AUTO GYRO CAVALON - Engine; Propeller; In-Flight Adjustment

Flight Manual
Cavalon
SECTION
1
GENERAL
RSUK0287_POH_Cavalon Revision 3.0, Issue Date 06.04.16 1-6
1.10 Engine
ROTAX 912 ULS
 4-cylinder, four-stroke spark-ignition engine with opposed cylinders
 Liquid cooled cylinder heads
 Air cooled cylinders
 Dry sump forced lubrication with separate oil tank
 Automatic valve adjustment by hydraulic tappet
 2 carburettors
 Mechanical and electrical fuel pump
 Electronic dual ignition
 Propeller speed reduction unit, engine mount assembly
 Electric starter (12V 0,6kW)
 Air intake system, exhaust system with muffler
 Slipper clutch
ROTAX 914 UL
 4-cylinder, four-stroke spark-ignition engine with opposed cylinders with turbo
charger
 Liquid cooled cylinder heads
 Air cooled cylinders
 Dry sump forced lubrication with separate oil tank
 Automatic valve adjustment by hydraulic tappet
 2 carburettors
 2 electrical fuel pumps
 Electronic dual ignition
 Propeller speed reduction unit, engine mount assembly
 Electric starter (12V 0,6kW)
 Air intake system, exhaust system
 Slipper clutch
1.11 Propeller
HTC 3 Blade
Airscrew with ground adjustable pitch made of CRP / GRP
Model ........................................................................ HTC 3 Blade 172 ccw 3B
Number of blades ........................................................................................... 3
Diameter ................................................................................................172 cm
In-flight pitch adjustment ........................................................................... none
IvoProp 3 blade
Airscrew with in-flight adjustable pitch
Model…………………………………………………………………………….DL3-68
Number of blades………………………………………………………………………3
Diameter……………………………………………………………………….172.7cm
In-flight adjustment……………………………………………….electrically actuated