what emergency systems are used in modern aircraft designs to provide a safe provision of hydraulic service when normal operating systems fail
؟؟
EACH MODREN AIRCRAFT HAS MORE THAN ONE HYD. SYSTEM AND
THERE IS ALWAYS A PRESENT OF BACKUP SYSTEMS POWRED MOSTLY BY ELECTRIC SYS.
e.g.
IN THE 737-300
THERE ARE TOW ELECTRIC DRIVEN *****, ONE FOR EACH SYSTEM A AND B
2
in the event of hydraulic system leak,what would be the physical consequences to the operating of the system and
what system indication would the pilot receive
؟؟
1- SWITCH THE FAILUAR SYSTEM TO OFF POSITON
FOR INDICATION
LOW PRESSURE AMBER LIGHT ILLUMINATE
AND
OVERHEAT ALSO ILLUMINATE
FOR MORE DETAILS ABOUT
HYD. SYS.
(737-300)
LOOK AT THIS