FlySynthesis STORCH CLASSIC Especificaciones técnicas

TWO-SEATERS ULTRALIGHT AIRCRAFT

STORCHCLASSIC

ENGINE JABIRU 2200

FLIGHT MANUAL

REV.0

Flight manual

Storch Classic Jabiru

Rev. 0 –07/2002 Pag. 2

STORCH CL FLIGHT MANUAL N° ........

THIS FLIGHT MANUAL IS SUPPLIED WITH ULTRA LIGHT AIRCRAFT STORCH CL

N°…………… AND MUST BE KEPT ON BOARD AT ALL TIMES.

PILOT MUST BE AWARE OF ALL “NORMAL” AND “EMERGENCY” PROCEDURES

IN ADDITION TO THE AIRCRAFT LIMITATIONS REPORTED IN THIS MANUAL.

ALL THESE INFORMATION ARE NECESSARY FOR SAFE OPERATION OF THE

AIRCRAFT.

THE FOLLOWING IS THE DATA SHEET FOR THIS PARTICULAR AIRCRAFT

AIRCRAFT.: .....................................................................................STORCH

MODEL:......................................................................................................CL

ENGINE TYPE:..........................................................................JABIRU 2200

BUILDER:.................................................................FLY SYNTHESIS S.R.L.

EDITION:.......................................................................................JULY 2002

AIRCRAFT DATA:

-SERIAL NUMBER ........................................................................................................................

-DATE OF MANUFACTURE .....................................................................................................

-EMPTY WEIGHT (TESTED) ..................................................................................................KG

-FUEL WEIGHT (WITH LIT....)................................................................................................KG

-ALLOWED WEIGHT FOR LUGGAGE ...............................................................................KG

INSTALLED ACCESSORIES (COUNTED IN EMPTY WEIGHT)

----------------------------------------------------------------------------

Flight manual

Storch Classic Jabiru

Rev. 0 –07/2002 Pag. 3

LOG OF REVISIONS

All the revisions to this manual, excluding data concerning weight

and load tests, must be registered in the following table and, in

case of approved sections, signed and stamped from CAAI.

Rev.

Nr.

Chapter Pages

affected

Date

Approval

Date Date of

modify

Signature

Flight manual

Storch Classic Jabiru

Rev. 0 –07/2002 Pag. 4

LOG OF PAGES

Chapter Pages Date Chapter Pages Date

Flight manual

Storch Classic Jabiru

Rev. 0 –07/2002 Pag. 5

INTRODUCTION

This Flight Manual contains all the information necessary for a Correct and SAFE use of the two

seats ultra light

STORCH CL

Such information includes:

Procedures to prepare aircraft for flight;

Normal Procedures;

Emergency Procedures;

Limitations;

Flight performances;

Adherence to these procedures is MANDATORY for the aircraft operator.

FLY SYNTHESIS Srl is not responsible for any damage or injury due to a total or partial non-

observance of directions / procedures stated in this Flight Manual.

FLY SYNTHESIS Srl reserves all rights to the property of this Manual, which can neither be

reproduced partially, nor integrally; this Manual is not to be disclosed to competitors without a

previous written authorization.

Flight manual

Storch Classic Jabiru

Rev. 0 –07/2002 Pag. 6

GENERAL INDEX

LOG OF REVISIONS.................................................................................................................................................3

LOG OF PAGES .........................................................................................................................................................4

FIGURES INDEX.......................................................................................................................................................8

1. DESCRIPTION......................................................................................................................9

FUSELAGE.................................................................................................................................................................9

LANDING GEAR................................................................................................................................................9

BRAKES ..............................................................................................................................................................9

FLIGHT AND ENGINE INSTRUMENTS..........................................................................................................9

SEATS AND SEAT BELTS..............................................................................................................................10

WINDSHIELD...................................................................................................................................................10

WING........................................................................................................................................................................10

EMPENNAGE ...................................................................................................................................................10

FLIGHT CONTROLS...............................................................................................................................................10

TRIM PLANT....................................................................................................................................................11

ENGINE DESCRIPTION .........................................................................................................................................11

ENGINE.............................................................................................................................................................11

PROPELLER.............................................................................................................................................................11

FUEL SYSTEM ........................................................................................................................................................11

ELECTRIC FUEL PUMP ..................................................................................................................................11

ELECTRIC REFUELING PUMP......................................................................................................................11

