FlySynthesis Storch S 500 LSA Installation guide

FLY SYNTHESIS
STORCH S 500 LSA
PILOT OPERATING HANDBOOK
AND TRAINING MANUAL
(for Rotax 912 UL and Jabiru 2200 engines versions)
00
11/10/07
Complete manual
revision
M. Fiorindo
M. Fiorindo
C. Pinzana
Num.
Date
Description
Issued
Verified
Approved
REVISION
FlySynthesis s.r.l. reserves it to terms of law the exclusive ownership of this manual and also forbids the partial reproduction of it.
THIS DOCUMENT MUST BE CARRIED IN THE AIRCRAFT AT ALL TIMES

Identification: POH_SS_LSA Rev.0
Page: 2 of 71
Date: 11/10/07
Issued: M. Fiorindo
Verified: M. Fiorindo
Approved: C. Pinzana
Revision Description:
New manual issue
Pilot Operating Handbook and
Training Manual
FLY SYNTHESIS
STORCH S 500 LSA
(for Rotax 912 UL and
Jabiru 2200 engines versions)
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) –Italy
Tel. [phone]
Fax [phone]
Sito web: www.flysynthesis.com
e-mail: [e-mail]
IDENTIFICATION:
Manufacturer
FLY SYNTHESIS SRL
Address
Provincial Rd 78 Km 12.150
Mortegliano 33050 (UD) ITALY
Model:
FLY SYNTHESIS STORCH
Version:
STORCH S 500 LSA
Airframe Serial
No:
Engine Model:
Engine Serial No:
Registration:
Date:
Signature:
Stamp:

Identification: POH_SS_LSA Rev.0
Page: 3 of 71
Date: 11/10/07
Issued: M. Fiorindo
Verified: M. Fiorindo
Approved: C. Pinzana
Revision Description:
New manual issue
Pilot Operating Handbook and
Training Manual
FLY SYNTHESIS
STORCH S 500 LSA
(for Rotax 912 UL and
Jabiru 2200 engines versions)
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) –Italy
Tel. [phone]
Fax [phone]
Sito web: www.flysynthesis.com
e-mail: [e-mail]
NOTE
This manual may be revised in the future and pages/or sections re-issued in part or whole.
Revisions will also be available on the Fly Synthesis website www.flysynthesis.com. Any
revisions and/or sections should be printed and replaced in the manual at the earliest
possible time for flight safety.
The revisions added to the manual should be logged and recorded in the table under log of
amendments of this manual, by the owner/user.
DEFINITIONS
Definitions used in this handbook such as WARNING, CAUTION and NOTE are employed
in the following context.
WARNING
Procedures or instructions that if not followed correctly may result in injury or death
CAUTION
Procedures or instructions that if not followed correctly may result in damage to the
aircraft or its parts
NOTE: Procedures or instructions that affect safety of flight are highlighted
INTELLECTUAL PROPERTY
The data and information contained in this document is the property of FLYSYNTHESIS
SRL. This document may not be reproduced or transmitted to a third party, in any form or by
any means. Any unauthorized copy or distribution is illegal as per international agreements
relating to property rights.
THIS AIRCRAFT WAS MANUFACTURED IN ACCORDANCE WITH THE FOLLOWING
LIGHT SPORT AIRCRAFT AIRWORTHINESS STANDARDS CS VLA, F2279, F2295 AND
F2483 AND DOES NOT CONFORM TO STANDARD CATEGORY AIRWORTHNESS
REQUIREMENTS.

