BRISTELL S-LSA Operating Instructions Manual
  1. Manuals
  2. Brands
  3. BRISTELL Manuals
  4. Aircrafts
  5. S-LSA
  6. Operating instructions manual

BRISTELL S-LSA Operating Instructions Manual

Hide thumbs Also See for S-LSA:
Table of Contents

Advertisement

Quick Links

BRM AERO, s.r.o.
LETECKÁ 255
686 04 KUNOVICE
CZECH REPUBLIC
Phone: +420 773 984 338
E-mail:
info@brmaero.com
www.brmaero.com

Advertisement

Table of Contents
loading

Related Manuals for BRISTELL S-LSA

Summary of Contents for BRISTELL S-LSA

  • Page 1 BRM AERO, s.r.o. LETECKÁ 255 686 04 KUNOVICE CZECH REPUBLIC Phone: +420 773 984 338 E-mail: info@brmaero.com www.brmaero.com...
  • Page 3 Registration: CC-AUV Serial Number: 317/2018 This airplane must be operated in compliance with information and limitations contained in herein. This AOI must be available on board of the airplane. Date of Issue: 09/2017 Revision: 1 Document No.: LSA-AOI-2-1-0-CL...
  • Page 4 INTENTIONALLY LEFT BLANK Date of Issue: 09/2017 Revision: 1 Document No.: LSA-AOI-2-1-0-CL...
  • Page 5 SECTION 0 Technical Information Record of revisions List of effective pages Table of contents Date of Issue: 09/2017 Revision: 1 Document No.: LSA-AOI-2-1-0-CL...
  • Page 6 Record of revisions Any revision of the present manual (except actual weighing data, cockpit description and list of instruments and avionics) must be recorded in the following table. Date of Date of Date Affected Pages Approved by Sign. Issue approval inserted P.Javorský...
  • Page 7 List of effective pages Section Page Date of Issue Section Page Date of Issue Title 01/2016 09/2017 page 09/2017 01/2016 09/2017 01/2016 09/2017 01/2016 09/2017 01/2016 09/2017 01/2016 09/2017 01/2016 09/2017 01/2016 09/2017 09/2017 01/2016 3-10 01/2016 01/2016 01/2016 01/2016 01/2016 01/2016 01/2016...
  • Page 8 Section Page Date of Issue Section Page Date of Issue 01/2016 09/2017 01/2016 01/2016 09/2017 01/2016 09/2017 09/2017 09/2017 7-10 09/2017 09/2017 09/2017 09/2017 01/2016 09/2017 09/2017 5-10 09/2017 09/2017 09/2017 01/2016 01/2016 01/2016 01/2016 01/2016 09/2017 01/2016 09/2017 01/2016 09/2017 01/2016 09/2017...
  • Page 9 Table of contents 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 HANDLING,SERVICING AND MAINTENANCE ..8 REQUIRED PLACARDS AND MARKINGS .......
  • Page 10 INTENTIONALLY LEFT BLANK Date of Issue: 09/2017 Revision: 1 Document No.: LSA-AOI-2-1-0-CL...
  • Page 11 SECTION 1 General Information Introduction Certification basis Warnings, cautions and notes Descriptive data Aircraft description Power plant Aircraft dimensions Aircraft layout Definitions and abbreviations Date of Issue: 01/2016 Revision: - Document No.: LSA-AOI-2-1-0-CL...
  • Page 12 Introduction This Aircraft Operating Instruction has been prepared to provide pilots with information for the safe and efficient operation of BRISTELL S-LSA aircraft. It also contains supplemental data supplied by the Aircraft Flight Training Supplement. Certification basis BRISTELL S-LSA is a special light sport category aircraft made by BRM Aero, s.r.o., Uherske Hradiste, Czech Republic,...

  • Page 13: Descriptive Data

    Descriptive data Aircraft description BRISTELL S-LSA is airplane intended especially for recreational and cross- country flying, basic training, and non-aerobatics operation. BRISTELL S-LSA is a single-engine, all metal, low-wing monoplane of semi-monocoque construction with two side-by-side seats. The airplane is equipped with a fixed tricycle undercarriage with steerable nose wheel.
  • Page 14 Aircraft layout Date of Issue: 01/2016 Revision: - Document No.: LSA-AOI-2-1-0-CL...

