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100 HP MCR SPORTSTER FLIGHT MANUAL

DynAero MCR-01 Sportster · Weight & Balance

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Overview

This document is the weight and balance section of the flight manual for the Dynaero MCR-01 Sportster aircraft. It provides essential information regarding the aircraft's weight limits, loading procedures, and balance considerations necessary for safe operation.

  • The aircraft must always be used in accordance with the information and limitations contained in this document.
  • The user is responsible for ensuring the aircraft complies with regulations.
  • This aircraft was built from a kit and must not be used for hire or reward.
  • Weight and balance procedures are critical for safe flight operations.
  • The flight manual includes specifications and limitations for the aircraft.
  • The aircraft is certified under French regulations.
  • The manual contains information imperative for pilots and instructors.
  • The builder must complete specific configuration details.

Document

Source

Originally published by mcr.aero. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

View original at mcr.aero

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Document details

Type
·
Weight & Balance
Year
·
2024
File size
·
1.3 MB
Publisher
·
mcr.aero
Language
·
fr

Specifications & performance

Extracted from this document.

Specifications

Span m
·
6.63
Height m
·
1.43
Aspect ratio
·
8.45
Cabin width m
·
1.12
Fuel capacity l
·
80
Wing surface m2
·
5.2
Overall length m
·
5.48
About this document
What is the 100 HP MCR SPORTSTER FLIGHT MANUAL?

The 100 HP MCR SPORTSTER FLIGHT MANUAL is a weight & balance for the DynAero MCR-01 Sportster, dated 2024.

Where does the 100 HP MCR SPORTSTER FLIGHT MANUAL come from?

This copy of the 100 HP MCR SPORTSTER FLIGHT MANUAL was originally published by mcr.aero and is hosted on Sprinkle as a free, searchable reference copy.

What year was the 100 HP MCR SPORTSTER FLIGHT MANUAL published?

The 100 HP MCR SPORTSTER FLIGHT MANUAL — the DynAero MCR-01 Sportster weight & balance on file — is dated 2024.

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In this document

General

The general section introduces the flight manual, emphasizing the importance of the information for pilots and the need for builders to complete specific configurations.

Limitations

This section outlines operating limitations, including airspeed limits and their operational significance, which are crucial for safe aircraft operation.

Specifications

Specifications detail the aircraft's dimensions, fuel capacity, and structural characteristics, providing essential data for understanding the aircraft's capabilities.

Weight & Balance

This section covers weight and balance registration, loading envelope, and procedures necessary to ensure the aircraft is within safe operational limits.

Warnings, Alarms and Notes

Definitions of warnings, alarms, and notes used in the manual are provided, highlighting their significance in relation to flight safety.

Emergency Procedures

Emergency procedures outline actions to take in various emergency situations, ensuring pilots are prepared for unexpected events.

Safety notes

  • This document is provided for information only; the owner must verify the accuracy of the material.
  • The aircraft must not be used for hire or reward.
  • The user is responsible for ensuring compliance with regulations.
  • Certain details must be added by the builder to reflect the actual configuration.
  • The aircraft must always be used in accordance with the limitations contained in this document.

