AIRCRAFT
Wings
DA 42 NG AMM
Detail Steps/Work Items
Key Items/References
Page 210
15 Mar 2018
57-10-00
Doc # 7.02.15
Rev. 4
(15)
Do an inspection of the flap controls which you
have connected or adjusted.
S
If necessary for your Airworthiness
Authority, do a second inspection of the
controls.
(16)
Do a test for correct operation and range of
movement of the aileron system. If necessary,
adjust the aileron system.
Refer to Section 27-10.
(17)
Do an inspection of the aileron controls which
you have connected or adjusted.
S
If necessary for your Airworthiness
Authority, do a second inspection of the
controls.
(18)
Do a functional check of these lights:
S
Position lights.
S
Strobe lights (ACLs).
Refer to Section 33-40.
(19)
Do a Pitot and static system leak test.
Left wing only.
Refer to Section 34-10.
(20)
Refuel the airplane to the unusable fuel level.
Refer to Section 12-10.
(21)
Do a fuel quantity indication calibration check.
Refer to Section 28-40.
(22)
Do a check flight.
Refer to the DA 42 NG Airplane Flight
Manual.
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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