  • Page 15: Definitions And Abbreviations

    Definitions and abbreviations °F temperature in degree of Fahrenheit Aircraft Operating Instructions Airspeed Indicator Air Traffic Control BEACON anti-collision beacon Calibrated Airspeed Center of Gravity COMM communication transmitter EFIS Electronic Flight Instrument System Emergency Locator Transmitter Engine Monitoring System foot / feet ft/min feet per minute Global Positioning System...
  • Page 16 Nautical Mile Outside Air Temperature system is switched off or control element is in off-position system is switched on or control element is in on-position Pilot Operating Handbook pound per square inch - pressure unit Raet-of-climb revolutions per minute sec. second US gal volume unit...
  • Page 17 SECTION 2 Operating Limitation Introduction Airspeed Airspeed indicator markings Power plant Engine operating speeds and limits Fuel Coolant Power plant instrument markings Miscellaneous Instrument Marking Weight Center of gravity Approved maneuvers 2.10 Maneuvering load factors 2.11 Crew 2.12 Kinds of operation 2.13 Other limitations Date of Issue: 01/2016...
  • Page 18 Introduction Section 2 includes operating limitations, instrument markings and basic placards necessary for the safe operation of the aircraft, its engine, standard systems and standard equipment. Airspeed Airspeed limitations and their operational significance are shown below: Speed KIAS Remarks (km/h) Never exceed Do not exceed this speed in any speed...

  • Page 19: Airspeed Indicator Markings

    Airspeed indicator markings Airspeed indicator markings and their color-code significance are shown below: IAS value or range Marking Significance knots km/h White 62-139 33-75 Flap Operating Range. Green Normal Operating 80-240 43-129 Range. Maneuvers must be Yellow conducted with 240-290 129-157 caution and only in smooth air.
  • Page 20 Power plant Engine operating speeds and limits ROTAX 912 ULS 2 Engine Model: Bombardier-Rotax GMBH Engine Manufacturer: 100 hp at 5800 rpm, max.5 min. Max Take-off: 92.5 hp at 5500 rpm Max. Continuous: 68.4 hp at 5000 rpm Cruising: 5800 rpm, max. 5 min. Max.
  • Page 21 Fuel Fuel volume: Wing fuel tank volume ....2x60 l 2x16 US gal Unusable fuel quantity ....2x0.5 l 2x0.13 US gal Date of Issue: 01/2016 Revision: - Document No.: LSA-AOI-2-1-0-CL...
  • Page 22 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 0.951 US gal Date of Issue: 01/2016 Revision: - Document No.: LSA-AOI-2-1-0-CL...
  • Page 23 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 0.66 US gal Date of Issue: 01/2016 Revision: - Document No.: LSA-AOI-2-1-0-CL...

  • Page 24: Power Plant Instrument Markings

    Power plant instrument markings Analogue engine instruments markings and their color-code significance are shown below Normal Minimum Caution Maximum Rotax 912 ULS Operating Limit Range Range 98.6 hp Range (red line) (yellow arc) (red line) (green arc) Engine speed 1400 1400-5500 5500-5800 5800...

  • Page 25: Approved Maneuvers

    22 lb Center of gravity Operating C.G. range ......25 to 35 % of MAC Approved maneuvers Airplane Category: LSA The BRISTELL S-LSA is approved for normal and below listed maneuvers:  Steep turns not exceeding 60° bank  Lazy eights ...

  • Page 26: Kinds Of Operation

    2.11 Crew Number of seats ........2 Minimum crew ......... 1 pilot in the left seat Minimum crew weight ......55 kg 121 lb Maximum crew weight ......see SECTION 6 WARNING Do not exceed maximum take-off weight 600 kg (1320 lb)! 2.12 Kinds of operation There are permitted Day VFR flights.
  • Page 27 SECTION 3 EMERGENCY PROCEDURES Engine Failure Engine failure during take-off run Engine failure during take-off Engine failure in flight In-flight Engine Starting Smoke and Fire Fire on ground at engine starting Fire on ground with engine running Fire during take-off Fire in flight Fire in the cockpit Glide...
  • Page 28 Introduction Section 3 provides checklists and amplified procedures for coping with various emergencies that may occur. Emergencies caused by aircraft or engine malfunction are extremely rare if proper pre-flight inspections and maintenance are practiced. However, should an emergency arise, the basic guidelines described in this section should be considered and applied as necessary to correct the problem.
  • Page 29 Engine failure in flight 1. Push control stick forward 2. Speed - gliding at 120 km/h (65 KIAS) 3. Altitude - below 150 ft: land in take-off direction - over 150 ft: choose a landing area 4. Wind - find direction and velocity 5.

