Dyn'Aéro MCR 01 VLA Flight Manual Download

Page: 29 / 39

Dyn'Aéro

17, rue de St Exupéry 64230 Sauvagnon



(33) 05 59 33 18 74 [email protected]

10/10/2013

MEXNO07

100

MCR

SPORTSTER

FLIGHT MANUAL

MAJ

[12/02/02]

Page N°29 /

5.3.

-F

LIGHT CHECK

Repeat the daily inspection

5.4.

ORMAL PROCEDURES AND CHECK

LISTS

5.4.1. Cabin check prior to engine start

Parking brake ..............................................................................................

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 .........................................................................................................

Fuel tap

...........................................................

check function / open

Fuel Quantity ......................................................................................

noted

Electric fuel pump ........................................................................................

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

...........................................................................................

Fuel tap

.......................................................................................

open

Fuel quantity

......................................................................................

noted

Propeller .....................................................................................

full fine pitch

Throttle

....................................................................................

closed

Magnetos

......................................................................................

BOTH

Propeller area .......................................................................................

clear

Starter

..............................................................

operate when ready

Then follow the procedure for starting when cold.

5.4.4. Taxiing

Summary of Contents for MCR 01 VLA

Page 1: ... 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 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 100 HP MCR SPORTSTER FLIGHT MANUAL ...

Page 2: ...tact dyn aero 10 10 2013 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 ...

Page 3: ...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 INFORMIN...

Page 4: ...cept 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 insert...

Page 5: ...MITATIONS 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 S ENGINE 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 S ENGINE 18 3 5 2 ROTAX 914 ENGINE 18 3 6 INSTRUMENT MARKINGS 19 3 7 WEIGHT 19 3 8 WEIGHT BALANCE 19 3 9...

Page 6: ...INE 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 STOPPED 25 4 6 2 PLANNED FORCED LANDING WITH ENGINE RUNNING 26 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 GENER...

Page 7: ...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 AIR...

Page 8: ...Dyn Aéro 17 rue de St Exupéry 64230 Sauvagnon 33 05 59 33 18 74 contact dyn aero 10 10 2013 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 12 02 02 Page N 8 39 Intentionally left blank ...

Page 9: ...ns 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...

Page 10: ...S 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 m 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 ...

Page 11: ...Dyn Aéro 17 rue de St Exupéry 64230 Sauvagnon 33 05 59 33 18 74 contact dyn aero 10 10 2013 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 12 02 02 Page N 11 39 2 6 THREE VIEW DIAGRAM ...

Page 12: ...Dyn Aéro 17 rue de St Exupéry 64230 Sauvagnon 33 05 59 33 18 74 contact dyn aero 10 10 2013 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 12 02 02 Page N 12 39 Intentionally left blank ...

Page 13: ...oved 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 con...

Page 14: ...ed 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 a...

Page 15: ...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 Ro...

Page 16: ...er Head Temperature 135 C 275 F Maximum Oil Temperature 130 C 266 F Oil pressure Minimum 1 5 Bar Maximum 7 Bars Fuel pressure 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 3 4 2 MT Propeller Propeller manufacturer MT Propeller Propeller model MTV 7 A 156 122 Type Three bladed electrical variable ...

Page 17: ... Maximum Propeller rotation speed 2400 rpm Torque 4 6 daN m 3 4 3 MT fixed pitch Propeller to be used with Rotax 912S engine only Propeller manufacturer MT Propeller Propeller model MT 156 220 2M Type Two bladed fixed pitch propeller Propeller diameter 1 56 m Reference pitch setting 75 of propeller radius normal 220 mm Maximum allowed propeller rotation speed 2400 rpm Torque 1 6 daN m Tighten prop...

Page 18: ...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 3 5 2 Rotax 914 Engine ROTAX 914 Red line Green sector Yellow sector Red Line Instrument Units Minimum Normal Warning Maximum Limit Range Range Limit Tachometer Tr Min 1500 to 5500 5500 to 5800 58...

Page 19: ...uilder 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 M A C 800 mm reference datum 13 5 mm ahead of left wing leading edge 3 9 APPROVED MANOEUVRES 250 300 350 400 450 500 10 15 20 25 30 35 40 45 50 Balance ratio compared to ...