FUEL SWITCHES.............................................................................................................................................11

ELECTRIC PLANT ..................................................................................................................................................11

GENERAL .........................................................................................................................................................11

ELECTRIC ALIMENTATION CIRCUIT.........................................................................................................12

STATIC AND DYNAMIC PORT ............................................................................................................................12

2. TECHNICAL DATA...........................................................................................................13

DIMENSION.............................................................................................................................................................13

OVERALL DIMENSION..................................................................................................................................13

WING.................................................................................................................................................................13

AILERON ..........................................................................................................................................................13

STABILATOR...................................................................................................................................................13

HORIZONTAL TRIM .......................................................................................................................................13

VERTICAL FIN (RUDDER INCLUDED)........................................................................................................13

RUDDER............................................................................................................................................................13

WEIGHTS.................................................................................................................................................................13

LANDING GEAR .....................................................................................................................................................14

FUEL SYSTEM ........................................................................................................................................................14

ELECTRICAL SYSTEM..........................................................................................................................................14

POWER PLANT .......................................................................................................................................................14

PERFORMANCE WITH JABIRU 2200 ENGINE...................................................................................................15

DIFFERENT USEFUL DIMENSION ......................................................................................................................15

GRAVITY CENTER POSITIONING.......................................................................................................................15

AIRCRAFT LIST OF PARTS...................................................................................................................................18

COCKPIT LIST OF PARTS.....................................................................................................................................19

3. ROUTINE SERVICES........................................................................................................20

FUEL DRAIN............................................................................................................................................................20

REFUELLING...........................................................................................................................................................20

PRE-FLIGHT INSPECTION....................................................................................................................................20

LEFT MAIN LANDING GEAR........................................................................................................................21

LEFT WING.......................................................................................................................................................21

FUSELAGE LEFT SIDE ...................................................................................................................................21

EMPENNAGE ...................................................................................................................................................21

FUSELAGE RIGHT SIDE.................................................................................................................................21

RIGHT WING....................................................................................................................................................21

RIGHT MAIN LANDING GEAR .....................................................................................................................22

FUSELAGE FRONT SIDE................................................................................................................................22

COCKPIT...........................................................................................................................................................22

CHECK BEFORE ENGINE START UP..................................................................................................................22

ENGINE START UP.................................................................................................................................................23

Flight manual

Storch Classic Jabiru

Rev. 0 –07/2002 Pag. 7

BEFORE TAXIING ..................................................................................................................................................23

TAXIING...................................................................................................................................................................23

CHECK ENGINE......................................................................................................................................................24

TAKE OFF................................................................................................................................................................24

CRUISING ................................................................................................................................................................24

NORMAL DESCENT...............................................................................................................................................24

FAST DESCENT ......................................................................................................................................................25

FLYING IN RAINY CONDITIONS.........................................................................................................................25

4. LIMITATION......................................................................................................................26

ENGINE LIMITATIONS (SEE ENGINE MANUAL SPECS.)..............................................................................26

SPEED LIMITATIONS (AT MAXIMUM WEIGHT)............................................................................................26

MANOUVERING LIMITATIONS ..........................................................................................................................26

AUTHORISED MANOUVERS................................................................................................................................26

(RELATED TO NORMAL CATEGORY) ...............................................................................................................26

PROHIBITED MANOUVRES .................................................................................................................................26

STRUCTURAL RESISTANCE................................................................................................................................26

WEIGHT LIMITATIONS.........................................................................................................................................26

WEIGHT & BALANCE LIMITATIONS.................................................................................................................26

FLIGHTS LIMITS.....................................................................................................................................................26

5. EMERGENCY PROCEDURE...........................................................................................27

INTRODUCTION.....................................................................................................................................................27

ENGINE FAILURE...................................................................................................................................................27

POWER FAILURE ...................................................................................................................................................27

LOW ENGINE OIL PRESSURE..............................................................................................................................27

LOW FUEL PRESSURE ..........................................................................................................................................27

RESTARTING ..........................................................................................................................................................28

ENGINE FAILURE DURING TAKE-OFF..............................................................................................................28

ENGINE FAILURE AFTER TAKE-OFF DURING CLIMB...................................................................................28

FORCED LANDING WITH ENGINE STOPPED...................................................................................................28

PRECAUTIONAL EMERGENCY LANDING........................................................................................................29