Identification: POH_SS_LSA Rev.0
Page: 4 of 71
Date: 11/10/07
Issued: M. Fiorindo
Verified: M. Fiorindo
Approved: C. Pinzana
Revision Description:
New manual issue
Pilot Operating Handbook and
Training Manual
FLY SYNTHESIS
STORCH S 500 LSA
(for Rotax 912 UL and
Jabiru 2200 engines versions)
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) –Italy
Tel. [phone]
Fax [phone]
Sito web: www.flysynthesis.com
e-mail: [e-mail]
LOG OF REVISIONS
Revision No.
Revision
Date
Signature

Identification: POH_SS_LSA Rev.0
Page: 5 of 71
Date: 11/10/07
Issued: M. Fiorindo
Verified: M. Fiorindo
Approved: C. Pinzana
Revision Description:
New manual issue
Pilot Operating Handbook and
Training Manual
FLY SYNTHESIS
STORCH S 500 LSA
(for Rotax 912 UL and
Jabiru 2200 engines versions)
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) –Italy
Tel. [phone]
Fax [phone]
Sito web: www.flysynthesis.com
e-mail: [e-mail]
LOG OF EFFECTIVE PAGES
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Identification: POH_SS_LSA Rev.0
Page: 6 of 71
Date: 11/10/07
Issued: M. Fiorindo
Verified: M. Fiorindo
Approved: C. Pinzana
Revision Description:
New manual issue
Pilot Operating Handbook and
Training Manual
FLY SYNTHESIS
STORCH S 500 LSA
(for Rotax 912 UL and
Jabiru 2200 engines versions)
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) –Italy
Tel. [phone]
Fax [phone]
Sito web: www.flysynthesis.com
e-mail: [e-mail]
INDEX
Title Section Page
IDENTIFICATION 2
DEFINITIONS 3
LOG OF REVISIONS 4
LOG OF EFFECTIVES PAGES 5
General information 1 7
Limitations 2 13
Emergency procedures 3 19
Normal operations 4 26
Performances 5 35
Weight and balance 6 44
Aircraft ground handling and service 7 47
Aircraft check list 8 51

Identification: POH_SS_LSA Rev.0
Page: 7 of 71
Date: 11/10/07
Issued: M. Fiorindo
Verified: M. Fiorindo
Approved: C. Pinzana
Revision Description:
New manual issue
Pilot Operating Handbook and
Training Manual
FLY SYNTHESIS
STORCH S 500 LSA
(for Rotax 912 UL and
Jabiru 2200 engines versions)
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) –Italy
Tel. [phone]
Fax [phone]
Sito web: www.flysynthesis.com
e-mail: [e-mail]
SECTION 1
General information
Title Page
1.1 Introduction 7
1.2 Warnings, suggestions and notes 7
1.3 Descriptive aircraft datas 7
1.4 Aircraft three views 12

Identification: POH_SS_LSA Rev.0
Page: 8 of 71
Date: 11/10/07
Issued: M. Fiorindo
Verified: M. Fiorindo
Approved: C. Pinzana
Revision Description:
New manual issue
Pilot Operating Handbook and
Training Manual
FLY SYNTHESIS
STORCH S 500 LSA
(for Rotax 912 UL and
Jabiru 2200 engines versions)
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) –Italy
Tel. [phone]
Fax [phone]
Sito web: www.flysynthesis.com
e-mail: [e-mail]
1.1 INTRODUCTION
This operating handbook contains the necessary information for a sure and efficient
employment of the aircraft FLYSYNTHESIS STORCH S LSA ROTAX 912 UL 80 HP and
STORCH S JABIRU 2200 85 HP. Unless indicated, all descriptive data are valid for both
engine versions. The POH has been prepared to comply with the requirements of CS-VLA
and where relevant the ASTM standard.
The Pilot Operating Handbook is valid only for the particular aircraft identified on page 2,
the identification page.
1.2 WARNINGS, SUGGESTIONS AND NOTES
The observance of this manual is compulsory for the aircraft's use.
FLYSYNTHESIS S.r.l. declines every responsibility for any damage to person and thing
derived by a missed or partial observance of the prescriptions contained in this manual.
FLYSYNTHESIS S.r.l. reserves it, to terms of law, the exclusive ownership of this manual
and also forbids the partial or integral reproduction of it and however to communicate it to
competing firms without a preventive written authorization.
1.3 DESCRIPTIVES AIRCRAFTS DATA
TYPE OF AIRCRAFT
Storch S is ultra light aircraft with airframe, wing and control surfaces in composite materials.
The tail beam is made of aeronautical aluminum alloy, fixed on composite structure. The
retangular shape high wing utilizes a laminar flow airfoil section. The ailerons are differential
whilst the flaps are electrically operated plain type. The vertical tail control surface is
composed by a fixed fin and by a mobile rudder, the horizontal tail control surface is
completely mobile, hinged in the central part with integrated trim. The tricycle type landing
gear is fixed, with dampened nose wheel and with main legs made of either spring steel or
ERGAL aeronautical aluminum alloy.
The Storch S aircraft is approved for Day VFR only. Flight into bad weather with IFR
conditions by VFR pilots and aircraft is extremely dangerous. As the owner and operator of
an aircraft you are responsible for the safety of your passenger and yourself.
DIMENSIONS (valid for Rotax 912 UL and Jabiru 2200 engines)
General
Wing span: 9.300 m
Length: 5.950 m
Height: 2.150 m
Wing
Surface: 10.250 m2
Wing chord: 1.100 m
Wing load: 44.500 kg/m2
Flap
Surface: 0.620 m2