  • Page 30: Smoke And Fire

    Smoke and Fire Fire on ground at engine starting 1. Starter - keep in starting position 2. Fuel Selector - close 3. Throttle - full power 4. Ignition - switch off 5. Leave the airplane 6. Extinguish fire by a fire extinguisher (if available) or call for a fire- brigade if you cannot do it.
  • Page 31 Fire in flight 1. Heating - close 2. Fuel Selector - close 3. Throttle - full power 4. Master switch - switch off 5. Ignition - switch off after the fuel in carburetors is consumed and engine shut down 6. Choose of area - heading to the nearest airport or choose emergency landing area 8.

  • Page 32: Landing Emergencies

    Glide An example of the use of gliding is in the case of engine failure 1. Speed - recommended gliding speed 120 km/h (65 KIAS) Landing Emergencies Emergency landing Emergency landings are generally carried out in the case of engine failure and the engine cannot be re-started.
  • Page 33 6. Reduce power to idle when flying 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 assistance. NOTE Watch the chosen area steadily during precautionary landing.
  • Page 34 Recovery from Unintentional Spin WARNING Intentional spins are prohibited! There is no an uncontrollable 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.

  • Page 35: Other Emergencies

    Other Emergencies Vibration If any forced aircraft vibrations appear, it is necessary: 1. To set engine speed to such power rating where the vibrations are lowest. 2. To land on the nearest airfield or to perform a precautionary landing according to 3.6 Carburetor icing The carburetor icing shows itself through a decrease in engine power and an increase of engine temperatures.
  • Page 36 INTENTIONALLY LEFT BLANK Date of Issue: 01/2016 Revision: - Document No.: LSA-AOI-2-1-0-CL 3-10...
  • Page 37 SECTION 4 NORMAL PROCEDURES Assembly and Disassembly Pre-flight Inspection Normal procedures Before engine starting Engine starting Engine warm up, Engine check Taxiing Before take-off Take-off Climb Cruise Descent Before landing Balked Landing (Go around) Landing After landing Engine shutdown Aircraft parking and tie-down Flight in rain Date of Issue: 01/2016...
  • Page 38 Section 4 provides checklists and recommended procedures for normal operation of the aircraft. Assembly and Disassembly Refer to the BRISTELL S-LSA Maintenance and inspection procedures manual. Pre-flight Inspection Carry out the pre-flight inspection every day prior to the first flight or after airplane assembly.
  • Page 39 The manufacturer recommends carrying out the pre-flight inspection as follows: Date of Issue: 01/2016 Revision: - Document No.: LSA-AOI-2-1-0-CL...
  • Page 40 Inspection Check List  Ignition  - OFF  Master switch - ON  Fuel gauge ind. - check fuel quantity  Master switch - OFF  Avionics - check condition  Control system - visual inspection, function, clearance, free movement up to stops - check wing flaps operation ...
  • Page 41 WARNING Visually check fuel level in each fuel tank before each take-off to be sure that 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 OFF!) by turning the propeller. Always handle the blade area by the palm i.e.
