Sennheiser SI 234 - ANNEXE 802 Operations Instructions Page 349

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DA 42 NG AFM Airplane Description
Doc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 7 - 1
CHAPTER 7
DESCRIPTION OF THE AIRPLANE
AND ITS SYSTEMS
Page
7.1 INTRODUCTION .......................................7-3
7.2 AIRFRAME ............................................7-3
7.3 FLIGHT CONTROLS ....................................7-4
7.4 INSTRUMENT PANEL ..................................7-11
7.5 LANDING GEAR.......................................7-13
7.6 SEATS AND SAFETY HARNESSES .......................7-19
7.7 BAGGAGE COMPARTMENT.............................7-21
7.8 CANOPY, REAR DOOR, AND CABIN INTERIOR .............7-21
7.9 POWER PLANT .......................................7-25
7.9.1 ENGINES, GENERAL..............................7-25
7.9.2 PROPELLER ....................................7-26
7.9.3 OPERATING CONTROLS ..........................7-29
7.9.4 ENGINE INSTRUMENTS ...........................7-33
7.9.5 FUEL SYSTEM ...................................7-35
7.9.6 COOLING SYSTEM ...............................7-45
7.9.7 OIL SYSTEMS ...................................7-46
7.9.8 TURBO-CHARGER SYSTEM ........................7-47
7.9.9 FIRE DETECTION SYSTEM ........................7-48
7.10 ELECTRICAL SYSTEM .................................7-49
7.10.1 GENERAL......................................7-50
7.10.2 ELECTRICAL ENGINE CONTROL UNIT / ECU .........7-56
7.10.3 WARNING, CAUTION AND ADVISORY MESSAGES ....7-58
7.11 PITOT-STATIC SYSTEM ................................7-64
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