7 7 Canopy 7 8 Power plant 7 8 1 Throttle 7 8 2 Heating 7 9 Fuel system 7 10 Electrical system 7 10 1 Battery 7 10 2 Master switch 7 10 3 Ig...

Page 87: ...uminium alloy construction provides long life and low maintenance costs thanks to its durability and corrosion resistance characteristics The wing has a high lift aerofoil equipped by fowler flaps con...

Page 88: ...e rear baggage compartment is located behind the seats It may accommodate up to 15 kg 33 lb This space is divide on two sections baggage compartment A and B Is not recommended give too heavy things in...

Page 89: ...er with composite blades NOTE For technical data refer to documentation supplied by the propeller manufacturer 7 8 1 Throttle Engine power is controlled by means of the THROTTLE lever THROTTLE lever i...

Page 90: ...with a vent outlet and screen filter Drain valve located in the lowest point of the each tank and on the bottom edge of the firewall on the gascolator Main fuel selector valve is on the central conso...

Page 91: ...the engine For safety remove key when engine is not running NOTE All switches and or engine controls are up or push forward for operation except the choke cabin heat and carburetor pre heat which is...

Page 92: ...rakes park brake brake limiter 11 Cabin heat 12 Carbon instrument panel 13 Key switch box 14 Lambert LINAK electric flaps actuator 15 Landing lights in both wings WIG WAG 16 Leather glareshield Leathe...

Page 93: ...mperature Probe TCW IBBS 12V 3AH backup battery for Garmin G3X Engine instruments 1 Garmin G3X flight display system including 2 Garmin GEA 24 Engine Interface Module COM NAV 1 GARMIN GNC 255 NAV COM...

Page 94: ...7 9 Date of Issue 11 2017 Document No ELSA AOI 2 1 0 US Revision 7 14 Cockpit 7 14 1 Cockpit layout BRISTELL ELSA S N 312 2018 has the following cockpit layout INSERT HERE A TOP VIEW OF THE COCKPIT...

Page 95: ...e of Issue 11 2017 Document No ELSA AOI 2 1 0 US Revision 7 14 2 Instrument panel BRISTELL ELSA S N 312 2018 has the following instrument panel arrangement INSERT HERE A VIEW ON THE AIRPLANE INSTRUMEN...

Page 96: ...on SECTION 8 8 Airplane handling servicing and maintenance 8 1 Introduction 8 2 Aircraft inspection periods 8 3 Aircraft alterations or repairs 8 4 Ground handling 8 4 1 Towing 8 4 2 Parking 8 4 3 Moo...

Page 97: ...for engine maintenance Maintain the prop according to its manual All repairs and maintenance should be made in accordance with AC 43 13 1B 8 3 Aircraft alterations or repairs It is recommended to con...

Page 98: ...ing procedure 1 Check Fuel Selector shut off Circuit breakers and Master switch switched off Switch box switched off 2 Fix the hand control using e g safety harness 3 Close air vent 4 Close and lock c...

Page 99: ...and care Use efficient cleaning detergents to clean the aircraft surface Oil spots on the aircraft surface except the canopy may be cleaned with gasoline The canopy may only be cleaned by washing it...

Page 100: ...9 1 Date of Issue 11 2017 Document No ELSA AOI 2 1 0 US Revision SECTION 9 9 REQUIRED PLACARDS AND MARKINGS 9 1 Limitation placards 9 2 Miscellaneous placards and markings...

Page 101: ...Tail heavy Flaps 0 10 20 30 Maximum rear baggage weight 15 kg 33 lb Maximum weight in each wing locker 20 kg 44 lb if installed Maximum weight in front locker 10 kg 22 lb if installed Instruments Cano...

Page 102: ...on the instrument panel Main baggage compartment behind the seats Additional baggage compartment behind the Baggage compartment A NOT TO BE USED FOR HEAVY ITEMS Maximum weight of baggage in the Bagga...

Page 103: ...9 4 Date of Issue 11 2017 Document No ELSA AOI 2 1 0 US Revision Maximum Takeoff Weight Limitation 600 kg 1320 lb limit for Light sport aeroplanes Located on the instrument panel or fuselage side...

Page 104: ...skin around the fuel tank filler neck Throttle and Choke placard located on the Throttle choke quadrant Located on the fuselage right left side under the instrument panel Placard point to the lever to...

Page 105: ...RS rescue system is installed Placard located on the both sides of fuselage between canopy and rear window Placard located in place rocket egress Located on both sides of the fuselage tail where are l...

Page 106: ...10 1 Date of Issue 11 2017 Document No ELSA AOI 2 1 0 US Revision SECTION 10 10 SUPPLEMENTS 10 1 Introduction 10 2 List of inserted supplements 10 3 Inserted Supplements...

Page 107: ...AOI 2 1 0 US Revision 10 1 Introduction This section contains the appropriate supplements necessary to safely and efficiently operate the aircraft when equipped with various optional systems and equip...

Page 108: ...017 Document No ELSA AOI 2 1 0 US Revision 10 2 List of inserted supplements Date Suppl No Title of inserted supplement 07 2011 01 2011 Aircraft Flight Training Supplement 11 2017 02 Description of th...

Page 109: ...10 4 Date of Issue 11 2017 Document No ELSA AOI 2 1 0 US Revision 10 3 Inserted Supplements...

Page 110: ...ilot is ready to continue on in next training step Training can be performed by Flight Instructor or by the experienced pilot who has minimum 20 hours on the BRISTELL LSA Type Rating Training Procedur...

Page 111: ...ning Procedure Dual Solo Flights hr min Flights hr min 1 Check flight 1 30 2 Pattern training flights up to 1000 ft AGL 4 20 3 15 3 Pattern training flights up to 500 ft AGL 4 20 3 15 4 Stall speed 45...

Page 112: ...raining flights up to 500 feet AGL high pattern procedures instructor is giving advice as necessary 4 Stall speed 45 turns sideslips stall speed flaps retracted and extended landing configuration side...

Page 113: ......

Page 114: ...in the Aircraft Operating Instructions during operation of the airplane Information contained in this Supplement add or replace information from the basic Aircraft Operating Instructions in the furthe...

Page 115: ...1 GENERAL INFORMATION No changes 2 OPERATING LIMITATION 2 4 3 Oil Type of oil Aircraft Manufacturer uses Aeroshell OIL SPORT PLUS 4 2 4 4 Coolant Type of coolant Dexcool 50 50 Type of coolant used by...

Page 116: ...11 2017 Revision 5 PERFORMANCE No changes 6 WEIGHT AND BALANCE No changes 7 AIRPLANE AND SYSTEMS DESCRIPTION No changes 8 AIRPLANE HANDLING SERVICING AND MAINTENANCE No changes 9 REQUIRED PLACARDS AND...

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