AIRCRAFT
DA 42 NG AMM
Landing Gear
Doc # 7.02.15
Rev. 4
32-60-00
Page 1
15 Mar 2018
Section 32-60
Position and Warning
1. General
This Section tells you about the parts of the landing gear system that give the pilot position and
warning data. Refer to these Sections for the related data:
)
Section 32-10. Main landing gear.
)
Section 32-20. Nose landing gear.
)
Section 32-30. Extension and retraction.
)
Section 32-50. Nose wheel steering.
2. Description
The landing gear position and warning system has these functions:
)
Landing gear control.
)
Landing gear position.
)
Landing gear warning.
)
To give position data for the extension and retraction system.
The system has these components:
)
A cockpit selector handle and indicators. The cockpit selector handle controls the position of the
landing gear. The indicators show the position/condition of the landing gear legs.
)
Switches that sense 'weight-on-wheels'.
)
Switches that sense 'folding-stay locked'.
)
Switches that sense 'landing gear retracted'.
)
Switches that sense the position of the engine power levers.
)
Control relays and circuit breakers.
Figure 1 shows the landing gear electrical system schematic diagram.
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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