AIRCRAFT
Standard
Practices/Structures
DA 42 NG AMM
Page 4
15 Mar 2018
51-00-00
Doc # 7.02.15
Rev. 4
4. Sandwich Construction
Many of the components in the DA 42 NG have a sandwich of two skins and a core. GFRP or CFRP
make the skins and rigid foam makes the core.
The skins must bond to the core of a sandwich structure completely. If the skins do not bond to the
core the component can fail.
5. Bonded Components
A number of components can bond together to make a larger component. Special thick resin bonds
these components together and fills the gap in a joint.
6. Repair Limitations
Repairs which are categorized as 'Class 1' in accordance with Section 51-10, Paragraph 2, may only
be carried out in accordance with a repair scheme which has been approved by Diamond Aircraft
Industries. Such repairs are not described in the Airplane Maintenance Manual (AMM).
Repair work on these components is not permitted:
)
Radome (nose cone, if OÄM 42-119 or OÄM 42-273 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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