Identification: POH_SS_LSA Rev.0
Page: 9 of 71
Date: 11/10/07
Issued: M. Fiorindo
Verified: M. Fiorindo
Approved: C. Pinzana
Revision Description:
New manual issue
Pilot Operating Handbook and
Training Manual
FLY SYNTHESIS
STORCH S 500 LSA
(for Rotax 912 UL and
Jabiru 2200 engines versions)
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) –Italy
Tel. [phone]
Fax [phone]
Sito web: www.flysynthesis.com
e-mail: [e-mail]
Span: 2.230 m
Chord: 0.280 m
Travel: 0° - 40°
Aileron
Surface: 0.410 m2
Span: 1.650 m
Chord: 0.250 m
Travel: down 20° / up 30°
Stabilator
Surface: 1.650 m2
Span: 2.450 m
Chord: 0.700 m
Travel: down 11° / up 16°
Vertical fin (with rudder)
Surface: 1.120 m2
Height: 1.280 m
Mean chord: 1.930 m
Rudder
Surface: 0.600 m2
Height: 1.200 m
Mean chord: 0.480 m
Travel: +/-22°
WEIGHTS
Rotax 912 UL Jabiru 2200
Empty weight 300 kg 297 kg
Maximum allowed weight in baggage compartment 12 kg 12 kg
Maximum Take Off Weight 500 kg 500 kg
Minimum Pilot Weight 55 kg 55 kg
LANDING GEAR (valid for Rotax 912 UL and Jabiru 2200 engines)
Type: Tricycle type landing gear with dampened nose wheel
Main gear track: 1.640 m
Wheelbase: 1.340 m
Tyre: Main: 4.00x6"
Nose wheel: 4.00x4"
Tyre pressure: Main: 2.2 - 2.4 bar
Nose wheel: 1.8 bar
Brakes: Main wheels hydraulic disc.
FUEL SYSTEM (valid for Rotax 912 UL and Jabiru 2200 engines)
Type: Two lines with mechanical and auxiliary eletric fuel pump
Fuel plant draining system and return line system in the left tank
Refueling by the fuel filler located on the upper layer of the wings

