TCH.1C-27J-2-29JG
CAUTION
––––––––––––––––––––––––––––––––––
Avoid hydraulic fluid spilling using a
clean cloth. This will reduce fluid
leakage.
––––––––––––––––––––––––––––––––––
12.Set up the hydraulic test stand (AGE NO. 00262) as
follows: delivery pressure 900 psi (63.3 kg/ cm
²
).
CAUTION
––––––––––––––––––––––––––––––––––
Check for absence of air bubbles in the
fluid flow.
––––––––––––––––––––––––––––––––––
13.Annul the hydraulic pressure in the No.1 (No. 2)
hydraulic system.
14.Connect the external electrical supply to the aircraft
(refer to manual
) .
15.Electrically open the Fire Shut-Off valve.
16.Disconnect the external electrical supply to the aircraft
(refer to manual
) .
17.Refill the reservoir with the used hydraulic fluid (LCM
NO. 00043) (refer to manual
).
18.Close the access panels 414D, 414J (424D,424J) and
913A, 913B.
19.Remove maintenance platform (AGE NO. 00074).
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