Full document text

SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 Operation REF: M EX NO 07 04 First issue: Pages Date Written by Visa Checked by Visa 100 HP MCR SPORTSTER FLIGHT MANUAL Serial number : SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 41 29/08/00 N. BOUCHOUT C. BELIN Edition : Edition Date Written by Visa Checked by Visa 04 23/03/2015 B.GARREAU L.CHICOUENE SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 Up-dates : Pages Date Written by Visa Checked by Visa 14, 33 22/12/00 N. BOUCHOUT C. BELIN + garde 12/02/02 C. BELIN N. BOUCHOUT +8, 15, 17 07/04/02 N. BOUCHOUT C. BELIN - 17/10/2014 L.CHICOUENE B.GARREAU 1,2,6,7,8,16, 17,18,19 06/03/2015 B.GARREAU L.CHICOUENE 10, 22 23/03/2015 B.GARREAU L.CHICOUENE 17/10/2024 L. VERDANT E. FUMEY Page N°3 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 0. WARNING THIS DOCUMENT IS PROVIDED FOR INFORMATION ONLY. IT IS THE OWNER'S RESPONSABILITY TO CHECK THE EXACTNESS OF THE PRESENT MATERIAL WITH RESPECT TO HIS/HER ACTUAL AIRCRAFT. Page N°4 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 1. FLIGHT MANUAL Model : MCR01 VLA Serial Number : Registration : Document number : Release date : The pages identified by "Appr" are approved by : Signature : Authority : Stamp : Date of approval: 420 Certain details must be added by the builder to reflect the exact configuration and installation of engine, Propeller and instrumentation. THIS PLANE MUST ALWAYS BE USED IN ACCORDANCE WITH THE INFORMATION AND LIMITATIONS CONTAINED IN THIS DOCUMENT. THIS PLANE WAS BUILT FROM A KIT. IT MUST NOT BE USED FOR HIRE OR REWARD. THE USER IS RESPONSIBLE FOR THE USE OF THE AIRCRAFT , ENSURING THAT IT COMPLIES WITH REGULATIONS AND INFORMING ANY PASSENGER OF THE LIMITATIONS OF THE AIRCRAFT WITH RESPECT TO ITS AIRWORTHINESS LIMITATIONS. THIS FLIGHT MANUAL WAS ESTABLISHED ACCORDING TO FRENCH REGULATION. Page N°5 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 1.1. REGISTRATION OF THE OVERHAULS All amendments to this document must be entered in the table below, except weighing data, and all cases of approved sections, aimed and approved by the Authority responsible for Airworthiness. The new text or amendment in the revised pages will be indicated by a dark vertical line in the left margin and the N° of the amendment and the date will be indicated on the bottom left corner of the page. Revision N° Affected section Affected pages Date Approval Date Date of insertion Signed 1.2. LIST OF PAGES Section Page Date Section Page Date Page N°6 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 1.3. TABLE OF CONTENTS Contenu 0. WARNING 3 1. FLIGHT MANUAL 4 1.1. REGISTRATION OF THE OVERHAULS 5 1.2. LIST OF PAGES 5 1.3. TABLE OF CONTENTS 6 2. GENERAL 10 2.1. INTRODUCTION 10 2.2. BASIS OF CERTIFICATION 10 2.3. WARNINGS, ALARMS AND NOTES 10 2.4. SPECIFICATIONS 11 2.5. CONTROL SURFACE DEFLECTION 11 2.6. THREE VIEW DIAGRAM 12 3. LIMITATIONS 14 3.1. INTRODUCTION 14 3.2. AIRSPEED 14 3.3. INDICATED AIRSPEED INSTRUMENTS MARKINGS 15 3.4. ENGINE INSTALLATION 16 3.4.1. ROTAX 912 ULS/S ENGINE 16 3.4.2. PROPELLERS 17 3.5. ENGINE INSTRUMENT MARKINGS 19 3.5.1. ROTAX 912 S ENGINE 19 3.6. INSTRUMENT MARKINGS 20 3.7. WEIGHT 20 3.8. WEIGHT & BALANCE 20 3.9. APPROVED MANOEUVRES 20 3.10. MANOEUVRING LOAD FACTOR 21 3.11. MINIMUM FLIGHT CREW 21 3.12. TYPES OF FLIGHT 21 3.13. FUEL 21 3.14. MAXIMUM NUMBER OF SEATS 21 3.15. TIRE PRESSION 21 3.16. INSTRUMENT PANEL WEIGHT LIMITATION 21 3.17. SOLO FLIGHT 22 3.18. OTHER LIMITATIONS 22 3.19. PLACARDS 22 Page N°7 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 3.19.1. DURING INITIAL EXPERIMENTATION PERIOD 22 3.19.2. IN FRONT OF PILOT VIEW 22 Page N°8 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 3.19.3. AIR SPEED INDICATOR 22 3.19.4. ENGINE INSTALLATION INSTRUMENTS 22 3.19.5. CONTROL SYSTEM MARKINGS 22 3.19.6. MISCELLANEOUS PLACARDS AND MARKINGS 23 4. EMERGENCY PROCEDURES 24 4.1. INTRODUCTION 24 4.2. ENGINE FAILURE 24 4.2.1. ENGINE FAILURE ON TAKE-OFF RUN 24 4.2.2. ENGINE FAILURE IMMEDIATELY AFTER TAKE-OFF 24 4.3. IN-FLIGHT RESTART 25 4.3.1. STARTER MOTOR RESTART 25 4.3.2. DIVE RESTART 25 4.4. SMOKE AND FIRE 25 4.4.1. FIRE ON ENGINE START 25 4.4.2. AIRBORNE ENGINE FIRE 26 4.4.3. CABIN FIRE 26 4.5. GLIDING 26 4.6. FORCED LANDING 26 4.6.1. PLANNED FORCED LANDING WITH ENGINE STOPPED 26 4.6.2. PLANNED FORCED LANDING WITH ENGINE RUNNING 27 4.7. RECOVERY FROM AN UNINTENTIONAL SPIN 27 4.8. OTHER EMERGENCIES 27 4.8.1. VIBRATIONS AND ERRATIC ENGINE BEHAVIOUR : LIKELY CAUSES. 27 4.8.2. OIL FEED MALFUNCTION 27 4.8.3. ICING 27 4.8.4. ELECTRIC GENERATION FAILURE 27 4.8.5. LOW VOLTAGE (VOLTMETER). 27 5. NORMAL PROCEDURES 28 5.1. INTRODUCTION 28 5.2. DAILY CHECK 28 5.3. PRE-FLIGHT CHECK 30 5.4. NORMAL PROCEDURES AND CHECK-LISTS 30 5.4.1. CABIN CHECK PRIOR TO ENGINE START 30 5.4.2. COLD ENGINE START (ROTAX) 30 5.4.3. HOT ENGINE START 30 5.4.4. TAXIING 30 5.4.5. ENGINE GROUND RUN 31 5.4.6. PRE-TAKE-OFF CHECKS 31 5.4.7. TAKE-OFF 31 5.4.8. CLIMB 31 5.4.9. CRUISE 32 5.4.10. DESCENT 32 5.4.11. APPROACH 32 5.4.12. FINAL 32 5.4.13. GO-AROUND 32 Page N°9 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER

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tel: 03 81 89 70 84 Ed 5 17/10/2024 5.4.14. POST-LANDING CHECKS 32 5.4.15. ENGINE STOP 32 Page N°10 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 6. PERFORMANCES 34 6.1. INTRODUCTION 34 6.2. APPROVED DATA 34 6.2.1. AIRSPEED INDICATOR CALIBRATION 34 6.2.2. STALLING SPEED (KNOTS) 34 6.2.3. TAKE-OFF PERFORMANCES (ROTAX 912 S 100 HP) 35 6.2.4. LANDING DISTANCES 35 6.2.5. TAKE-OFF DISTANCES CALCULATION 35 6.2.6. EFFECT OF RAIN AND INSECTS ON AIRCRAFT PERFORMANCE, FLYING AND HANDLING QUALITIES. 35 6.2.7. CROSS-WIND DEMONSTRATED PERFORMANCES 35 6.2.8. NOISE LIMITATIONS 35 7. WEIGHT & BALANCE 36 7.1. INTRODUCTION 36 7.2. WEIGHT & BALANCE REGISTRATION AND LOADING ENVELOPE 36 7.2.1. LOADING ENVELOPE 36 7.2.2. WEIGHT & BALANCE PROCEDURE 37 8. AIRCRAFT OPERATION, SERVICING AND MAINTENANCE 38 8.1. INTRODUCTION 38 8.2. AIRCRAFT MAINTENANCE SCHEDULE 38 8.3. AIRCRAFT MODIFICATIONS AND REPAIRS 38 8.4. PARKING 39 8.4.1. GROUND FIXING 39 8.5. CLEANING AND TREATMENT 39 9. SUPPLEMENTARY SYSTEMS AND EQUIPMENTS 40 9.1. INTRODUCTION 40 9.2. MINIMUM EQUIPMENT LIST 40 9.3. LIST OF THE SUPPLÉMENTARY SYSTEMS AND EQUIPMENTS 40 9.4. SUPPLEMENTARY ELEMENTS DESCRIPTIONS 40 Page N°11 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 Intentionally left blank Page N°12 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 2. GENERAL 2.1. INTRODUCTION The flight manual for the aircraft was designed to provide pilots and instructors with the information necessary to efficiently and safely fly this very light aircraft. This manual contains information that are imperative to be given to the MCR VLA pilot. It also contains supplementary information given by the builder. The builder should complete the information appropriate to the particular configuration and selection of options. A special place must be reserved on the luggage compartment floor in order to store this flight manual. 2.2. BASIS OF CERTIFICATION This type of aircraft was approved by DGAC in accordance with the regulations applicable to kit aircraft, including the FAR 23 amendment 7 and the certificate of restricted Airworthiness N°2A-0005 has been issued on the 26/06/2001. Category of Airworthiness : Restricted (kit) 2.3. WARNINGS, ALARMS AND NOTES The following definitions apply to Warnings, Alarms & Notes used in the flight manual. ALARM: Signifies that a failure to observe the corresponding procedures will lead to an immediate or important deterioration of the flight safety. WARNING: Signifies that a failure to observe the corresponding procedures will lead to a minor or major deterioration of the long term flight safety. Page N°13 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 NOTE: Draws attention to a condition which although not particularly related to the flight safety is important or unusual. 2.4. SPECIFICATIONS Kit aircraft of the type : Dyn'Aéro MCR Sportster Cantilever low-mounted wing. Carbon structure with wing and control surface skins made in light alloy. Span 6.63 m Wing surface 5.2 m² Aspect ratio 8.45 Cabin width 1.12 m Fuel capacity 80 l Overall Length 5.48 m Height 1.43 m 2.5. CONTROL SURFACE DEFLECTION Ailerons : - 5° (1) trailing edge upwards +3° (1) trailing edge downwards Flaps : 0-25° (+0-1) Rudder : 20° (-0+5) in both directions (left and right) Tailplane : - 10° (+0-2) trailing edge upwards +3.5° (-0+1) trailing edge downwards Page N°14 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 2.6. THREE VIEW DIAGRAM MCR SPORTSTER Page N°15 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 Intentionally left blank Page N°16 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 3. LIMITATIONS 3.1. INTRODUCTION This section includes operating limitations, reference marks of instruments and placards necessary for the safe use of the aircraft, its engine, standard systems and equipment. The limitations included in this section and in section 9 were approved by . 3.2. AIRSPEED Airspeed limits and their operational significance. Airspeed (IAS) Remarks VNE Never exceed speed 320 km/h Velocity you must Never Exceed, in any case 173 kts VNO Maximum structural cruising speed 264 km/h Do not exceed this Velocity in Normal Operations, except in calm air, and then , only with great cautions. 143 kts VA Manoeuvring speed 235 km/h Do not apply abrupt or full-range control deflections beyond this speed, because under certain conditions, the Aircraft might be exposed to excessive loads. 127 kts VFE Maximum speed allowed with flaps extended 170 km/h Do not exceed this Velocity with Flaps Extended 92 kts Page N°17 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 3.3. INDICATED AIRSPEED INSTRUMENTS MARKINGS Air speed indicator reference marks and colour significance. Marking (IAS) Significance White segment (92 / 170 km/h) (50 / 92 kts) Speed range allowed with flaps extended Green segment (120 / 264 km/h) (65 / 143 kts) Speed range for normal operational flight Yellow segment (264 / 320 km/h) (143 / 173kts) Manoeuvres must be carried out with caution and only in conditions of calm air Red segment (320 km/h) (173 kts) Maximum speed for all operations Page N°18 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 3.4. ENGINE INSTALLATION Only the configurations of engine and propeller written in this manual are allowed 3.4.1. Rotax 912 ULS/S Engine Engine manufacturer Rotax Engine model 912 S Maximum power Take-off 100 HP Continuous 92 HP Maximum manifold pressure Take-off 27.5” Hg / 930 mbar Continuous 27” Hg / 920 mbar Maximum engine RPM Take-off 5800 RPM Continuous 5500 RPM Maximum Cylinder Head Temperature 135 °C / 275 °F Maximum Oil Temperature: 130 °C / 266 °F Oil pressure Minimum: 0.8 Bar Maximum: 7 Bars Fuel pressure Minimum: 0.15 Bar Maximum: 0.40 Bar Octane grade of fuel: Refer to Rotax manual Oil quality: Refer to Rotax manual Page N°19 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 3.4.2. Propellers MT Propeller MT 156-220-2M Three blades, fixed pitch Diameter : 156 cm Composition : wood and composite MTV-7-A / 156-122 Three blades, electrical variable pitch Diameter : 156 cm