Dyn'Aéro Sportster Technical specifications

17, rue de St Exupéry 64230 Sauvagnon FRANCE : (33) 05 59 33 18 74 [e-mail]
DATE :10/10/13
Operation REF: M EX NO 07 00
Serial number :
First issue:
Pages Date Written by Visa Checked by Visa
35 29/08/00 N. BOUCHOUT C. BELIN
Up-dates :
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+ garde 12/02/02 C. BELIN N. BOUCHOUT
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100 HP MCR SPORTSTER
FLIGHT MANUAL

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MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ [12/02/02] Page N°2 / 39
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.

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MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ [12/02/02] Page N°3 / 39
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:
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.

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MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ [12/02/02] Page N°4 / 39
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

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MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ [12/02/02] Page N°5 / 39
1.3. TABLE OF CONTENTS
Contenu
0. WARNING 2
1. FLIGHT MANUAL 3
1.1. REGISTRATION OF THE OVERHAULS 4
1.2. LIST OF PAGES 4
1.3. TABLE OF CONTENTS 5
2. GENERAL 9
2.1. INTRODUCTION 9
2.2. BASIS OF CERTIFICATION9
2.3. WARNINGS,ALARMS AND NOTES 9
2.4. SPECIFICATIONS 10
2.5. CONTROL SURFACE DEFLECTION 10
2.6. THREE VIEW DIAGRAM 11
3. LIMITATIONS 13
3.1. INTRODUCTION 13
3.2. AIRSPEED 13
3.3. INDICATED AIRSPEED INSTRUMENTS MARKINGS 14
3.4. ENGINE INSTALLATION 15
3.4.1. ROTAX 912 SENGINE 15
3.4.2. MT PROPELLER 16
3.4.3. MT FIXED PITCH PROPELLER TO BE USED WITH ROTAX 912S ENGINE ONLY 17
3.5. ENGINE INSTRUMENT MARKINGS 18
3.5.1. ROTAX 912 SENGINE 18
3.5.2. ROTAX 914 ENGINE 18
3.6. INSTRUMENT MARKINGS 19
3.7. WEIGHT 19
3.8. WEIGHT &BALANCE 19
3.9. APPROVED MANOEUVRES 19
3.10. MANOEUVRING LOAD FACTOR 20
3.11. MINIMUM FLIGHT CREW 20
3.12. TYPES OF FLIGHT 20
3.13. FUEL 20
3.14. MAXIMUM NUMBER OF SEATS 20
3.15. TIRE PRESSION 20
3.16. INSTRUMENT PANEL WEIGHT LIMITATION 20
3.17. SOLO FLIGHT 21
3.18. OTHER LIMITATIONS 21
3.19. PLACARDS 21

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3.19.1. DURING INITIAL EXPERIMENTATION PERIOD 21
3.19.2. IN FRONT OF PILOT VIEW21
3.19.3. AIR SPEED INDICATOR 21
3.19.4. ENGINE INSTALLATION INSTRUMENTS 21
3.19.5. CONTROL SYSTEM MARKINGS 21
3.19.6. MISCELLANEOUS PLACARDS AND MARKINGS 21
4. EMERGENCY PROCEDURES 23
4.1. INTRODUCTION 23
4.2. ENGINE FAILURE 23
4.2.1. ENGINE FAILURE ON TAKE-OFF RUN 23
4.2.2. ENGINE FAILURE IMMEDIATELY AFTER TAKE-OFF 23
4.3. IN-FLIGHT RESTART 24
4.3.1. STARTER MOTOR RESTART 24
4.3.2. DIVE RESTART 24
4.4. SMOKE AND FIRE 24
4.4.1. FIRE ON ENGINE START 24
4.4.2. AIRBORNE ENGINE FIRE 25
4.4.3. CABIN FIRE 25
4.5. GLIDING 25
4.6. FORCED LANDING 25
4.6.1. PLANNED FORCED LANDING WITH ENGINE STOPPED25
4.6.2. PLANNED FORCED LANDING WITH ENGINE RUNNING26
4.7. RECOVERY FROM AN UNINTENTIONAL SPIN 26
4.8. OTHER EMERGENCIES 26
4.8.1. VIBRATIONS AND ERRATIC ENGINE BEHAVIOUR :LIKELY CAUSES. 26
4.8.2. OIL FEED MALFUNCTION 26
4.8.3. ICING 26
4.8.4. ELECTRIC GENERATION FAILURE 26
4.8.5. LOW VOLTAGE (VOLTMETER). 26
5. NORMAL PROCEDURES 27
5.1. INTRODUCTION 27
5.2. DAILY CHECK 27
5.3. PRE-FLIGHT CHECK 29
5.4. NORMAL PROCEDURES AND CHECK-LISTS 29
5.4.1. CABIN CHECK PRIOR TO ENGINE START 29
5.4.2. COLD ENGINE START (ROTAX) 29
5.4.3. HOT ENGINE START 29
5.4.4. TAXIING 29
5.4.5. ENGINE GROUND RUN 30
5.4.6. PRE-TAKE-OFF CHECKS 30
5.4.7. TAKE-OFF 30
5.4.8. CLIMB 30
5.4.9. CRUISE 31
5.4.10. DESCENT 31
5.4.11. APPROACH 31
5.4.12. FINAL 31
5.4.13. GO-AROUND 31

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5.4.14. POST-LANDING CHECKS 31
5.4.15. ENGINE STOP 31
6. PERFORMANCES 33
6.1. INTRODUCTION 33
6.2. APPROVED DATA 33
6.2.1. AIRSPEED INDICATOR CALIBRATION 33
6.2.2. STALLING SPEED (KNOTS) 33
6.2.3. TAKE-OFF PERFORMANCES (ROTAX 912 S100 HP) 34
6.2.4. LANDING DISTANCES 34
6.2.5. TAKE-OFF DISTANCES CALCULATION 34
6.2.6. EFFECT OF RAIN AND INSECTS ON AIRCRAFT PERFORMANCE,FLYING AND HANDLING QUALITIES. 34
6.2.7. CROSS-WIND DEMONSTRATED PERFORMANCES 34
6.2.8. NOISE LIMITATIONS 34
7. WEIGHT & BALANCE 35
7.1. INTRODUCTION 35
7.2. WEIGHT &BALANCE REGISTRATION AND LOADING ENVELOPE 35
7.2.1. LOADING ENVELOPE 35
7.2.2. WEIGHT &BALANCE PROCEDURE 36
8. AIRCRAFT OPERATION, SERVICING AND MAINTENANCE 37
8.1. INTRODUCTION 37
8.2. AIRCRAFT MAINTENANCE SCHEDULE 37
8.3. AIRCRAFT MODIFICATIONS AND REPAIRS 37
8.4. PARKING 38
8.4.1. GROUND FIXING 38
8.5. CLEANING AND TREATMENT38
9. SUPPLEMENTARY SYSTEMS AND EQUIPMENTS 39
9.1. INTRODUCTION 39
9.2. MINIMUM EQUIPMENT LIST39
9.3. LIST OF THE SUPPLÉMENTARY SYSTEMS AND EQUIPMENTS 39
9.4. SUPPLEMENTARY ELEMENTS DESCRIPTIONS 39

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Intentionally left blank

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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 in accordance with the regulations
applicable to kit aircraft, including the amendment and the certificate of
restricted Airworthiness N° has been issued on the .
Category of Airworthiness : Restricted (kit)
Basis of certification and/or acceptance:
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.

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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