  • Page 42 Normal procedures Before engine starting 1. Control system - free & correct movement 2. Canopy - clean 3. Brakes - fully applied Safety harness - tighten 5. Rudder pedal position - set WARNING Adjusting of rudder pedals position during flight is PROHIBITED. Engine starting 1.
  • Page 43 Engine warm up, Engine check 4.4.3.1 Engine warm up Prior to engine check block the main wheels using chocks. Initially warm up the engine to 2000 rpm for approx. 2 minutes, then continue to 2500 rpm till oil temperature reaches 50° (122°F). The warm up period depends on ambient air temperature.
  • Page 44 Before take-off 1. Altimeter - set 2. Trim - set neutral position 3. Control system - check free movement 4. Cockpit canopy - closed 5. Safety harness - tighten 6. Fuel Selector - ON (LEFT or RIGHT tank) 7. Ignition A,B - ON 8.
  • Page 45 Climb 1. Best ROC speed - 130 km/h (70 KIAS) 2. Throttle - Max. take-off power (max. 5800 rpm for 5 minutes) - Max. cont.power 5500 rpm 3. Trim - trim the airplane 3.1 Instruments - oil temperature and pressure, cylinder head/coolant temperature within limits CAUTION...
  • Page 46 Balked Landing (Go around) 1. Throttle - full power (max.5800 rpm) 2. Wing flaps - extend as needed 3. Trim - adjust as needed 4. Wing flaps - retract at height of 150 ft after reaching 120 km/h (65 KIAS) 5.
  • Page 47 Aircraft parking and tie-down 1. Ignition check - OFF 2. Master switch check - OFF 3. Fuel selector - OFF 4. Parking brake - use it as necessary (if installed) 5. Canopy - close, lock as necessary 6. Secure the airplane NOTE It is recommended to use parking brake (if installed) for short-time parking only, between flights during a flight day.
  • Page 48 INTENTIONALLY LEFT BLANK Date of Issue: 01/2016 Revision: - Document No.: LSA-AOI-2-1-0-CL 4-12...
  • Page 49 SECTION 5 PERFORMANCE Introduction Performance Airspeed indicator system calibration Stall speeds Take-off performance Landing distances Climb performance Cruise Endurance and Range Demonstrated crosswind performance Optimum glide speed Ceiling Date of Issue: 01/2016 Revision: - Document No.: LSA-AOI-2-1-0-CL...
  • Page 50 Introduction Section 5 provides data for airspeed calibration, stall speeds, take-off performance and additional information. 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 stated in this section is valid for maximum take-off weight and under ISA conditions.
  • Page 51 Performance Airspeed indicator system calibration KIAS KCAS (km/h) (km/h) Date of Issue: Date of Issue: 01/2016 09/2017 Revision: 1 Revision: - Document No.: LSA-AOI-2-1-0-CL...
  • Page 52 Stall speeds Altitude Conditions: Wing KIAS KCAS loss Max.takeoff-off flaps pos. [km/h] [km/h] at recovery weight Engine idle run [ft] 0° 20° Wing level stall 30° 0° Co-ordinated 20° turn 30° bank 30° Date of Issue: Date of Issue: 01/2016 09/2017 Revision: 1 Revision: -...
  • Page 53 Take-off performance Date of Issue: Date of Issue: 09/2017 01/2016 Revision: 1 Revision: - Document No.: LSA-AOI-2-1-0-CL...
  • Page 54 Landing distances Date of Issue: Date of Issue: 01/2016 09/2017 Revision: 1 Revision: - Document No.: LSA-AOI-2-1-0-CL...
  • Page 55 Climb performance CONDITIONS: BEST RATE OF CLIMB BEST ANGLE OF CLIMB RATE OF RATE OF RATE OF RATE OF KIAS KIAS MTOW CLIMB CLIMB CLIMB CLIMB Flaps retract. ALTITUDE [mph] [km/h] [knots] [m/s] [fpm] [mph] [km/h] [knots] [m/s] [fpm] 0 ft ISA 2000 ft ISA 4000 ft ISA 6000 ft ISA...