Composition : wood and composite MTV-6-A / 156-122 Three blades, hydraulic variable pitch Diameter : 156 cm Composition : wood and composite MTV-34-A / 164-200 Three blades, hydraulic variable pitch Diameter : 164 cm Composition : wood and composite Aupa Dyn’Aero MKIHE10 Three blades, fixed pitch Diameter : 156 cm Composition : composite MKIHE11 Two blades, fiwed pitch Diameter : 156 cm Composition : composite MKIHE12 Two blades, hydraulic variable pitch Diameter : 156 cm Composition : composite MKIHE13 Three blades, hydraulic variable pitch Diameter : 156 cm Composition : composite MKIHE32 Two blades, hydraulic variable pitch Diameter : 170 cm Composition : bois et composite DUC HELICE SW3_3-D-1 Tripale, pas réglable au sol Diameter : 160 cm Composition : composite E-PROPS GLOR-3-160-C8-T Three blades, hydraulic variable pitch Diameter : 160 cm Composition : composite Page N°20 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 !! Tighten propeller bolts before first flight, after 1 flight hour and 5 flight hours. Then control tightening every 50 flight hours and after each ground period that last more than 1 month !!!!!!!! Page N°21 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 Intentionally left blank Page N°22 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 3.5. ENGINE INSTRUMENT MARKINGS 3.5.1. Rotax 912 S Engine ROTAX 912 S Instrument Units Red line Green sector Yellow sector Red Line Minimum Normal Warning Maximum Limit Range Range Limit Tachometer Tr/Min 1500 to 5500 5500 to 5800 5800 Oil temperature °C 50 °C 122 °F 90 to 100 °C 194 to 212 °F 110 to 130 °C 230 to 266 °F 130 °C 266 °F Cylinder Head °C 50 °C 80 to 120 °C 120 to 150 °C 150 °C Temperature 122 °F 176 to 248 °F 248 to 275 °F 275 °F Fuel Pressure Bar 0.15 Bar 0.15 to 0.40 Bar 0.40 Bar PSI 2.2 PSI 2.2 to 5.8 PSI 5.8 PSI Oil Pressure Bar 1.5 Bars 1.5 to 4 Bars 4 to 5 Bars 5 Bars Fuel Quantity Litre 1 Litre 79 Litres Note carefully : Do not switch off the main switch before turning off the engine. Never run continuously the engine above 5 500 rpm more than 5 minutes. Page N°23 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 3.6. INSTRUMENT MARKINGS (to be completed by the builder according to the actual instrument configuration) 3.7. WEIGHT Maximum take-off weight : 490 kg Maximum landing weight : 490 kg Maximum weight without fuel 432 kg 3.8. WEIGHT & BALANCE Centre of Gravity range 15 / 45% M.A.C. Datum M.A.C. 500 450 400 350 300 250 10% 15% 20% 25% 30% 35% 40% 45% 50% Balance ratio compared to M AC M.A.C. = 800 mm ; reference datum : 13.5 mm ahead of left wing leading-edge. M a ss ( k g Page N°24 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 3.9. APPROVED MANOEUVRES Page N°25 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 THIS AIRCRAFT IS CERTIFIED IN THE NORMAL CATEGORY. AEROBATIC FLIGHT IS PROHIBITED. SPINS ARE PROHIBITED. 3.10. MANOEUVRING LOAD FACTOR +3.8 / -1.5 g 3.11. MINIMUM FLIGHT CREW Minimum flight crew is one pilot. Two people onboard maximum. 3.12. TYPES OF FLIGHT VFR / DAY. 3.13. FUEL Total fuel : 80 l Useable fuel : 79 l Unusable fuel : 1 l Fuel Octane grade approved: Refer to Rotax manual 3.14. MAXIMUM NUMBER OF SEATS Two 3.15. TIRE PRESSION Nose landing gear : 280 mm diameter wheel 2.2 bar 210 mm diameter wheel 3 bar Main landing gear : 280 mm diameter wheel 2.2 bar Page N°26 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 3.16. INSTRUMENT PANEL WEIGHT LIMITATION Page N°27 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 Maximum weight of instrument panel when equipped and wired = 15 kg 3.17. SOLO FLIGHT For each solo flight, the unused harness must be locked. 3.18. OTHER LIMITATIONS USE FOR HIRE OR REWARD - PROHIBITED. THIS AIRCRAFT MUST BE USED STRICTLY IN ACCORDANCE WITH THE LEGISLATION APPROPRIATE FOR KIT AIRCRAFT. 3.19. PLACARDS 3.19.1. During initial experimentation period Minimum 5 cm high placard "EXPERIMENTAL" must be placed next to each cabin openings. 3.19.2. In front of pilot view Written in minimum 6 mm high letters and so that both pilots can easily read it, the following placard : CET AERONEF VOLE SOUS UN REGIME DU CERTIFICAT DE NAVIGABILITE RESTREINT. IL NE REPOND PAS AUX CONDITIONS DE DELIVRANCE ET DE MAINTIEN DU CERTIFICAT DE NAVIGABILITE NORMAL. SON UTILISATION A TITRE ONEREUX EST INTERDITE. TOUTES LES MANŒUVRES ACROBATIQUES, Y COMPRIS LA VRILLE INTENTIONNELLE, SONT INTERDITES. UTILISATION UNIQUEMENT POUR LE VFR DE JOUR DANS DES CONDITIONS SANS GIVRAGE A placard indicating the manoeuvring speed VA = 127kts (235km/h) 3.19.3. Air speed indicator Each air speed indicator must be marked as indicated in paragraph 3.3 3.19.4. Engine installation instruments Each engine installation instrument must be marked as indicated in paragraph 3.5.1. 3.19.5. Control system markings Page N°28 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 Each control system other than main flight control systems must be marked in order to explain its function and operation mode : brake control system, parachute control system must be marked in red if installed... 3.19.6. Miscellaneous placards and markings In luggage compartment : "Maximum luggage weight = 15 kg" Fuel tank filler : "Fuel tank : 80 l Mini fuel grade : RON 90" Oil tank filler "Oil tank : 3.5 l 10 W 40" Page N°29 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 4. EMERGENCY PROCEDURES 4.1. INTRODUCTION This section provides a list of appropriate actions in the event of certain emergencies. Providing that the aircraft is well maintained and proper pre-flight inspections are made, emergencies due to failure of the aircraft, aircraft engine or other systems is very rare. However, should an emergency occur, the procedures described in this section of the manual should be adopted. 