Across
- 2. In the reservoirs these should stop fluid loss at 20%.
- 5. Impact that a dual hydraulic failure would have on the aircraft.
- 6. Panel where the 4 hydraulic switches are located.
- 7. Number of independent hydraulic systems.
- 9. Transfers System A pressure to System B in certain situations.
- 10. Impact would a single hydraulic failure have on the aircraft.
Down
- 1. Three thousand (3000) psi is normal _______ for the hydraulic system.
- 3. Hydraulic system used for normal landing gear extension and retraction.
- 4. Source of power for standby hydraulic system.
- 8. Is used to cool the hydraulics via a heat exchanger.