Identification: POH_SS_LSA Rev.0
Page: 10 of 71
Date: 11/10/07
Issued: M. Fiorindo
Verified: M. Fiorindo
Approved: C. Pinzana
Revision Description:
New manual issue
Pilot Operating Handbook and
Training Manual
FLY SYNTHESIS
STORCH S 500 LSA
(for Rotax 912 UL and
Jabiru 2200 engines versions)
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) –Italy
Tel. [phone]
Fax [phone]
Sito web: www.flysynthesis.com
e-mail: [e-mail]
Tanks: Two integrated tanks in glass fibers with 45 liters of capacity for
each tank
Fuel tank caps
Non-usable fuel 2 liters for each tank
Fuel filter: Gascolator on firewall, entry fuel line filtered.
Fuel specification
Rotax 912ULS Premium Automotive Unleaded fuel min 95Ron.
Jabiru 2200A Avgas 100LL.
ELETRIC SYSTEM (valid for Rotax 912 UL and Jabiru 2200 engines)
Type: 12 V electrical wiring with starting battery
Electrical wiring protected with fuses or circuit breakers
External rectifier-regulator
POWERPLANT
Engine: Rotax 912 UL
Type: 4 strokes, 4 cylinder horizontal opposed, spark ignition engine, liquid
cooled cylinder heads, ram air cooled cylinders, two constant depression
carburettors, mechanical fuel pump, dry sump forced lubrification.
Ignition: Increased electric ignition system HD
Battery: Sealed Lead Acid Battery 12 Volts
Standard propeller: DUC composite three blades propeller, diameter 1670 mm, ground
variable pitch.
DUC composite two blades propeller, diameter 1670 mm, ground
variable pitch
GT-2 wood two blades propeller, diameter 1660 mm, fixed pitch 1450
mm.
___________________________________________________________________________________________________________________________________________________
Engine: Jabiru 2200
Type: 4 strokes, 4 cylinder horizontal opposed, spark ignition engine, ram air
cooled cylinders, 2 carburatori a depressione costante, two constant
depression carburettors, mechanical fuel pump, warm air at carburettor
system.
Ignition: Eletric ignition system
Battery: Sealed Lead Acid Battery 12 Volts
Standard propeller: DUC composite three blades propeller, diameter 1520 mm, ground
variable pitch. DUC composite two blades propeller, diameter 1620 mm,
ground variable pitch

Identification: POH_SS_LSA Rev.0
Page: 11 of 71
Date: 11/10/07
Issued: M. Fiorindo
Verified: M. Fiorindo
Approved: C. Pinzana
Revision Description:
New manual issue
Pilot Operating Handbook and
Training Manual
FLY SYNTHESIS
STORCH S 500 LSA
(for Rotax 912 UL and
Jabiru 2200 engines versions)
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) –Italy
Tel. [phone]
Fax [phone]
Sito web: www.flysynthesis.com
e-mail: [e-mail]
GT-2 wood two blades propeller, diameter 1510/1520/1570 mm, fixed
pitch 1050/1000 mm.
Other propeller types as approved by the manufacturer and listed in appendix C of the
maintenance manual. (Applicable to both engines)
INSTRUMENTS (valid for Rotax 912 ULS and Jabiru 2200 engines)
Standard instruments: air speed indicator, altimeter, vertical speed indicator, magnetic
compass, bank indicator, flap angular range indicator, two low
fuel level amber lamp, CHT, EGT, RPM, oil temperature indicator,
oil pressure indicator, fuel pressure indicator, engine run time
indicator, 12 V aux socket.
OTHER STANDARD EQUIPMENTS (valid for Rotax 912 UL and Jabiru 2200 engines)
Main wheels and nose wheel fairings, main legs and nose camper aerodynamic fairing, four
points safety belts, electric flap system (travel: 0° - 40°), manual trim regulation system, full
moquette cabin covering, baggage compartment with baggage net.

Identification: POH_SS_LSA Rev.0
Page: 12 of 71
Date: 11/10/07
Issued: M. Fiorindo
Verified: M. Fiorindo
Approved: C. Pinzana
Revision Description:
New manual issue
Pilot Operating Handbook and
Training Manual
FLY SYNTHESIS
STORCH S 500 LSA
(for Rotax 912 UL and
Jabiru 2200 engines versions)
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) –Italy
Tel. [phone]
Fax [phone]
Sito web: www.flysynthesis.com
e-mail: [e-mail]
1.4 AIRCRAFT THREE VIEWS