4.2. ENGINE FAILURE 4.2.1. Engine failure on take-off run If there is enough runway length remaining : - Fully reduce Power and apply brakes. If there is insufficient runway length remaining : - Fully reduce power - Brake hard - Fuel tap............................................................................................. closed - Magnetos ............................................................................................... OFF - Battery ................................................................................................... OFF 4.2.2. Engine failure immediately after take-off - Airspeed ........................................................................................ 70 knots - Fuel tap............................................................................................. closed - Magnetos ............................................................................................... OFF - Flaps ......................................................................................... as required - Battery ................................................................................................... OFF Never attempt to make a U turn to return to the runway. Page N°30 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 4.3. IN-FLIGHT RESTART 4.3.1. Starter motor restart If the altitude is sufficient to attempt to restart the engine : - Airspeed ........................................................................................ 70 knots - Fuel tap................................................................................................ open - Electric fuel pump .................................................................................... on - Throttle setting ......................................................................................... 1/2 - Magnetos ........................................................................................ "BOTH" - Starter ...................................................................................................... on If the motor does not start, plan to make a forced landing. 4.3.2. Dive restart If the altitude is sufficient to attempt to restart the engine (minimum altitude lost 1500 feet) : Nose dive as explained : - Airspeed .................................................................................... >135 knots - Fuel Tap .............................................................................................. open - Electric pump ........................................................................................... on - Throttle setting ......................................................................................... 1/2 - Magnetos ........................................................................................ "BOTH" If the motor does not start, plan to make a forced landing. 4.4. SMOKE AND FIRE 4.4.1. Fire on engine start Continue starting the engine (or leave it running if it is has already started) - Throttle setting ............................................................................. fully open - Electric fuel pump .................................................................................... off - Fuel tap............................................................................................. closed If the fire persists : - Magnetos ................................................................................................. off - Battery ..................................................................................................... off EVACUATE THE AIRCRAFT Page N°31 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 4.4.2. Airborne engine fire - Fuel tap............................................................................................. closed - Full throttle until the engine stops - Electric fuel pump .................................................................................... off - Cabin heating and ventilation ............................................................ closed - Airspeed ........................................................................................ 70 knots Prepare for a forced landing with an engine inoperative. 4.4.3. Cabin fire Extinguish the fire Open ventilation to eliminate the smoke. In case of an electrical fire (recognised by the smell of burning insulation) : - Reduce cabin ventilation - Battery ..................................................................................................... off LAND QUICKLY 4.5. GLIDING Recommended air speed,......................................................................... 70 knots Flaps ................................................................................................................... 0° Glide ratio ......................................................................................................... 13.4 4.6. FORCED LANDING 4.6.1. Planned forced landing with engine stopped Choose a suitable site - Best glide ratio airspeed................................................................. 70 knots - Flaps ....................................................................... retracted / as required - Belt / Safety harness ............................................................................. tight - Electric fuel pump .................................................................................... off - Throttle setting .................................................................................. closed - Magnetos ................................................................................................. off - Fuel Tap ........................................................................................... closed - Battery ..................................................................................................... off Page N°32 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 4.6.2. Planned forced landing with engine running - Proceed as for a normal landing - Best glide ratio speed .................................................................... 70 knots - On final approach, unlock the canopy - Approach speed on final................................................................. 