AIRCRAFT
Hydraulic Power
DA 42 NG AMM
Page 234
15 Mar 2018
29-10-00
Doc # 7.02.15
Rev. 4
(2) Detailed Check
Static (landing gear extended, ELECT. MASTER switch ON / set GEAR circuit breaker):
)
Max. leakage 1 drop of fluid in 10 hours.
Dynamic (after 25 extend/retract cycles):
)
Max. leakage 1 drop of fluid.
Note:
If one of the measurements don’t comply with these set-points send the actuator
to the vendor for a repair. Otherwise you can continue the operation but observe
the situation.
E. Pump Pressure Switch and Pressure Limitation Valve Operation Test
(1) Equipment
Item
Quantity
Part Number
Airplane jacks.
3
Commercial.
Wing trestle.
2
Commercial.
Rear fuselage trestle.
1
Commercial.
Manometer to test hydraulic pressure.
1
X11-P001.
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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