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钻石42飞机飞行手册 DA 42 Airplane Flight Manual(14)

时间:2011-10-28 13:17来源:蓝天飞行翻译 作者:admin
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15  4.0 
20  5.3 
25  6.6 
30  7.9 
35  9.2 
40  10.6 
45  11.9 
50  13.2 
60  15.9 
70  18.5 
80  21.1 
90  23.8 
100  26.4 
110  29.1 
120  31.7 
130  34.3 
140  37.0 
150  39.6 
160  42.3 
170  44.9 
180  47.6 

US Gallons  Liters 
1  3.8 
2  7.6 
4  15.1 
6  22.7 
8  30.3 
10  37.9 
12  45.4 
14  53.0 
16  60.6 
18  68.1 
20  75.7 
22  83.3 
24  90.9 
26  98.4 
28  106.0 
30  113.6 
32  121.1 
34  128.7 
36  136.3 
38  143.8 
40  151.4 
45  170.3 
50  189.3 

 

General
DA 42 AFM

 

1.7 THREE-VIEW DRAWING
' ' ' ' ' ' ' ' '
1735 mm (5 ft 8 in) 2950 mm(9 ft 8 in)
8560 mm (28 ft 1 in)
13420 mm (44 ft 0 in) 13550 mm (44.5 ft) including ACL

'

' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' '
2205 mm (7 ft 3 in)
1950 mm (6 ft 5 in)
2490 mm (8 ft 2 in)

Page 1 - 18
Rev. 5 15-Nov-2007
Doc. No. 7.01.05-E

 

1.8 G1000 AVIONICS SYSTEM

1.
The G1000 Integrated Avionics System is a fully integrated flight, engine, communication, navigation and surveillance instrumentation system. The system consists of a Primary Flight Display (PFD), Multi-Function Display (MFD), audio panel, Air Data Computer (ADC), Attitude and Heading Reference System (AHRS), engine sensors and processing unit (GEA), and integrated avionics (GIA) containing VHF communications, VHF navigation, and GPS (Global Positioning System).

2.
The primary function of the PFD is to provide attitude, heading, air data, navigation, and alerting information to the pilot. The PFD may also be used for flight planning. The primary function of the MFD is to provide engine information, mapping, terrain information, and for flight planning. The audio panel is used for selection of radios for transmitting and listening, intercom functions, and marker beacon functions.

3.
The primary function of the VHF Communication portion of the G1000 is to enable external radio communication. The primary function of the VOR/ILS Receiver portion of the equipment is to receive and demodulate VOR, Localizer, and Glide Slope signals. The primary function of the GPS portion of the system is to acquire signals from the GPS satellites, recover orbital data, make range and Doppler measurements, and process this information in real-time to obtain the user*s position, velocity, and time.
 
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