65 knots Prior to touchdown: - Magnetos ................................................................................................. off - Battery ..................................................................................................... off 4.7. RECOVERY FROM AN UNINTENTIONAL SPIN - Throttle ............................................................................................. reduce - Flaps .................................................................................................. retract - Rudder .................................................................. opposite spin direction - Elevator ....................................................................................... to neutral - Aileron ......................................................................................... to neutral 4.8. OTHER EMERGENCIES 4.8.1. Vibrations and erratic engine behaviour : likely causes. - Contaminated fuel .................................. switch on the electric fuel pump - Ignition : magneto switch ....................................................... "L", then "R", .......................................................... then return to "BOTH" Select the position that gives the smoothest running and land as soon as possible on the closest runway. 4.8.2. Oil feed malfunction If the oil pressure us low, look at the oil temperature If the oil temperature rises (into the red), do not touch the throttle but contact the closest airfield and prepare to make a forced landing. 4.8.3. Icing Avoid entering icing meteorological zones and change altitude. Set heating system to de-mist and/or apply carb heat (if equipped). 4.8.4. Electric generation failure Low battery warning light ...................................................................................... lit 4.8.5. Low voltage (voltmeter). Switch off all non-essential electrical equipment and fly to the nearest airfield and land. Page N°33 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 5. NORMAL PROCEDURES 5.1. INTRODUCTION This section provides with a list of standard checks and procedures to be used in normal flight conditions. Procedures applicable to the use and check of optional equipment should be found in the "Supplementary systems and equipment" section. 5.2. DAILY CHECK 1 CABIN - Seats ................................................................................................................ adjusted, locked - Safety harness attachments .......................................................................................... checked - Elastic (left and right side) .............................................................................................. in place - Flap control belt ..................................................................................................... in place, tight - Primary wing attachment pins ................................................................ in place, safety pinned - Front wing fixings............................................................................................... in place, secure - Rear wing fixings ............................................................................................... in place, secure - Pitot tube .................................................................................................................... connected - Controls ................................................................................................................................ free - Magneto contacts ............................................................................................................off / cut - Master (battery) switch ............................................................................................................on - Fuel level ....................................................................................................................... checked - Fuel tank ......................................................................................................... check actual level - Fuel filler cap ......................................................................................................in place, locked - Master (battery) switch ............................................................................................................off - Documentation ........................................................................................ all present and correct - Weight and balance (including luggage) ....................................................................... checked - Canopy condition (clean) ............................................................................................... checked 2 FUSELAGE, LEFT SIDE - Static vent, ................................................................................................... clean, unobstructed - Antenna mounting ......................................................................................................... checked Watch out not to hurt yourself with antennas Page N°34 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 3 TAIL - Smooth, non-blemished surfaces .................................................................................. checked - Rudder ................................................ mounting / fixing / movement / cables / absence of play - Tailplane ........................................................... mounting / fixing / movement / absence of play - Control rod ......................................................................................................... in place, secure - Anti servo tab control ...................................................................................................... in place 4 FUSELAGE, RIGHT SIDE - Static vent .................................................................................................... clean, unobstructed - Antenna mounting ......................................................................................................... checked Watch out not to hurt yourself with antennas 5 RIGHT WING - Aileron and flap conditions and hinges .......................................................................... checked - Tightness to fuselage .................................................................................................... checked - Tightness & safety of front wheel and main undercarriage fairings and spats.............. checked - Wing tip condition and safety, navigation lights (where fitted) ....................................... checked - Main undercarriage......................................................................brakes / tyre inflation checked 6 ENGINE COWLS - Cowl fixing screws ......................................................................................................... checked - Air vents ...................................................................................................... clean, unobstructed - Propeller spinner ........................................................... screws checked, no play or looseness - Propeller ................................................................................................... clean, good condition - Oil level.......................................................................................................................... checked - Fuel drain : Check for absence of water and impurities................................. operate and check - Exhaust pipe ....................................................................................................... fixings checked - Fuel tank air vent (beneath fuselage) .......................................................... clean, unobstructed * To correctly determine the oil level it is necessary to remove and clean the dip stick before dipping and reading the level. 7 LEFT WING - Main undercarriage (left) ............................................. mounting, brakes, tyre inflation checked - Pitot ............................................................................................................. clean, unobstructed - Wing tip condition and security, navigation lights (where fitted) .................................... checked - Aileron and flap conditions and hinges .......................................................................... checked - Tightness to fuselage .................................................................................................... checked - Tightness & security of front wheel and main undercarriage fairings and spats ............ checked Page N°35 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 5.3. PRE-FLIGHT CHECK Repeat the daily inspection 5.4. NORMAL PROCEDURES AND CHECK-LISTS 5.4.1. Cabin check prior to engine start - Parking brake ............................................................................................... on - Flaps ................................................................................................. retracted - Seats ................................................................................................. adjusted - Rudder pedals.................................................................................... adjusted - Safety harness .................................................................................. tightened - Flight controls ...............................................................................full and free - Pitch trim operation .............. full fwd / aft range checked / take-off position - Canopy ............................................................................... closed not locked 5.4.2. Cold engine start (ROTAX) - Battery ......................................................................................................... on - Fuel tap ........................................................................ check function / open - Fuel Quantity .......................................................................................... noted - Electric fuel pump......................................................................................... on - Propeller ........................................................................... set minimum pitch - Throttle setting ............................................................................................. 1/4 - Choke ........................................................................................................ pull - Propeller area .......................................................................................... clear - Magneto contacts .................................................................................... BOTH - Starter ............................................................................. operate when ready As soon as the motor starts : - Choke ...................................................................................................... push - RPM ................................................................................................. 1 600 rpm - Oil pressure ............... within yellow sector in 10 sec. (4 bar for Rotax 912) - Battery voltage ................................................................................... checked - Canopy ................................................................................ locked / checked 5.4.3. Hot engine start - Battery ......................................................................................................... on - Fuel tap .................................................................................................... open - Fuel quantity ........................................................................................... noted - Propeller .....................................................................................full fine pitch - Throttle.................................................................................................. closed - Magnetos ................................................................................................ BOTH - Propeller area .......................................................................................... clear - Starter ............................................................................. operate when ready Page N°36 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 Then follow the procedure for starting when cold. 5.4.4. Taxiing Page N°37 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 - Parking brake ............................................................................................... off - Brakes................................................................................................ checked 5.4.5. Engine ground run - Parking brake ............................................................................................... on - Oil temperature and pressure .......................................... within green sector - RPM set to ....................................................................................... 