XtremeAIR XA42, Руководство по эксплуатации самолета

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Airplane Flight Manual XA42
Page 7 Page date:
Chapter 07 09.11.2010
7.10.2 OIL SYSTEM
The oil is cooled by a two oil coolers mounted on the left and right hand side in the engine
compartment. The oil level is determined by a dipstick. A thermostatic valve is fitted upstream of the
oil cooler. This valve ensures a quick warmup of the oil after engine start.
Oil capacity and grades:
Maximum sump quantity: 15.15 L / 16 qt
Minimum sump quantity: 8.52 L / 9 qt
For oil temperatures and oil grades refer to chapter 1.
7.10.3 ENGINE INSTALLATION
The engine is attached to the steel tube engine mount using 4 shock mounts. The engine mount itself
is connected to the fuselage with 14 bolts on the firewall surface.
The cowling is separated in a lower and an upper part; both are carbon fiber / glass fiber reinforced
composites. The upper cowling houses a hatch to easily check the oil dipstick.
7.10.4 PROPELLER
The aircraft is equipped with a constant speed, 3 blade MTV-9-B-C/C203-20d propeller. The diameter
is 2030 mm. It is produced by MT Propeller Entwicklungs GmbH, blades are made out of wood and
composite.
7.10.5 THROTTLE
Parallel-motion control mounted on the left side of both cockpits.
7.10.6 MIXTURE
Vernier-control located at the left side of the rear cockpit (red knob).
7.10.7 RPM CONTROL
Vernier-control on the left side of the rear cockpit (blue knob).
Preselection of RPM possible due to constant speed governor.
7.10.8 EXHAUST SYSTEMS
The aircraft is equipped with an exhaust system that merges three pipes on each side of the engine
into one tail pipe on each side. These two tail pipes exit the cowling through special outlets.