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1-58 SERVICE ROTARY-WING SHOCK ABSORBER    (Continued) - TM-55-1520-240-23-1_253
POWER SERVICE UTILITY HYDRAULIC SYSTEM RESERVOIR    (Continued) - TM-55-1520-240-23-1_255

TM-55-1520-240-23-1 UH-1H/V and EH-1H Aircraft Manual
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TM 55-1520-240-23-1 1-59 POWER SERVICE UTILITY HYDRAULIC SYSTEM RESERVOIR 1-59 INITIAL SETUP Applicable Configurations: All Tools: Hydraulic Test Stand or AGPU Thermometer Aircraft Mechanic’s Tool Kit, NSN 5180-00-323-4692 Materials: Hydraulic Fluid (E199) Goggles (E473) Personnel Required: CH-47 Helicopter Repairer Aircraft Pneudraulics Repairer References: TM 1-1520-240-10 TM 55-1730-229-12 TM 55-4920-335-14 TM 55-4920-373-14&P Equipment Condition: Battery Connected (Task 1-39) Electrical Power Off Hydraulic Power Off Hydraulic Connection Access Panel Open (Task 2-2) Cargo  Ramp  Fully  Up  or  Full  Down  (TM 55-1520-240-T) Utility Hydraulic System Depressurized (Task 7-135.1) WARNING Make sure all connections are tight before operating hydraulic test stand. High-pressure fluid from test stand can injure personnel. WARNING Hydraulic fluid (E199) is toxic.  It can irritate skin and cause burns.  Avoid inhaling.  Use only with adequate ventilation.  Avoid contact with skin, eyes, or clothing.  In case of contact, immediately flush skin or eyes for at least  15 minutes.  Get medical attention for eyes. 1. Remove dust cover (1) from utility system pressure connection (2). 2. Connect test stand pressure line (3) to utility pressure connection (2). Change 3 1-227







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