AIRCRAFT
Hydraulic Power
DA 42 NG AMM
Detail Steps/Work Items
Key Items/References
Page 232
15 Mar 2018
29-10-00
Doc # 7.02.15
Rev. 4
(11)
Check operation of the protection valve on the
main control block:
S
Increase the pressure of the hydraulic system
to >180 bar (2610 PSI).
S
The protection valve should open and after
the valve closes and the pressure in the
hydraulic system is stabilized the pressure is
steady at 150 bar (2175 PSI).
Refer to Figure 4.
(12)
Move the wings and rear fuselage trestles clear
of the airplane.
(13)
Lower the airplane with the jacks.
Make sure that area around the airplane is clear.
(14)
Reset the GEAR circuit breaker.
Right side of instrument panel.
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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