Aquila A211 Instructions d'exploitation Page 14

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Aviation
AIRPLANE FLIGHT MANUAL
AQUILA AT01
Section 1
GENERAL
Dokument No.: Issue: Supersedes Issue: Date: Page:
FM-AT01-1010-100E
A.12 A.08 (30/06/2005) 17/09/2008 1 - 6
1.6 ENGINE
The ROTAX
®
912 S3 is a 4-cylinder 4-stroke engine with ram air cooled and horizontally
opposed cylinders as well as liquid cooled cylinder heads.
The Propeller is driven via an internal reduction gearbox with an integrated overload
clutch and a hydraulic constant speed propeller governor.
Reduction Ratio of internal gearbox: 2.43 : 1
Displacement: 1352 cm³
Take-Off Performance: 69.0 kW
at a Propeller Shaft Speed of 2263 1/min
1.7 PROPELLER
Two-blade, constant speed propeller manufactured by mt-Propeller Entwicklung GmbH.
Type: MTV-21-A/175-05
Hydraulically Controlled Variable
Pitch (Constant Speed) Propeller
Max. Propeller Diameter: 175 cm
1.8 FUEL
The following fuel grades are approved for usage (min. RON 95):
EN228 Premium
EN228 Premium plus
AVGAS 100LL
Left Fuel Tank Right Fuel Tank
Fuel Capacity (total): 60 60 Litres
Usable Fuel (total) : 54.8 54.8 Litres
Unusable Fuel: 5.2 5.2 Litres
Due to the higher lead content in AVGAS, the wear of the valve seats, the deposits in
the combustion chamber and lead sediments in the lubrication system will increase
when using this type of fuel. Therefore, use AVGAS only if you encounter problems with
vapour lock or if the other fuel types are not available (refer also to the Operators
Manual for ROTAX Engine Type 912 Series, latest revision).
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