Identification: POH_SS_LSA Rev.0
Page: 13 of 71
Date: 11/10/07
Issued: M. Fiorindo
Verified: M. Fiorindo
Approved: C. Pinzana
Revision Description:
New manual issue
Pilot Operating Handbook and
Training Manual
FLY SYNTHESIS
STORCH S 500 LSA
(for Rotax 912 UL and
Jabiru 2200 engines versions)
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) –Italy
Tel. [phone]
Fax [phone]
Sito web: www.flysynthesis.com
e-mail: [e-mail]
SECTION 2
Limitations
Title Page
2.1 Introduction 14
2.2 Airspeed limitations 14
2.3 Anemometers marking 14
2.4 Powerplant and propeller limitations 15
2.5 Powerplant instruments marking 15
2.6 Weight limitations 16
2.7 Center of gravity limitations 16
2.8 Manoeuvre limitations 16
2.9 Load factor limitations 17
2.10 Crew 17
2.11 Placards 17

Identification: POH_SS_LSA Rev.0
Page: 14 of 71
Date: 11/10/07
Issued: M. Fiorindo
Verified: M. Fiorindo
Approved: C. Pinzana
Revision Description:
New manual issue
Pilot Operating Handbook and
Training Manual
FLY SYNTHESIS
STORCH S 500 LSA
(for Rotax 912 UL and
Jabiru 2200 engines versions)
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) –Italy
Tel. [phone]
Fax [phone]
Sito web: www.flysynthesis.com
e-mail: [e-mail]
2.1 INTRODUCTION
This section contains the operational limitations and the instruments marking for use in
safety condition the aircraft, the engine, the equipments and standard plant. The limitations
of speed are been calculated following the BCAR-S rules, the structures are been tested
following the same rules.
2.2 AIRSPEED LIMITATIONS
Speed
Rotax
912 ULS
IAS
Jabiru
2200
IAS
Notes
Vne
Never Exceed speed
220 km/h
118 KTS
220 km/h
118 KTS
Never exceed this speed in every
condition or configuration
Vmo
Maximum Structural
Cruising Speed
160 km/h
86 KTS
160 km/h
86 KTS
Never exceed this speed in
turbolent air condition
Va
Manoeuvring speed
130 km/h
70 KTS
130 km/h
70 KTS
Do not use full stick and full rudder
deflections above this speed
Vfe
Maximum speed with full
flaps
105 km/h
57 KTS
105 km/h
57 KTS
Do not exceed this speed with flap
extended
Vs
Stall speed without flap
65 km/h
35 KTS
65 km/h
35 KTS
Do not descende this speed without
flap to avoid undesired stall
conditions
Vs1
Stall speed in take off
position (15°)
63 km/h
34 KTS
63 km/h
34 KTS
Do not descende this speed with
flap in take off position to avoid
undesired stall conditions
Vso
Stall speed in landing
position - full flap (40°)
59 km/h
32 KTS
59 km/h
32 KTS
Do not descende this speed with
flap in landing position to avoid
undesired stall conditions
2.3 ANEMOMETERS MARKING
(valid for Rotax 912 UL and Jabiru 2200 engines)
Marking
Speed range (IAS)
Definition
White arc
[Vs0 - Vfe] 59 - 105 km/h
[Vs0 - Vfe] 32 - 57 KTS
Speed range where flap may be extended
Green arc
[Vs - Vmo] 65 - 160 km/h
[Vs - Vmo] 35 - 86 KTS
Speed range of normal operation
Yellow arc
[Vmo- Vne] 160 - 220 km/h
[Vmo- Vne] 86 - 118 KTS
Manoeuvre the aircraft with great caution
Red line
[Vne] 220 km/h
[Vne] 118 KTS
Maximum speed allowed