  • Page 56 Cruise 4300 rpm 4800 rpm 5000 rpm 5500 rpm 5800 rpm KIAS 87 knots 101 knots 106 knots 119 knots 127 knots 0 ft KCAS 89 knots 102 knots 107 knots 120 knots 127 knots KTAS 89 knots 102 knots 107 knots 120 knots 127 knots KIAS 85 knots 99 knots 104 knots 117 knots 125 knots 2000 ft...
  • Page 57 Endurance and Range The table below shows fuel consumption, endurance and range 120 l Fuel qty. = NO FUEL RESERVE CONSIDERED ! Unusable fuel = 4300 rpm 4800 rpm 5000 rpm 5500 rpm 5800 rpm KIAS 87 knots 101 knots 106 knots 119 knots 127 knots...
  • Page 58 Demonstrated crosswind performance 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 Optimum glide speed Optimum glide speed .........
  • Page 59 SECTION 6 WEIGHT AND BALANCE Introduction Weight and Balance Record Weight and 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 Permitted payload range Date of Issue: 01/2016 Revision: - Document No.: LSA-AOI-2-1-0-CL...
  • Page 60 Introduction This section contains the payload range within which the BRISTELL S-LSA may be safely operated. Procedures for weighing the aircraft and the calculation method for establishing the permitted payload range are contained in last revision of FAA Aviation Advisory Circular AC.43.13 – 1B...
  • Page 61 25. Garmin GTR 20 remote-mount comm radio 26. Garmin GTX 23 ES mode S transponder 27. Grey interior 28. Key switch box 29. Lambert+LINAK electric flaps actuator 30. Leather glareshield, Leather upholstery 31. Lockable canopy, Lockable fuel tank caps 32. Long HTU (2.9 m) with long trim and horn balance 33.
  • Page 62 Weight and Balance Report 6.2.1.1 Empty Aircraft Weight and CG MAC (mm): 1350,0 WEIGHT MOMENT = WEIGHT x ARM ITEM (kg) (mm) (kg.mm) RIGHT MAIN WHEEL 140,2 100916,3 LEFT MAIN WHEEL 142,4 102549,2 NOSE WHEEL 71,2 -750 -53411,0 EMPTY WEIGHT EMPTY ACFT TOTAL MOMENT CG (mm) = 424,12 (kg)
  • Page 63 6.2.1.2 Loaded Aircraft Weight and CG ITEM WEIGHT MOMENT = WEIGHT x ARM (kg) (mm) (kg.mm) 353,8 424,12 150054,4 EMPTY AIRCRAFT 600,0 PILOT PASSENGER 600,0 BAGGAGE - BEHIND 1400,0 SEATS BAGGAGE - FRONT -300,0 optional) BAGGAGE - WING 630,0 LOCKERS 200,0 FUEL TANKS TAKEOFF WEIGHT...
  • Page 64 6.2.1.3 Weight and CG Blank Form ITEM WEIGHT MOMENT = WEIGHT x ARM (kg) (mm) (kg.mm) RIGHT MAIN WHEEL 720,0 LEFT MAIN WHEEL 720,0 NOSE WHEEL -750,0 EMPTY WEIGHT CG (mm) = EMPTY ACFT TOTAL MOMENT (kg) (kg.mm) EMPTY AIRCRAFT CG (%MAC) = ITEM WEIGHT...
  • Page 65 Permitted payload range PERMITTED PAYLOAD RANGE OF BRISTELL (kg) S/N: 317/2018 Empty weight (kg): MTOW (kg): 600,0 VOLUME (litres) WEIGHT (kg) 14,5 29,0 43,5 58,0 72,5 87,0 PERMITTED CREW WEIGHT (kg) NO BAGGAGE 35,0 %MAC 35,0 %MAC 34,6 %MAC 33,9 %MAC...
  • Page 66 INTENTIONALLY LEFT BLANK Date of Issue: 01/2016 Revision: - Document No.: LSA-AOI-2-1-0-CL...
  • Page 67 SECTION 7 AIRPLANE AND SYSTEMS DESCRIPTION Introduction Airframe Control system Landing gear Seats and safety harness Baggage compartment Canopy Power plant Throttle Heating Fuel system 7.10 Electrical system Battery Master switch Ignition Switch 7.11 Pitot and static pressure system 7.12 Miscellaneous equipment 7.13 Instruments and Avionics 7.14 Cockpit Cockpit layout...

