AIRCRAFT
Heating and Ventilation
DA 42 NG AMM
Page 2
15 Mar 2018
21-CONTENTS
Doc # 7.02.15
Rev. 4
B. Cabin Ventilation/Cooling
Ambient air flows through a NACA duct at the lower surface of the right-side wing center-section.
In flight, ambient air flows through this NACA duct into the cabin ventilation/cooling system via
flexible hoses. The flow of air into the forward cockpit is controlled by outlets located in each side
of the instrument panel. The flow of air to the rear passenger area is controlled by air outlets
located in the cockpit instrument panel and the rear-cabin overhead-panel. The volume and
direction of the air flowing from the outlets can be controlled at the outlets.
Refer to Section 21-50 for more details about the RACC system (if OÄM 42-193/c or earlier is
installed).
Refer to Section 21-51 for more details about the RACC system (if OÄM 42-193/d or later is
installed).
Summary of Contents for DA 42 NG
Page 933: ...AIRCRAFT DA 42 NG AMM Fuel Doc 7 02 15 Rev 4 28 TITLE Page 1 15 Mar 2018 CHAPTER 28 FUEL ...
Page 1459: ...AIRCRAFT DA 42 NG AMM Lights Doc 7 02 15 Rev 4 33 TITLE Page 1 15 Mar 2018 CHAPTER 33 LIGHTS ...
Page 1711: ...AIRCRAFT DA 42 NG AMM Doors Doc 7 02 15 Rev 4 52 TITLE Page 1 15 Mar 2018 CHAPTER 52 DOORS ...
Page 1853: ...AIRCRAFT DA 42 NG AMM Wings Doc 7 02 15 Rev 4 57 TITLE Page 1 15 Mar 2018 CHAPTER 57 WINGS ...
Page 2071: ...AIRCRAFT DA 42 NG AMM Engine Doc 7 02 15 Rev 4 72 TITLE Page 1 15 Mar 2018 CHAPTER 72 ENGINE ...
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