Identification: POH_SS_LSA Rev.0
Page: 15 of 71
Date: 11/10/07
Issued: M. Fiorindo
Verified: M. Fiorindo
Approved: C. Pinzana
Revision Description:
New manual issue
Pilot Operating Handbook and
Training Manual
FLY SYNTHESIS
STORCH S 500 LSA
(for Rotax 912 UL and
Jabiru 2200 engines versions)
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) –Italy
Tel. [phone]
Fax [phone]
Sito web: www.flysynthesis.com
e-mail: [e-mail]
2.4 POWERPLANT AND PROPELLER LIMITATIONS
(Refer always to Rotax's or Jabiru operator manual)
Engine manufacturer: Rotax Jabiru Aircraft
Engine model: 912 UL 2200
Maximum take off power: 60 kW 63.4 kW
Maximum continuos power: 58 kW 63.4 kW
Maximum take-off RPM: 5800 rpm 3300 rpm
Maximum continuos RPM: 5500 rpm 3300 rpm
Minimum cylinder head temperature: 150°C 200°C
Maximum oil temperature: 140°C 118°C
Minimum oil pressure: 1.5 bar 2.2 bar
Maximum oil pressure: 7 bar 5.25 bar
Minimum fuel pressure: 0.15 bar 0.05 bar
Maximum fuel pressure: 0.4 bar 0.2 bar
Usable type of fuel: minimum 95 RON Avgas or >95 RON
Usable type of oil: See engine manual specifications
________________________________________________________________________
Propeller manufacturer: DUC Hélices GT Propellers
Propeller model: Carbon three-blades Wood two-blades
Carbon two-blades
Ground variable pitch Fixed pitch
Maximum diameter: 1670 mm 1660 mm
2.5 POWERPLANT INSTRUMENTS MARKING
Rotax 912 UL engine version
Strumento
Red line
Inf. limit
Inf. yellow
arc -Caution
Green arc-normal
operations
Sup. yellow
arc -Caution
Red line
Sup. limit
RPM indicator
n/a
n/a
1.400 - 5.500 rpm
5.500 - 5.800 rpm
5.800 rpm
Fuel pressure gauge
0.15 bar
n/a
0.15 - 0.4 bar
n/a
0.4 bar
Oil pressare gauge
0.8 bar
0.8 - 2 rpm
2 - 5 bar
5 - 7 rpm
7 bar
Oil temp. gauge
50°C
50° - 90°C
90° - 100°C
110° - 140°C
140°C
CHT
50°C
n/a
50° - 100 °C
110° - 150°C
150°C
Jabiru 2200 engine version
Strumento
Red line
Inf. limit
Inf. yellow
arc -Caution
Green arc-normal
operations
Sup. yellow
arc -Caution
Red line
Sup. limit
RPM indicator
n/a
n/a
900 - 3.300 rpm
n/a
3.300 rpm
Fuel pressure
gauge
0.05 bar
n/a
0.05 - 0.2 bar
n/a
0.2 bar
Oil pressare gauge
0.8 bar
n/a
2.2 - 5.25 bar
n/a
5.25 bar
Oil temp. gauge
15°C
15° - 80°C
80° - 100°C
100° - 118°C
118°C
CHT
50°C
n/a
50° - 180 °C
180° - 200°C
200°C
EGT
Below 70% of power
Above 70% of power
680° - 750°C
640° - 780°C
2.6 WEIGHT LIMITATIONS

Identification: POH_SS_LSA Rev.0
Page: 16 of 71
Date: 11/10/07
Issued: M. Fiorindo
Verified: M. Fiorindo
Approved: C. Pinzana
Revision Description:
New manual issue
Pilot Operating Handbook and
Training Manual
FLY SYNTHESIS
STORCH S 500 LSA
(for Rotax 912 UL and
Jabiru 2200 engines versions)
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) –Italy
Tel. [phone]
Fax [phone]
Sito web: www.flysynthesis.com
e-mail: [e-mail]
Rotax 912 UL Jabiru 2200
Empty weight 300 Kg 297 Kg
Maximum fuel weight 69 Kg 69 Kg
Maximum allowed weight in baggage compartment 12 Kg 12 Kg
Maximum Take Off Weight 500 Kg 500 Kg
2.7 CENTER OF GRAVITY LIMITATIONS
With the purpose to get the best performances of flight and operations in complete safety,
according to the procedures described in this manual, the aircraft must have employed
respecting all the schemes of load and balancing pointed out in the following pages.
Pilot must consider the limit of weighing and all correlated parameters.
Before the delivery of the airplane, centre gravity position and weight of the airplane are
verified.
NOTE: Empty weight & Centre gravity position must be updated after a new weighing, in the
following case:
- Substitution and/or modify of one or plus accessories and equipment;
- After painting or reparations of fusolage.
Weight and Centre Gravity position must be reported after every relief in the weighing report
inside this manual only by authorized personnel.
The location of the CG can be defined by reference to the % MAC.
Maximum anterior limit: 30% M.A.C. correspondent to 330 mms
Maximum back limit: 36% M.A.C. correspondent to 396 mms
For methodology and conditions for weight and balance procedure, see section 6.
2.8 MANOEUVRE LIMITATIONS
All aerobatics maneuvers are prohibited.
The normal flight operations are the followings:
- Every connected manoeuvre to the normal flight operation,
- Stalls, with exclusion of the accelerated stall (superior to 1 g)
- Low speed figure eight, chandelle, turns below 60°
The use of the aircraft has to be conforming with the Rules of the State within it fly.
WARNING
Flight in known icing conditions, snow and heavy rain is prohibited.
The pilot is responsible for determining the airworthiness of the aircraft for each flight
including on board fuel lever verification.
All maneuvers at load factor less than - 0.5 g, must be performed for no longer than 5
seconds.
In single pilot operation, belt and shoulder harness of the vacant seat must be secured to
avoid uncontrolled movement of seat back and belt.

