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DA 42 NG AMM
Detail Steps/Work Items
Key Items/References
Page 210
15 Mar 2018
34-10-00
Doc # 7.02.15
Rev. 4
(12)
Disconnect the Pitot-static probe adaptor and
install a blanking cap, with pennant, onto the
airplane Pitot static probe.
(13)
Remove the blockage of the static line.
At the filter on top of the fuselage.
(14)
Install the aft baggage compartment.
Refer to Section 25-50.
Table 1: Altimeter Indication Error
Altitude
Permissible Error
-1000 ft.*
±20 ft.*
Sea level.
±20 ft.
4,000 ft.
±35 ft.
8,000 ft.
±60 ft.
12,000 ft.
±90 ft.
16,000 ft.
±110 ft.
20,000 ft.
±130 ft.
* Only required for airplanes for which 14 CFR § 91.411 and 14 CFR § 91.411 part 43 Appendix E
is applicable.
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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