FIRE ON THE GROUND AND DURING STARTING PROCEDURE..................................................................29

FIRE DURING FLIGHT...........................................................................................................................................29

FIRE IN FLIGHT DUE TO AN ELECTRICAL FAILL. (WITH SMOKE).............................................................30

FIRE ON THE GROUND DUE TO AN ELECTRICAL FAIL. (WITH SMOKE)..................................................30

FIRE IN THE COCKPIT DURING FLIGHT...........................................................................................................30

NON INTENTIONAL FLIGHT IN ICING CONDITIONS .....................................................................................30

SPIN RECOVERY....................................................................................................................................................30

LANDING WITH A FLAT TIRE.............................................................................................................................31

LANDING WITH BRAKE FAILURE .....................................................................................................................31

GLIDE.......................................................................................................................................................................31

ELECTRIC PLANT FAILURE.................................................................................................................................31

GENERATOR INDICATOR ILLUMINATED DURING ENGINE RUN IN FLIGHT...................................31

LOW TENSION INDICATOR ILLUMINATED..............................................................................................31

LOW TENSION INDICATOR ILLUMINATED ON THE GROUND ............................................................31

LOW TENSION INDICATOR ILLUMINATED IN FLIGHT .........................................................................32

FLAPS FAILURE .....................................................................................................................................................32

ENGINE STARTER FAILURE................................................................................................................................32

6. SPECIFICATIONS / PERFORMANCES.........................................................................33

CORRECTION TO THE INDICATED AIRSPEED (IAS)......................................................................................33

WIND INFLUENCE .................................................................................................................................................33

CLIMB ......................................................................................................................................................................33

CRUISE.....................................................................................................................................................................33

LANDING.................................................................................................................................................................34

MAXIMUM RATE OF GLIDE CONFIGURATION...............................................................................................34

7. DIAGRAMS & CHARTS ...................................................................................................35

8. WEIGHT AND BALANCE ................................................................................................40

GENERAL.................................................................................................................................................................40

WEIGHT CONDITIONS..........................................................................................................................................41

WEIGHT AND BALANCE REPORT......................................................................................................................41

MODEL“A” WEIGHT REPORT..............................................................................................................................42

9. APPENDIX...........................................................................................................................43

Flight manual

Storch Classic Jabiru

Rev. 0 –07/2002 Pag. 8

FIGURES INDEX

fig. 1 triptych, STORCH CL MODEL 3 views .................................................................................16

fig. 2 Sketch of Storch –part list –first part.......................................................................................17

fig. 3 Sketch of Storch –part list –second part..................................................................................17

fig. 4 Sketch of Storch –part list –inside cockpit..............................................................................19

fig. 5 PRE-FLIGHT inspection path..................................................................................................20

fig. 6 Table showing available distance from each altitude at best glide ratio..................................34

fig. 7 ROLL DISTANCE / TAKE-OFF DISTANCE -.....................................................................35

fig. 8 LANDING RUN / LANDING DISTANCE ............................................................................36

fig. 9 RELATIVE WIND DIAGRAM VERSUS WIND COMPONENT.........................................37

fig. 10 MAX. RATE OF CLIMB DIAGRAM AT MAXIMUM RPM.............................................38

fig. 11 FLIGHT ENVELOPE ............................................................................................................39

FIG. 12 CONVERSION TABLE KILOMETERS/HOUR (km/h) –KNOTS.................................43

fig. 13 CONVERSION TABLE KNOTS (knots) –METERS / SECONDS (m/sec.).......................43

fig. 14 VERTICAL SPEED (m/sec.) ’ (feet/min.)............................................................................44

fig. 15 AIR CORRECTION TABLE.................................................................................................45

fig. 16 CONVERSION TABLE meters/feet......................................................................................46

fig. 17 CONVERSION OF ALTITUDE PRESSURE FROM mb TO inch Hg................................47

fig. 18 TABLE WITH. STANDARD. ATM. CONVERSION .........................................................48

Flight manual

Storch Classic Jabiru

Rev. 0 –07/2002 Pag. 9

1. Description

In this charter the aircraft is described in all its parts:

FUSELAGE

THE FUSELAGE consists of a cockpit of composite materials with a self-support

Ting shell structure. The cockpit shell contains five transverse frames of composite materials, which

guarantee the rigidity of the structure and high degree of safety and reliability.

