Dyn'Aéro MCR ULC ECOLIGHT HB-WAZ Technical specifications

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19, RUE DE L’AVIATION
F21121 DAROIS
FRANCE
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Ref : N EX NO 09 01
MCR ULC ECOLIGHT
Aircraft Flight Manual
3rd Edition – 2009/08/20

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THIS PLANE MUST ALWAYS BE USED IN ACCORDANCE WITH THE INFORMATION AND LIMITATIONS CONTAINED
IN THIS DOCUMENT.
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.
BUILDERS:DYN’AERO FRANCE

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THIS MANUAL BELONGS TO THE AIRCRAFT:HB-WAZ S/N: 363
0.1. REGISTRATION OF THE REVISIONS
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.
Revision
N°
Affected
section
Affected
pages
Date
Approval
Date
Date of
insertion
Signed

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0.2. TABLE OF CONTENTS
0.1. REGISTRATION OF THE REVISIONS 5
0.2. TABLE OF CONTENTS 6
1. GENERAL 9
1.1. INTRODUCTION 9
1.2. CERTIFICATION BASIS 9
1.3. WARNINGS,CAUTIONS AND NOTES 9
1.4. DESCRIPTIVE DATA 10
1.5. THREE VIEW DRAWING 10
2. LIMITATIONS 11
2.1. INTRODUCTION 11
2.2. AIRSPEED 11
2.3. AIRSPEED INDICATOR MARKINGS 11
2.4. POWER PLANT 12
2.5. POWER PLANT INSTRUMENT MARKINGS 13
2.6. MISCELLANEOUS INSTRUMENT MARKINGS 13
2.7. WEIGHT 13
2.8. CENTRE OF GRAVITY 14
2.9. APPROVED MANOEUVRES 14
2.10. MANOEUVRING LOAD FACTOR 14
2.11. FLIGHT CREW 15
2.12. KINDS OF OPERATION 15
2.13. FUEL 15
2.14. MAXIMUM NUMBER OF SEATS 15
2.15. OTHER LIMITATIONS 16
2.16. PLACARDS 16
3. EMERGENCY PROCEDURES 19
3.1. INTRODUCTION 19
3.2. ENGINE FAILURE 19
3.3. AIR START 20
3.4. SMOKE AND FIRE 20
3.5. GLIDE 21
3.6. LANDING EMERGENCIES 21
3.7. RECOVERY FROM UNINTENTIONAL SPIN 22
3.8. PARACHUTE RESCUE SYSTEM OPERATION (IF FITTED). 22
3.9. OTHER EMERGENCIES 22
4. NORMAL PROCEDURES 26
4.1. INTRODUCTION 26
4.2. DAILY INSPECTION 26
4.3. PRE-FLIGHT INSPECTION 28
4.4. NORMAL PROCEDURES AND CHECK LIST 28

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5. PERFORMANCES 31
5.1. INTRODUCTION 31
5.2. APPROVED DATA 31
5.3. ADDITIONAL INFORMATION34
6. WEIGHT &BALANCE 35
6.1. INTRODUCTION 35
6.2. WEIGHT &BALANCE REGISTRATION AND LOADING ENVELOPE 35
6.1. EQUIPEMENT LIST 38
7. AIRCRAFT AND SYSTEMS DESCRIPTION 40
7.1. INTRODUCTION 40
7.2. AIRFRAME 40
7.3. FLIGHTS CONTROLS 40
7.4. INSTRUMENT PANEL 41
7.5. LANDING GEAR SYSTEM 42
7.6. SEATS AND SAFETY HARNESS 42
7.7. BAGGAGE COMPARTMENT 42
7.8. CANOPY 42
7.9. POWER PLANT 42
7.10. FUEL SYSTEM 43
7.11. ELECTRICAL SYSTEM 44
7.12. PITOT AND STATIC PRESSURE SYSTEMS 46
7.13. MISCELLANEOUS EQUIPMENT 46
7.14. AVIONICS 46
8. AEROPLANE HANDLING,SERVICING AND MAINTENANCE48
8.1. INTRODUCTION 48
8.2. RIGGING AND DERIGGING 48
8.3. AIRCRAFT MAINTENANCE SCHEDULE 49
8.4. AIRCRAFT MODIFICATIONS AND REPAIRS 49
8.5. GROUND HANDLING 49
8.6. CLEANING AND TREATMENT49
9. SUPPLEMENTARY SYSTEMS AND EQUIPMENTS 50
9.1. INTRODUCTION 50
9.2. LIST OF THE SUPPLÉMENTARY SYSTEMS AND EQUIPMENTS 50
9.3. SUPPLEMENTARY ELEMENTS DESCRIPTIONS 50
10. SUPPLEMENT AEROTOW 51
10.1. PRELIMINARY LIMITATIONS: 51
10.2. GENERAL 51
10.3. LIMITATIONS 51
10.4. EMERGENCY PROCEDURES 51
10.5. NORMAL PROCEDURES 52
10.6. PERFORMANCES 52
10.7. AIRCRAFT AND SYSTEMS DESCRIPTION 53

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10.8. CARE AND MAINTENANCE 54
10.9. PLACARDS 54
11. SUPPLEMENT EDIATEC FLARM ECW 100 55
12. SUPPLEMENT TOW CABLE RETRACTOR WINCH TOST 62

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1. GENERAL
1.1. 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's that are imperative to be given to the MCR ULC
ECOLIGHT pilot. It also contains supplementary information given by the builder.
1.2. CERTIFICATION BASIS
This aircraft was approved by ____________________________________
Category of Airworthiness: ECOLIGHT
Basis of acceptance: LTF UL 2003
Noise certification basis: ICAO Annex 16, Chapter 10
1.3. WARNINGS,CAUTIONS AND NOTES
The following definitions apply to Warnings, Alarms & Notes used in the flight manual.
WARNING:
Means that a failure to observe the corresponding procedures will lead to an immediate or important
deterioration of the flight safety.
CAUTION:
Means that a failure to observe the corresponding procedures will lead to a minor or major
deterioration of the long term flight safety.
NOTE:
Draws attention to a condition which although not particularly related to the flight safety is important
or unusual.

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1.4. DESCRIPTIVE DATA
Kit aircraft of the type : Dyn'Aéro MCR ULC
Cantilever low-mounted wing, fixed gear.
Flying tail.
2 seats.
Carbon structure.
Engine: From Rotax 912 to 914 (Only 914 will be described here, each other engine (912 and 912S) will be added as soon as it equips an aircraft.)
Propeller: Dyn’Aero-Prop two/three-blades, fix or variable pitch.
Span 8.62 m
Wing surface 8.31 m²
Aspect ratio 9.02
Wing loading
54.5
kg/ m²
Cabin width
1.12
m
Fuel capacity 72 l
Overall Length 5.53 m
Height 1.53 m
MAC 22/40 %
1.5. THREE VIEW DRAWING