  • Page 68: Control System

    Introduction This section provides description and operation of the aircraft and its systems. Airframe All-metal construction, single curvature metal skins riveted to stiffeners. Construction is of 6061-T6 aluminium sheet metal riveted to aluminium angles with Avex rivets. This high strength aluminium alloy construction provides long life and low maintenance costs thanks to its durability and corrosion resistance characteristics.

  • Page 69: Landing Gear

    Landing gear Tricycle landing gear with the steerable nose wheel. Main landing gear uses two fiberglass spring elements. Seats and safety harness Side-by-side seating. Seat cushions are removable to make easier cleaning and drying. Four point safety belts provided to each seat. Optional, is additional seat upholstery to raise the small pilot or move him forward.
  • Page 70 Power plant Engine: ROTAX 912 ULS S engine 98.6 hp is installed. Rotax 912 ULS is 4-stroke, 4 cylinder, horizontally opposed, spark ignition engine with one central camshaft-push-rod-OHV. Liquid cooled cylinder heads, ram air cooled cylinders. Dry sump forced lubrication. Dual contactless capacitor discharge ignition. The engine is fitted with an electric starter, AC generator and mechanical fuel pump.

  • Page 71: Fuel System

    Fuel system Wing tanks volume: ......2x60 l 2x16 US gallons Each tank is equipped 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 console in the cockpit.

  • Page 72: Electrical System

    7.10 Electrical system Battery The battery is mounted on the forward side of the firewall. Master switch Master switch connects the electrical system to the 12 Volt battery and charger/coils, controlled by the regulator. See Engine Manual for electrical system details. NOTE Ignition system is independent on the power source and will operate even with Master switch and/or breaker off.
  • Page 73 7.12 Miscellaneous equipment BRISTELL S-LSA S/N 317/2018 is fitted with: 1. 12V/5V socket behind seats and on instrument panel 2. 2 map pockets 3. 3-pos.adjustable rudder pedals on both sides 4. 4-point safety belts 5. Arm rest box 6. Aveo Silver Max air vents 7.

  • Page 74: Instruments And Avionics

    7.13 Instruments and Avionics BRISTELL S-LSA S/N 317/2018 is fitted with: 1. Back-up ALT Winter 4 FGH 40 2. Back-up ASI Winter 7FMS 513 (0-160 kts) 3. Back-up variometer BC6 (+/- 2000 f) 4. Airpath C2400 L4P Compass 5. Garmin G3X flight display system including: 6.
  • Page 75 7.14 Cockpit Cockpit layout Date of Issue: 01/2016 Revision: - Date of Issue: 09/2017 Revision: 1 Document No.: LSA-AOI-2-1-0-CL...
  • Page 76 Instrument panel Date of Issue: 01/2016 Revision: - Date of Issue: 09/2017 Revision: 1 Document No.: LSA-AOI-2-1-0-CL 7-10...
  • Page 77 SECTION 8 Airplane handling, servicing and maintenance Introduction Aircraft inspection periods Aircraft alterations or repairs Ground handling Towing Parking Mooring Jacking Road transport Cleaning and care Date of Issue: 01/2016 Revision: - Document No.: LSA-AOI-2-1-0-CL...
  • Page 78 50 flight hours after every 100 flight hours or at least annual inspection For BRISTELL S-LSA aircraft maintenance refer to the Maintenance and Inspection Procedures, Section 2. For Rotax 912 ULS engine maintenance refer to the Maintenance Manual (Line Maintenance) for Rotax Engine Type 912 Series.

  • Page 79: Ground Handling

    Ground handling Towing To handle the airplane on the ground, use the Tow Bar, or the fuselage rear pushed down in the place of a bulkhead. CAUTION Avoid excessive pressure at the airplane airframe-especially at control surfaces. Keep all safety precautions, especially in the propeller area. Parking It is advisable to park the airplane inside a hangar or alternatively inside any other suitable space (garage) with stable temperature, good ventilation, low...

  • Page 80: Cleaning And Care

    Jacking Since the empty weight of this aircraft is relatively low, two people can lift the aircraft easily. First of all prepare two suitable supports to support the aircraft. It is possible to lift the aircraft by handling the following parts: −...
  • Page 81 SECTION 9 REQUIRED PLACARDS AND MARKINGS Limitation placards Miscellaneous placards and markings Date of Issue: 01/2016 Revision: - Document No.: LSA-AOI-2-1-0-CL...

