SCHEMPP-HIRTH FLUGZEUGBAU GmbH., KIRCHHEIM/TECK
Arcus M
FLIGHT MANUAL
2.4 Power plant, fuel and oil
Engine manufacturer:
Solo Kleinmotoren GmbH.
D-71050 Sindelfingen, Germany
Engine model:
SOLO 2625-02i
Take-off power at
6600 RPM (MSL, ISA):
50 kW (68 HP)
Max. continuous power
at 6700 RPM:
50 kW (68 HP)
Maximum permitted coolant
liquid temperature:
115° C (240° F)
Fuel: premium
unleaded
not below RON 95,
AVGAS 100LL, or mixtures of
the two fuels
Oil (lubrication):
Fuel / oil mixture 1 : 50 (2%)
Oils according to the specification
JASO FC or FD, recommended oil
Castrol
ACT>EVO
Propeller
manufacturer:
Technoflug Leichtflugzeugbau GmbH.
D-78713 Schramberg, Germany
Propeller
model:
KS-1G-160-R-120
or Propeller
manufacuter:
Binder Motorenbau GmbH
D-97645 Ostheim v.d. Rhön, Germany
Propeller
model:
BM-G-160-R-120-1
Reduction ratio:
1 : 2.75
Fuel capacity:
See table below
Tank in fuselage
Tank(s) in inboard wing panels
Total capacity incl.
optional tank
starbd. side
port side
- OPTION -
US IMP US IMP US IMP US IMP
Liter Gal Gal Liter Gal Gal Liter Gal Gal Liter Gal Gal
Fuel capacity
15.9
4.2
3.5
13.0
3.4 2.9 13.0 3.4 2.9 41.9
11.1 9.2
Usable fuel
15.7
4.1
3.5
12.5
3.3 2.7 12.5 3.3 2.7 40.7
11.5 9.6
Non-usable fuel
0.2
0.05 0.04
0.5
0.13 0.11 0.5 0.13 0.11 1.2 0.3 0.3
October 2011
Revision --
appr. 2.4