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TCH.1C-27J-2-27JG
5.After the installation of any component in the hydraulic
system, restore the fluid level in the reservoirs and
carry out a complete cycle of manoeuvres of the
relevant system before the next flight.
6.Cap the disconnected hydraulic tubes immediately
after removing the component. After having fitted the
hydraulic component, fill and bleed the system,
pressurise it and check for leaks.
7.If particular hydraulic contamination event occurs,
check and clean internal filters.
8.Hydraulic fluid is acid. Prevent contact with skin.
Screw tops must be fixed on pipes after removal.
9.In many cases, corrosion results from fingerprints
caused by careless handling. Avoid handling the units
when not necessary and keep all disassembled parts
submerged in preservative oil (LCM NO. 00088).
27-00-00
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