Identification: POH_SS_LSA Rev.0
Page: 17 of 71
Date: 11/10/07
Issued: M. Fiorindo
Verified: M. Fiorindo
Approved: C. Pinzana
Revision Description:
New manual issue
Pilot Operating Handbook and
Training Manual
FLY SYNTHESIS
STORCH S 500 LSA
(for Rotax 912 UL and
Jabiru 2200 engines versions)
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) –Italy
Tel. [phone]
Fax [phone]
Sito web: www.flysynthesis.com
e-mail: [e-mail]
2.9 LOAD FACTOR LIMITATIONS
The load factors limit used for the calculation of the structures conform with CS VLA rules:
Flap retracted Flap extendeed
- Maximum positive load factor 4.0 (+) - Maximum positive load factor 2.0 (+)
- Maximum negative load factor 2.0 (-) - Maximum negative load factor 0.0 (+)
2.10 CREW
The minimum crew for flight operations is a person. The owner can choose the place of
pilotage to the right or to the left. The maximum number of people permitted on board is two.
2.11 PLACARDS
The following placards are to be located and visible to the pilot where an inspection or
function is relevant and required in the designated area.
Located on the Instrument panel
WARNING
THIS AIRCRAFT WAS MANUFACTURED IN ACCORDANCE WITH LIGHT SPORT AIRCRAFT
AIRWORTHINESS STANDARDS AND DOES NOT CONFORM TO STANDARD CATEGORY
AIRWORTHINESS REQUIREMENTS.
Located on Nose Leg fairing Located on both Main Leg fairing
Located next to fuel each filler cap Located in baggage compartment
BAGGAGE COMPARTMENT
Maximum 12 Kg
Evenly distribuited
INFLATE MAIN WHEEL TO
2.2 –2.4 bar (32 –35 psi)
INFLATE NOSE WHEEL TO
1.8 bar (26.1 psi)
FUEL CAPACITY 45 LTRS
MINIMUM 95 OCTANE AUTO
FUEL
OR 100 LL AVGAS

Identification: POH_SS_LSA Rev.0
Page: 18 of 71
Date: 11/10/07
Issued: M. Fiorindo
Verified: M. Fiorindo
Approved: C. Pinzana
Revision Description:
New manual issue
Pilot Operating Handbook and
Training Manual
FLY SYNTHESIS
STORCH S 500 LSA
(for Rotax 912 UL and
Jabiru 2200 engines versions)
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) –Italy
Tel. [phone]
Fax [phone]
Sito web: www.flysynthesis.com
e-mail: [e-mail]
STORCH S 500 LSA
Speed: KTS Weight: Kg
Vne (Not Exceeded) 118 Maximum Take-off 500
Vmo (Max Operating) 86 Empty Weight 300
Va (Min Maneuvering) 70 Minimum Pilot 55
Vfe (Max Full Flap) 57 Maximum Pilot +
Vs (Stall) 35 passenger 180
Vso (Stall with flap) 32
AEROBATIC MANOEUVRES AND
SPINS ARE PROHIBITED
Located on fuselage next to fuel refill tap Located on fuselage next to fuel drain tap
AUXHILARY
RE FUELING POINT
AUXHILARY
FUEL DRAIN
Located in baggage
compartment
Located in baggage
compartment
Located on internal and external side of doors
STORCH 550 LSA DATA PLATE
Aircraft s/n __________ Fusolage s/n __________
Date of Manufacture ____________________
Engine Type ____________________
Engine s/n ____________________
Propeller type ____________________
Propeller s/n ____________________
Hub s/n ____________________

