• Home
  • Download PDF
  • Order CD-ROM
  • Order in Print
1-58 SERVICE ROTARY-WING SHOCK ABSORBER    (Continued) - TM-55-1520-240-23-1_252
POWER SERVICE UTILITY HYDRAULIC SYSTEM RESERVOIR

TM-55-1520-240-23-1 UH-1H/V and EH-1H Aircraft Manual
Page Navigation
  215    216    217    218    219  220  221    222    223    224    225  
TM 55-1520-240-23-1 1-58 SERVICE ROTARY-WING SHOCK ABSORBER    (Continued) 1-58 5. Add hydraulic fluid (E197) through filler (7). Wear gloves (E186). 6. Check fluid level in indicator (3) again. a. If added fluid remains in indicator, add more fluid (E197) until fluid level is at top of bull’s-eye (5). b. If added fluid disappears from indicator, add fluid (E187) at filler (7) to top of bull’s-eye (5). Then bleed shock absorber (Task 5-92). 7. Install cap (6). 8. Lockwire cap (6).  Use lockwire (E231). INSPECT FOLLOW-ON MAINTENANCE: Remove tiedown line (Task 1-26). Close work platforms (Task 2-2). END OF TASK 1-226 Change 3







Western Governors University

Privacy Statement
Press Release
Contact

© Copyright Integrated Publishing, Inc.. All Rights Reserved. Design by Strategico.