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Dyn'Aéro MCR 4S Flight Manual

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19, rue de l'Aviation 21121 DAROIS FRANCE
Exploitation
N° d'exemplaire
Edition de base:
Pages
Date
39
30/04/01
Mise à jour:
17
28/06/01
(+1) ; 11-17
13/05/02
; 33-36
13-14 ;18
05/03/03
29-31
25/08/03
38
19/04/04
38
11/01/05
24-26 ;
27/01/05
30 ;31
18 ,37
28/02/06
D
: 28/02/06
ATE
MCR 4S FLIGHT
MANUAL
Rédigé par
N. BOUCHOUT
N. BOUCHOUT
N. BOUCHOUT
N. BOUCHOUT
N. BOUCHOUT
N. BOUCHOUT
N. MAHUET
N. BOUCHOUT
C. BELIN
S.A.
: (33) 03 80 35 60 62 Fax: (33) 03 80 35 60 63
Visa
Vérifié par
C. BELIN
C. BELIN
C. BELIN
C. BELIN
C. BELIN
C. BELIN
C. BELIN
C. BELIN
N. MAHUET
REF: Q EX NO 07 00
Visa

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  • Page 1 S.A. 19, rue de l'Aviation 21121 DAROIS FRANCE : (33) 03 80 35 60 62 Fax: (33) 03 80 35 60 63 Exploitation REF: Q EX NO 07 00 MCR 4S FLIGHT MANUAL N° d'exemplaire Edition de base: Pages Date Rédigé...
  • Page 2 0. W ARNING HIS DOCUMENT IS PROVIDED FOR INFORMATION ONLY T IS THE OWNER RESPONSABILITY CHECK THE EXACTNESS OF THE PRESENT MATERIAL WITH RESPECT ACTUAL AIRCRAFT Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°2 /...

  • Page 3: Flight Manual

    REGULATIONS AND INFORMING ANY PASSENGER OF THE LIMITATIONS OF THE AIRCRAFT WITH RESPECT TO ITS AIRWORTHINESS LIMITATIONS HIS FLIGHT MANUAL WAS ESTABLISHED ACCORDNG TO FRENCH REGULATION Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°3 /...

  • Page 4: Registration Of The Overhauls

    N° of the amendment and the date will be indicated on the bottom left corner of the page. Revision Affected Affected Date Approval Date Date of Signed N° section pages insertion Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°4 /...

  • Page 5: List Of Pages

    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 1.2. IST OF PAGES Section Page Date Section Page Date Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°5 /...

  • Page 6: Table Of Contents

    3.15. T IRE PRESSION 3.16. I NSTRUMENT PANEL WEIGHT LIMITATION 3.17. S OLO FLIGHT 3.18. O THER LIMITATIONS 3.19. P LACARDS MERGENCY PROCEDURES 4.1. I NTRODUCTION Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°6 /...
  • Page 7 UPPLEMENTARY SYSTEMS AND EQUIPMENTS 9.1. I NTRODUCTION 9.2. M INIMUM EQUIPMENT LIST 9.3. L IST OF THE SUPPLÉMENTARY SYSTEMS AND EQUIPMENTS 9.4. S UPPLEMENTARY ELEMENTS DESCRIPTIONS Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°7 /...
  • Page 8 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 Intentionally left blank Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°8 /...

  • Page 9: Warning

    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.

  • Page 10: Specifications

    Flaps : 0-30° (-0+5) Rudder : 20° in both directions (left and right) (+0-2) Tailplane : - 10° trailing edge upwards (-0+1) +3.5° trailing edge downwards Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°10 /...

  • Page 11: Three View Diagram

    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 2.6. HREE VIEW DIAGRAM Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°11 /...
  • Page 12 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 Intentionally left blank Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°12 /...

  • Page 13: Limitations

    Aircraft might be exposed to excessive loads. VFE Maximum speed allowed with flaps 160 km/h Do not exceed this Velocity with Flaps Extended extended 86 kts Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°13 /...

  • Page 14: Ndicated Airspeed Instruments Markings

    Manoeuvres must be carried out with caution and (131 / 165 kts) only in conditions of calm air Red segment (306 km/h) Maximum speed for all operations (165 kts) Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°14 /...

  • Page 15: Engine Installation

    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 Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°15 /...
  • Page 16 Minimum: pression admission + 0.15 Bar Maximum: pression admission + 0.35 Bar Octane grade of fuel: Refer to Rotax manual Oil quality: Refer to Rotax manual Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°16 /...
  • Page 17 Two-bladed, hydraulic variable pitch Propeller diameter 1.70 m Reference pitch setting (75% of propeller radius) normal: variable pitch Maximum allowed propeller rotation speed 2400 rpm Torque 4.6 daN.m Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°17 /...

  • Page 18: Ngine Instrument Markings

    0.8 - 2 2 - 5 5 - 7 Fuel Quantity Litre 2x60 Note carefully : Do not switch off the main switch before turning off the engine. Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°18 /...