Identification: POH_SS_LSA Rev.0
Page: 19 of 71
Date: 11/10/07
Issued: M. Fiorindo
Verified: M. Fiorindo
Approved: C. Pinzana
Revision Description:
New manual issue
Pilot Operating Handbook and
Training Manual
FLY SYNTHESIS
STORCH S 500 LSA
(for Rotax 912 UL and
Jabiru 2200 engines versions)
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) –Italy
Tel. [phone]
Fax [phone]
Sito web: www.flysynthesis.com
e-mail: [e-mail]
SECTION 3
Emergency procedures
Title Page
3.1 Introduction 20
3.2 Ground emergency procedures 20
3.3 Take off emergency procedures 20
3.4 During flight emergency procedures 21
3.5 Electrical wiring failure 22
3.6 Landing emergency procedures 23
3.7 Opening parachute procedure 24
3.8 Other emergency 25

Identification: POH_SS_LSA Rev.0
Page: 20 of 71
Date: 11/10/07
Issued: M. Fiorindo
Verified: M. Fiorindo
Approved: C. Pinzana
Revision Description:
New manual issue
Pilot Operating Handbook and
Training Manual
FLY SYNTHESIS
STORCH S 500 LSA
(for Rotax 912 UL and
Jabiru 2200 engines versions)
Provincial Road n.78 Km 12.150
33050 Mortegliano (UD) –Italy
Tel. [phone]
Fax [phone]
Sito web: www.flysynthesis.com
e-mail: [e-mail]
3.1 INTRODUCTION
An emergency situation is extremely rare; even so, the pilot responsible for the aircraft
should meticulously carry out daily pre-flight controls checks. A safe airworthy aircraft should
be maintained according to the requirements of the accompanying maintenance manual.
This section contains the recommended procedures should an emergency arise. It is
strongly advised that Pilots become familiar with these procedures.
3.2 GROUND EMERGENCY PROCEDEDURES
ENGINE ON FIRE
1. Fuel tank faucet - Close
2. Electric fuel pump - Off
3. Cabin heating - Off
4. Throttle - All forward
5. Master switch - OFF
6. Ignition magnets key - OFF
7. Get out of aircraft immediatly
8. If possible, use an extinguisher to extinguish the fire.
WARNING: Don’t remove the engine cowling until the complete extinction of the fire.
Don't use water to extinguish the fire.
3.3 TAKE OFF EMERGENCY PROCEDURES
TAKE OFF INTERRUPTION (during take off run)
1. Throttle - All rearward (reduce to minimum RPM)
2. Brakes - Brake and avoiding skidding the wheels
3. Flap - Retract
4. Ignition magnets key - OFF
5. Master switch - OFF
6. Fuel tank faucet - OFF
ENGINE FAILURE DURING TAKE OFF (after rotation - below 50 mt)
1. Fuel tank faucet - Close
2. Electric fuel pump - OFF
3. Master switch & ignition magnets key - OFF
4. Safety belts - Tighten well
5. Maintain a linear line of flight, without turning if possible, and if the area allows it, get
ready to a forced landing (see relative paragraph)
ENGINE FAILURE DURING TAKE OFF (during climb)
If the height allows it, proceed in the following way:
1. Best glide speed - (57 KTS)
2. Electric fuel pump - Verify ON
3. Fuel tank faucet - Verify LH tank faucet open
4. Fuel tank level - check fuel quantity