通航信息_通航_通用航空_General Aviation

7.5 LANDING GEAR........................................ 14

7.6 SEATS AND SAFETY HARNESSES ........................ 20

7.7 BAGGAGE COMPARTMENT.............................. 22

7.8 CANOPY, REAR DOOR, AND CABIN INTERIOR .............. 22

7.9 POWER PLANT ........................................ 24

7.9.1  ENGINES, GENERAL............................... 24

7.9.2  PROPELLER ..................................... 25

7.9.3  OPERATING CONTROLS ........................... 28

7.9.4  ENGINE INSTRUMENTS ............................ 32

7.9.5 FUEL SYSTEM.................................... 34

7.9.6 COOLING SYSTEM ................................ 45

7.9.7 OIL SYSTEMS .................................... 46

7.9.8 TURBO-CHARGER SYSTEM......................... 47

7.9.9 FIRE DETECTION SYSTEM ......................... 48

7.10 ELECTRICAL SYSTEM .................................. 49

7.10.1  GENERAL....................................... 50

7.10.2  ENGINE CONTROL UNIT / ECU ..................... 56

7.10.3 WARNING, CAUTION AND ADVISORY MESSAGES ..... 58
7.11 PITOT-STATIC SYSTEM ................................. 64

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7.12 STALL WARNING SYSTEM ............................... 64

7.13 GARMIN G1000 INTEGRATED AVIONICS SYSTEM ........... 65

7.13.1   GENERAL ....................................... 65

7.13.2   PRIMARY FLIGHT DISPLAY (PFD) ................... 66

7.13.3  MULTI-FUNCTION DISPLAY (MFD)................... 68

7.13.4   AUDIO PANEL ................................... 69

7.13.5  ATTITUDE AND HEADING REFERENCE SYSTEM (AHRS) ................................................ 69
7.13.6   AIR DATA COMPUTER (ADC) ....................... 69

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7.1 INTRODUCTION
Chapter 7 contains a description of the airplane and its systems, together with operating instructions.
For details about optional equipment see Chapter 9.
7.2 AIRFRAME
Fuselage
The CFRP fuselage is of semi monocoque molded construction. The center wing is attached to the fuselage with bolts. The two main spars and both nacelles are part of the center wing. The two main spars are CFRP items. The engine compartment in each nacelle is separated from the other structure with a firewall. The fire protection on the firewall is of a special fire-resistant matting, which is covered on the engine side by stainless steel cladding.
Wings
The wings have a front and rear spar; each wing has a top shell and a bottom shell; The whole wing is 'fail-safe' design. The wings, as well as the ailerons and flaps, are made of GFRP/CFRP, and are principally of sandwich construction. An aluminum fuel tank is installed in each of the wings.
　
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