AIRCRAFT
Standard
Practices/Structures
DA 42 NG AMM
Page 16
15 Mar 2018
51-60-00
Doc # 7.02.15
Rev. 4
Pivot Axis
Moment Arm
Spring
Balance
Moment Arm
Pivot Axis
Horizontal
Hinges
Horn
8. Wing Inner Flap Static Balance
Refer to Figure 7 or 8 for the weight and residual moment.
Use any suitable method to support the inner flap horizontally at the pivot axis. The inner flap must be
able to rotate freely around the pivot axis.
The balance includes the horn and hinges.
The residual moment is tail heavy.
Figure 13: Wing Inner Flap Static Balance
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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