曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
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
Displacement: ' TAE 125-01 engine: 1689 cm3 (103 in3) ' TAE 125-02-99 engine (M.M 42-198 carried out): 1991 cm3 (121.5 in3)
Max. power: 99 kW (135 DIN-HP) at 2300 RPM at sea level and ISA
Max. continuous power: 99 kW (135 DIN-HP) at 2300 RPM at sea level and ISA
The indications for monitoring important engine parameters during operation are integrated within the Garmin G1000 display. Each engine can only be operated with the ENGINE MASTER switch ON. Each engine has an own ECU (Engine Control Unit) which receives its electrical power from the generator when at least one engine is running. When both engines are at standstill, the ECU receives its electrical power from the battery.
中国通航网 www.ga.cn
通航翻译 www.aviation.cn
本文链接地址：钻石42飞机飞行手册 DA 42 Airplane Flight Manual(100)
|