Page 20: ...NOEUVRING 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 ge...

Page 21: ... that both pilots can easily read it the following placard THE COMPLIANCE OF THIS AICRAFT WITH A CERTIFICATE OF AIRWORTHINES HAS NOT BEEN DEMONSTRATED USE FOR HIRE OR REWARD PROHIBITED AEROBATIC FLIGHT AND INTENTIONAL SPINS ARE PROHIBITED MANOEUVRING SPEED 127 KTS 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...

Page 22: ...Dyn Aéro 17 rue de St Exupéry 64230 Sauvagnon 33 05 59 33 18 74 contact dyn aero 10 10 2013 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 12 02 02 Page N 22 39 Oil tank filler Oil tank 3 5 l 10 W 40 ...

Page 23: ...e 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...

Page 24: ...or 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 engi...

Page 25: ...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 ai...

Page 26: ...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...

Page 27: ...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 ...

Page 28: ...n 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 beneat...

Page 29: ...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...

Page 30: ...acts 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 ...

Page 31: ...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 Magne...

Page 32: ...Dyn Aéro 17 rue de St Exupéry 64230 Sauvagnon 33 05 59 33 18 74 contact dyn aero 10 10 2013 MEXNO07 100 HP MCR SPORTSTER FLIGHT MANUAL MAJ 12 02 02 Page N 32 39 Intentionally left blank ...

Page 33: ...ds stall speeds take off performance and supplementary non approved information The information given in the diagrams was obtained from flight tests with an aircraft and an engine in good condition and in the hands of an average pilot 6 2 APPROVED DATA 6 2 1 Airspeed indicator calibration V Vi 1 1 6 knots 6 2 2 Stalling speed knots m 490 Kg Flaps 0 10 25 Bank angle 0 64 56 49 30 68 59 52 60 90 79 ...

Page 34: ... 2 5 Take off distances calculation Take off distances must be increased by 20 on a grass strip 40 on a wet runway take off only They must be reduced by 10 for each 10 kts head wind step They can be computed for intermediary masses by considering a 2 5 change for each 10 kg step 6 2 6 Effect of rain and insects on aircraft performance flying and handling qualities Decrease the performances by 4 6 ...

Page 35: ...aft can be safely operated Weighing and balance calculation procedures and a complete list of the equipment available especially those mounted for weighing on the aircraft are included in the maintenance manual 7 2 WEIGHT BALANCE REGISTRATION AND LOADING ENVELOPE 7 2 1 Loading envelope M A C 800 mm Reference datum 13 5 mm ahead of left wing leading edge 250 300 350 400 450 500 10 15 20 25 30 35 40...

Page 36: ...d with the actual empty weight and moment arm of the Aircraft Also update if possible the actual moment arms of movable weight by weighing your Aircraft refer to MBENOPP Weighing procedure Calculation method Note movable weights in fill above chart shaded boxes Compute total mass Multiply weights and corresponding moment arms and note the results in Moment column Compute the moment sum Divide the ...

Page 37: ... inspection requirements which must be fulfilled in order to ensure performance and reliability of a new aircraft According to the environment and flight conditions a lubrication and maintenance schedule must be applied 8 2 AIRCRAFT MAINTENANCE SCHEDULE Advised inspections 50 hours 6 months 100 hours 1 year 1 000 hours 2 years 2 000 hours 6 years RESPECT THE MAINTENANCE MANUAL SCHEDULE MEXNO03 8 3...

Page 38: ... Canopy cover advised Main landing gear wheels choked 8 4 1 Ground fixing The aircraft can be secured to the ground from the wheels Wing attach fittings using 6 mm diameter captive nut can also be installed 8 5 CLEANING AND TREATMENT Regularly clean all control surfaces and the inside of the aircraft Cleaning products must be suitable for surfaces to be cleaned Check product before each canopy cle...

Page 39: ...with the following optional systems and equipment that are not delivered with the standard aircraft list to be completed by the assembler 9 2 MINIMUM EQUIPMENT LIST Flight instruments Air speed indicator Altimeter Magnetic compass Ball bank indicator Engine instruments Tachometer Oil temperature Oil pressure Cylinder head temperature Fuel level indicator Oil level indicator 9 3 LIST OF THE SUPPLÉM...

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