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Page Title:
Appendix G: CONVERTING THE OV-1 AIRCRAFT HYDRAULIC SYSTEMS FROM MIL-H-5606 TO MIL-H-83282 HYDRAULIC FLUID (Cont) |
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 TB 55-1500-334-25
G-11. Reconnect the number 1 and number 2 engine
G-9. After all systems are flushed, disconnect the D6A
discharge line from the pressure line at the reservoir.
hydraulic pump discharge lines.
G-10. Fill the reservoir with MIL-K 83282 hydraulic
G-12. Bleed the right and left brakes at the wheel
cylinder bleed ports.
fluid. Motor each engine to clean up the suction lines to
the hydraulic pumps.
G-13. Remove the aircraft from the jacks.
Change 2
G-2
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