  • Page 82: Limitation Placards

    Limitation placards The airplane must be placarded with: − All fuses − Ignition switches − Choke − Starter − Trim: Nose heavy and Tail heavy − Flaps: 0°, 10°, 20°, 30° − Maximum rear baggage weight 15 kg (33 lb) −...
  • Page 83 Passenger warning for LSA category aeroplanes. Located on the instrument panel. Passenger notice for LSA category aeroplanes. Located on the instrument panel. Operation limitation. Located on the instrument panel. Operation limitation. Located on the instrument panel. Main baggage compartment behind the seats.
  • Page 84 Maximum Takeoff Weight Limitation. 1320 lb limit for Light sport aeroplanes. Located on the instrument panel or fuselage side. Date of Issue: Date of Issue: 01/2016 09/2017 Revision: 1 Revision: - Document No.: LSA-AOI-2-1-0-CL...
  • Page 85 Miscellaneous placards and markings Wing flap root area Areas to avoid pushing on them. Wing trailing edge, control surfaces trailing edges, etc. Located on wing upper skin around the fuel tank filler neck. Throttle and Choke placard located on the Throttle-choke quadrant.
  • Page 86 Located on the top of the canopy inside. Located on the lever between seats. If BRS 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 located static ports.
  • Page 87 SECTION 10 SUPPLEMENTS 10.1 Introduction 10.2 List of inserted supplements 10.3 Inserted Supplements Date of Issue: 01/2016 Revision: - Document No.: LSA-AOI-2-1-0-CL 10-1...
  • Page 88 10.1 Introduction This section contains the appropriate supplements necessary to safely and efficiently operate the aircraft when equipped with various optional systems and equipment not provided with the standard airplane. Date of Issue: 01/2016 Revision: - Document No.: LSA-AOI-2-1-0-CL 10-2...
  • Page 89 10.2 List of inserted supplements Suppl. Date Title of inserted supplement 07/2011 01/2011 Aircraft Flight Training Supplement 12/2017 Description of the aircraft S/N 317/2018 Date of Issue: 01/2016 Revision: - Document No.: LSA-AOI-2-1-0-CL 10-3...
  • Page 90 10.3 Inserted Supplements Date of Issue: 01/2016 Revision: - Document No.: LSA-AOI-2-1-0-CL 10-4...
  • Page 91 SUPPLEMENT No. 01/2011 Aircraft Flight Training Supplement The BRISTELL LSA flying characteristics and behavior are similar to single engine aircraft. Following training procedure is applicable if the pilot is holder of UL, PPL or LSA Pilot License. The training flight hours are recommended minimum and depends on the Flight Instructor if student pilot is ready to continue on in next training step.
  • Page 92 Flight training program - recommended Dual Solo Flight Training Procedure Flights hr/min Flights hr/min 30’ Check flight Pattern training flights up to 20’ 15’ 1000 ft AGL Pattern training flights up to 20’ 15’ 500 ft AGL Stall speed, 45°turns, side slips 30’...
  • Page 93 Flight Training Procedure - description 1. Check flight – Student Pilot will fly the airplane in local flight, instructor is giving advice as necessary. 2. Pattern training flights up to 1000 feet AGL - high pattern procedures, instructor is giving advice as necessary. 3.
  • Page 95 SUPPLEMENT No. 02 AIRCRAFT DESCRIPTION Registration: CC-AUV Serial number: 317/2018 This Supplement must be contained 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 further mentioned parts only. Limitations, procedures and information not mentioned in this Supplement are contained in the basic Aircraft Operating Instructions.
  • Page 96 0 TECHNICAL INFORMATION This Supplement adds information necessary for airplane operation with equipment installed in the airplane BRISTELL S-LSA of S/N 317/2018. 0.1 Record of revisions No changes. GENERAL INFORMATION No changes. OPERATING LIMITATION 2.4.3 Oil NOTE: Type of oil used by aircraft manufacturer : Aeroshell OIL SPORT PLUS 4 2.4.4 Coolant...
  • Page 97 6 WEIGHT AND BALANCE No changes. 7 AIRPLANE AND SYSTEMS DESCRIPTION No changes. 8 AIRPLANE HANDLING, SERVICING AND MAINTENANCE No changes. Date of Issue: 12/2017 Revision: - 3 of 3...

Table of Contents