  • Page 19: Instrument Markings

    664 kg 3.8. & B EIGHT ALANCE Centre of Gravity range 15/42% M.A.C. Datum Centrage (m) M.A.C. = 960 mm ; reference datum : wing leading-edge. Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°19 /...

  • Page 20: Approved Manoeuvres

    3.13. F Total fuel 120 l Useable fuel 118 l Unusable fuel Fuel Octane grade approved: Refer to Rotax manual 3.14. M AXIMUM NUMBER OF SEATS Four Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°20 /...

  • Page 21: Tire Pression

    SE FOR HIRE OR REWARD PROHIBITED EROBATIC FLIGHT AND INTENTIONAL SPINS ARE PROHIBITED ANOEUVRING SPEED 3.19.3. Air speed indicator Each air speed indicator must be marked as indicated in paragraph 4.3 Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°21 /...
  • Page 22 Fuel tank filler : "Fuel tank : 2 x 60 l Mini fuel grade : RON 95" Oil tank filler "Oil tank : 3.5 l 10 W 40" Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°22 /...

  • Page 23: Mergency Procedures

    ................. 92 knots Fuel tap ..................closed Magnétos ..................OFF Flaps ................as required Battery ..................OFF Never attempt to make a U turn to return to the runway. Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°23 /...

  • Page 24: I N - Flight Restart

    Throttle setting................fully open Electric fuel pump ..................off Fuel tap ..................closed If the fire persists : Magnetos ................... off Battery ................... off EVACUATE THE AIRCRAFT Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°24 /...

  • Page 25: Gliding

    Flaps ..............retracted / as required Belt / Safety harness ................tight Electric fuel pump ..................off Throttle setting.................. closed Magnetos ................... off Fuel Tap ..................closed Battery ................... off Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°25 /...

  • Page 26: Recovery From An Unintentional Spin

    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. Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°26 /...

  • Page 27: Normal Procedures

    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 Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°27 /...
  • Page 28 Aileron and flap conditions and hinges ................. checked Tightness to fuselage....................checked Tightness & security of front wheel and main undercarriage fairings and spats ..checked Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°28 /...

  • Page 29: Pre -Flight Check

    Electric fuel pump ..................on Fuel quantity ..................noted Propeller ..................full fine pitch Throttle ..................closed Magnetos ..................BOTH Propeller area ..................clear Starter .............. operate when ready Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°29 /...
  • Page 30 Electric fuel pump @ 300 ft AAL..............off Engine readings................. checked Warning light panel................... unlit Flaps ................Retracted 5.4.8. Climb Full throttle, maintain 92 kts I.A.S. until reaching 4000 ft AAL. Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°30 /...
  • Page 31 Parking brake ................... on Radio, Navigation and instruments.............. off Magnetos ............cut-off test @ 2000 rpm Strobe light ................... off Magneto contact ..................off Battery ................... off Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°31 /...
  • Page 32 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 Intentionally left blank Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°32 /...

  • Page 33: Performances

    6.2.2. Stalling speed (knots) Flaps 0° 17° 30° Bank angle 0 ° 30 ° 60 ° Flaps 0° 17° 30° Bank angle 0 ° 30 ° 60 ° Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°33 /...
  • Page 34 Decrease the performances by 4% 6.2.7. Cross-wind demonstrated performances 20 kts 6.2.8. Noise limitations Noise certificate is not required for aircraft with certificate of restricted Airworthiness. Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°34 /...

  • Page 35: Weight & Balance

    ALANCE REGISTRATION AND LOADING ENVELOPE 7.2.1. Loading envelope : 0.100 0.150 0.200 0.250 0.300 0.350 0.400 0.450 Centrage (m) M.A.C. = 960 mm ; reference datum : wing leading-edge. Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°35 /...
  • Page 36 • Divide the moment sum by the total weight. The result gives the location in meter of the actual Aircraft center of gravity. • Check the computed moment arm is within the weight and balance envelope shown on previous page. Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°36 /...

  • Page 37: Aircraft Operation , Servicing And Maintenance

    ESPECT MAINTENANCE MANUAL SCHEDULE 8.3. IRCRAFT MODIFICATIONS AND REPAIRS The Airworthiness authorities and the manufacturer must be informed before all modification or repair, which can change the aircraft Airworthiness. Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°37 /...

  • Page 38: Parking

    You may have to disassemble the wings and the tailplane, to store the plane, or to carry out a maintenance check. In such a case, please refer to the document QEXNO12 : MCR-4S DE-RIGGING / RIGGING PROCEDURE. Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°38 /...

  • Page 39: Upplementary Systems And Equipments

    Fuel level indicator Oil level indicator 9.3. IST OF THE SUPPLÉMENTARY SYSTEMS AND EQUIPMENTS Date Document N° Title of the supplementary element 9.4. UPPLEMENTARY ELEMENTS DESCRIPTIONS Q EX NO 07 00 MCR 4S FLIGHT MANUAL [MAJ 28/02/06] Page N°39 /...

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