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. +39.(0)432.992482 – +39.(0)432.993557
Fax +39.(0)432.931280
Sito web:
www.flysynthesis.com
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
