Dyn'Aéro MCR 4S Technische Daten
S.A.
19, rue de l'Aviation 21121 DAROIS FRANCE : (33) 03 80 35 60 62 Fax: (33) 03 80 35 60 63
DATE : 28/02/06
Exploitation REF: Q EX NO 07 00
MCR 4S FLIGHT
MANUAL
N° d'exemplaire
Edition de base:
Pages Date Rédigé par Visa Vérifié par Visa
39 30/04/01 N. BOUCHOUT C. BELIN
Mise à jour:
17 28/06/01 N. BOUCHOUT C. BELIN
(+1) ; 11-17
; 33-36 13/05/02 N. BOUCHOUT C. BELIN
13-14 ;18 05/03/03 N. BOUCHOUT C. BELIN
29-31 25/08/03 N. BOUCHOUT C. BELIN
38 19/04/04 N. BOUCHOUT C. BELIN
38 11/01/05 N. MAHUET C. BELIN
24-26 ;
30 ;31 27/01/05 N. BOUCHOUT C. BELIN
18 ,37 28/02/06 C. BELIN N. MAHUET
Dyn'Aéro S.A. 19, rue de l'Aviation 21121 DAROIS (33) 03 80 35 60 62 Fax: (33) 03 80 35 60 63 28/02/2006
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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.
Dyn'Aéro S.A. 19, rue de l'Aviation 21121 DAROIS (33) 03 80 35 60 62 Fax: (33) 03 80 35 60 63 28/02/2006
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1. FLIGHT MANUAL
Model : MCR 4S
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 NOTE 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 ACCORDNG TO FRENCH REGULATION.
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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
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1.2. LIST OF PAGES
Section Page Date Section Page Date
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1.3. TABLE OF CONTENTS
0. WARNING 2
1. FLIGHT MANUAL 3
1.1. REGISTRATION OF THE OVERHAULS 4
1.2. LIST OF PAGES 5
1.3. TABLE OF CONTENTS 6
2. GENERAL 9
2.1. INTRODUCTION 9
2.2. BASIS OF CERTIFICATION 9
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
3.5. ENGINE INSTRUMENT MARKINGS 18
3.6. INSTRUMENT MARKINGS 19
3.7. WEIGHT 19
3.8. WEIGHT & BALANCE 19
3.9. APPROVED MANOEUVRES 20
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 21
3.16.INSTRUMENT PANEL WEIGHT LIMITATION 21
3.17.SOLO FLIGHT 21
3.18.OTHER LIMITATIONS 21
3.19.PLACARDS 21
4. EMERGENCY PROCEDURES 23
4.1. INTRODUCTION 23
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4.2. ENGINE FAILURE 23
4.3. IN-FLIGHT RESTART 24
4.4. SMOKE AND FIRE 24
4.5. GLIDING 25
4.6. FORCED LANDING 25
4.7. RECOVERY FROM AN UNINTENTIONAL SPIN 26
4.8. OTHER EMERGENCIES 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
6. PERFORMANCES 33
6.1. INTRODUCTION 33
6.2. APPROVED DATA 33
7. WEIGHT & BALANCE 35
7.1. INTRODUCTION 35
7.2. WEIGHT & BALANCE REGISTRATION AND LOADING ENVELOPE 35
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
8.5. CLEANING AND TREATMENT 38
8.6. DE-RIGGING AND RIGGING 38
9. SUPPLEMENTARY SYSTEMS AND EQUIPMENTS 39
9.1. INTRODUCTION 39
9.2. MINIMUM EQUIPMENT LIST 39
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 4S 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:
Attracts the 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 4S
Cantilever low-mounted wing.
Carbon structure and wing skin with control surface skins made in light alloy.
Engine and Propeller
Span 8.66 m
Wing surface 8.15 m²
Aspect ratio 9.2
Cabin width 1.17 m
Fuel capacity 2 x 60 l
Overall Length 6.72 m
Height 1.95 m
2.5. CONTROL SURFACE DEFLECTION
Ailerons : - 20° (±1) trailing edge upwards
+10° (±1) trailing edge downwards
Flaps : 0-30° (+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
Inhaltsverzeichnis
Andere Dyn'Aéro Flugzeug Handbücher