3 850 rpm - Magneto contact ......................................................... "L", BOTH, "R", BOTH ....................................... max drop 300 rpm, max difference 100 rpm, checked - Reduce throttle setting ..................................................................... 1 600 rpm 5.4.6. Pre-take-off checks - Magneto contacts .................................................................................... BOTH - Controls ........................................................................................full and free - Cabin (canopy, harness) .................................................................... checked - Oil pressure and temperature .......................................... within green sector - Charge ............................................................................................... checked - Trim.................................................................................................... checked - Altimeter............................................................................................. checked - Fuel tap .................................................................................................... open - Fuel quantity ...................................................................................... checked - Electric fuel pump......................................................................................... on - Warning light panel ................................................................................... unlit - Flaps .............................. Check full extension, and set to take-off position - Compass............................................................................................ checked 5.4.7. Take-off - Minimum RPM at full throttle ............................................. 5 500 rpm checked - Take-off airspeed .................................................................................... 55 kts - Initial climb airspeed ....................................................................... Vx : 70 kts - Climb airspeed when clear of obstacles .......................................... Vy : 75 kts - Electric fuel pump @ 300 ft AAL .................................................................. off - Engine readings ................................................................................. checked - Warning light panel ................................................................................... unlit - Flaps ................................................................................................ Retracted 5.4.8. Climb Full throttle, maintain 75 kts I.A.S. until reaching 4000 ft AAL. Page N°38 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 5.4.9. Cruise See "Performance" section for rpm setting and performances. 5.4.10. Descent - Fuel tap .................................................................................................... open - Engine minimum rpm ....................................................................... 2 400 rpm 5.4.11. Approach - Cabin (harness) ........................................................................................ tight - Electric fuel pump......................................................................................... on - Flaps (under 90 kts) .......................................................................... extended - Warning light panel ................................................................................... unlit - Altimeter....................................................................................................... set - Brakes........................................................................................................ free 5.4.12. Final - Airspeed.................................................................................................. 65 kts 5.4.13. Go-Around - Airspeed........................................................................................... >70 knots - Flaps ................................................................................................. retracted - Climb airspeed ................................................................................... 75 knots 5.4.14. Post-landing checks - Flaps ................................................................................................. retracted - Electric fuel pump......................................................................................... off 5.4.15. Engine Stop - Parking brake ............................................................................................... on - Radio, Navigation and instruments............................................................... off - Magnetos .................................................................. cut-off test at 2000 rpm - Strobe light ................................................................................................... off - Magneto contact .......................................................................................... off - Battery ......................................................................................................... off Page N°39 / 47 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 17/10/2024 SE-AVIATION AIRCRAFT, AERODROME DE PONTARLIER,25300 PONTARLIER tel: 03 81 89 70 84 Ed 5 17/10/2024 Intentionally left blank

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