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7.8 CANOPY, REAR DOOR, AND CABIN INTERIOR
Front canopy
The front canopy is closed by pulling down on the canopy frame, following which it is locked by means of a handle on the left hand side of the frame. On locking, steel bolts lock into mating holes in polyethylene blocks.
“Cooling Gap” position: A second setting allows the bolts to lock in, leaving a gap under the forward canopy.
The canopy can be blocked by a locking device on the left side near the canopy opening lever by turning the key clockwise. The closed and blocked canopy can be opened from inside by pulling the lever inside the opening handle.
WARNING
The airplane may be operated with the front canopy in the “cooling gap” position on the ground only. Before take-off the front canopy must be completely closed and locked.
Do not block the front canopy with the locking key before flight in order to assure emergency evacuation from outside.
A window on the left and right hand side of the canopy can be opened for additional ventilation or as an emergency window.
Rear door
The rear door is closed in the same way, by pulling down on the frame and locking it with the handle. A gas pressure damper prevents the door from dropping; in strong winds the assembly must be securely held. The rear door is protected against unintentional opening by an additional lever.
The door can be blocked by a locking device on the left side near the door opening lever by turning the key clockwise. The closed and blocked door can be opened from inside by pulling the lever inside the opening handle.
WARNING
Do not block the door with the locking key before flight in order to assure emergency access from outside.
Heating and ventilation
Heating and ventilation are operated using two levers located on the small center console under the instrument panel.
Right lever: up = HEATING ON (Seats, Floor) down = HEATING OFF
Center lever : up = DEFROST ON (Airflow to canopy) down = DEFROST OFF
The heat of the RH engine is used for the front seats and floor, the heat of the LH engine is used to defrost the canopy.
The Air inlet for the Ventilation System is placed on the underside of the RH wing, inboard of the engine nacelle. The air is distributed within the cabin via 6 nozzles (2 on the instrument panel LH/RH side, 2 on the overhead panel and 2 on the LH/RH side of the passenger compartment). The jet direction of each cone can be changed easily and the jet intensity can be regulated by rotation of the nozzle.
Doc. No. 7.01.05-E Rev. 5 15-Nov-2007 Page 7 - 23
7.9 POWER PLANT
7.9.1 ENGINES, GENERAL
There are two Thielert Aircraft Engines TAE125 installed, which have the following principal specifications:
-Liquid-cooled four-cylinder four-stroke Diesel-cycle engine with wet sump
lubrication -Inline construction -Common rail direct injection -Propeller speed reducing gear 1:1.69 -Digital Engine Control with Integrated Propeller Governor (separate oil system) -Turbo charger with Intercooler
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