The central transverse frame crosses the whole cockpit section and bears the loads of the aircraft

both during flight and on the ground. To it is connected

The tail trunk consisting of a metal tubular beam of the same type as used on the wing. A fireproof

bulkhead, on the edge of which is also fastened the metal engine-support frame, which also supports

the front wheel, closes the front area of the cockpit.

The cockpit ceiling is crossed by a welded-tube frame, which allows good upward visibility without

affecting the structural compactness. The undercarriage is fastened to the belly of the fuselage

through a welded tube structure and the bending element consists of two milled bars of light alloy.

LANDING GEAR

The landing gear has a fixed tricycle configuration where the main part is mounted on two

Self-suspension high resistance aluminum entering of the lower part of the fuselage, fixed

inside connected by tube. The front part is a light metal suspension fork independent and

pivoting directionally intended by the pilot on ground movement, 30° L-R from his

centerline.

The wheels are covered by aerodynamic fairings, easy to remove.

In case of using the airplane without these fairings you must beware of decreasing

seriously the performance of the airplane.

BRAKES

A central system is related to a brake, which act on both wheels.

FLIGHT AND ENGINE INSTRUMENTS

The flight instruments are mounted at the front panel at the pilot’s convenience right or left.

The engine instruments on the opposite side.

The serial mounted instruments are:

Engine instruments: rpm counter, cylinder. head temp., exhaust gas temp., oil temp., oil

press.,

Fuel press., hour counter, fuel low level lamp.

Flight instruments: speed indicator, altimeter, variometer, magnetic compass, slip

indicator.

Flight manual

Storch Classic Jabiru

Rev. 0 –07/2002 Pag. 10

SEATS AND SEAT BELTS Seats

The seats are fixed on the floor part and can be adapted to the size of the pilot or

passenger. The bottom of the seat has an easy take away system to allow underlying

inspection of flight commands. The stick bottom has a protection to avoid that some

objects will fall down, blocking partially the steering components.

SEAT ADAPTION

The seats of the airplane can be adapted to the convenience of the occupant.

These adjustments are only possible on the ground, NOT IN-FLIGHT!

Seat belts

All the seats are equipped with 4-points attached seat-belts independent adjustable by the

Occupant. Safely locked due to a bayonet quick release locking-system.

These can be released by pushing the red bottom at the lock system.

WINDSHIELD

A fixed windshield in lexan material frontally closes the airplane.

WARNING

Before starting the engine make sure that the windows are properly locked at all their

points.

WING

THE WING is designed with full-length slotted detached ailerons (Junker Type) to allow high lift

coefficients and a good degree of maneuverability. The wing contour adopted is of the laminar flow

type to obtain very low frictional resistance and therefore high cruising speeds (for an ultra light

aircraft) with low fuel consumption.

The wing consists of a shell of layered compounds held together by a metal structure consisting of a

tubular longeron to which are fastened the metal wing ribs. The Material Used Is aerospace

Aluminum alloy. The skin is riveted to the structure.

The aileron is built with the same principle as the wing, to which it is connected through pods

fastened to the ribs. The wind bracing consists of metal structural elements of drop-shaped cross

section to increase the streamlining. The wing and fuselage are connected to each other thought two

bearing points: a lower frame which supports the bracing and the landing gear and an upper frame

of welded steel tube which crosses the cockpit ceiling. The first part of the leading edge of the wing

houses the fuel tanks.

FULL COMPOSITE WING ARE NOW AVAIABLE

EMPENNAGE

THE EMPENNAGE is entirely of epoxy-fiberglass. PVC compounds and consists of a fin riveted

directly to the cantilever tail and supporting directly the rudder through two metal hinges fastened

directly to the fin longeron. The horizontal tail assembly is a stabilator with anti-tab, which also

acts as trim-tab, and the whole assembly is fastened to the fuselage through a welded steel unit,

while the smoothness of the controls is guaranteed by two ball bearings.

FLIGHT CONTROLS

THE DUAL CONTROLS are of conventional type with control stick and rudder pedals, central gas

throttle. All the controls are of welded steel construction and milled alloy elements. The ailerons are

controlled directly from inside the fuselage through rigid rods with ball joints. The horizontal tail

elements are operated through double push-pull controls with ball-joint terminals. The rotation

movement of both the ailerons and the stabilator is statically balanced.

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