AIRCRAFT
Hydraulic Power
DA 42 NG AMM
Page 228
15 Mar 2018
29-10-00
Doc # 7.02.15
Rev. 4
B. Emergency Operation Function Test of the Hydraulic System
(1) Equipment
Item
Quantity
Part Number
Airplane jacks.
3
Commercial.
Wing trestle.
2
Commercial.
Rear fuselage trestle.
1
Commercial.
(2) Emergency Extension Test
Detail Steps/Work Items
Key Items/References
WARNING:
TAKE PRECAUTIONS BY SECURING THE AREA AROUND THE
AIRPLANE BEFORE YOU PERFORM MAINTENANCE ON THE
LANDING GEAR. THE LANDING GEAR RETRACTION SYSTEM CAN
CAUSE SERIOUS INJURY TO PERSONS IF OPERATED
ACCIDENTALLY.
CAUTION:
MAKE SURE THAT THE AREA AROUND THE AIRPLANE IS CLEAR.
IF THE LANDING GEAR HITS AN OBJECT THE LANDING GEAR CAN
BE DAMAGED.
(1)
Pull the GEAR circuit-breaker.
Right side of the instrument panel.
(2)
Raise the airplane on jacks and move the wing
and rear fuselage trestles into position to support
the airplane.
Refer to Section 07-10.
(3)
Connect an external power supply to the
airplane.
Refer to Section 24-40.
(4)
Release the hydraulic pressure from the
hydraulic system:
S
Fold the rear passenger seat-backs forward.
S
Remove the rear baggage compartment
lower access panel.
Refer to Section 25-10.
Refer to Section 25-60.
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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