landing gear Flashcards
which hyd sys is used during normal landing gear extension and retraction
3 had system
with the aircraft on the ground what is incorporated within the landing gear control lever to prevent an up selection
a solenoid lock
during the landing gear retraction sequence why is HYD pressure routed to activate the brake control valve
to stop NOSE wheel rotation
what means is provided to mute the landing gear horn
horn mute SWlight on the landing gear control panel
where are the landing gear position and status page displayed
EICAS pri page
the ALTernate landing gear extention method should be used in case of a failure in the landing gear control system
3 hydraulic system
pulling the landing gear manual release handle will permit the main landing gear to extend and lock into position
using gravity and down lock assist actuator force from the #2 HYD system
what powers the wheel brakes
3 HYD inboard brakes #2 HYD outboard brakes
where is brake pressure displayed
EICAS HYD synoptic page
when the parking brake is applied with all HYD pumps OFF hydraulic pressure is trapped within which brake system for prolonged period of time
the INBOARD breaks
the BTMS Brake Temp Monitoring System
Monitors the Temp of each brake and the information is displayed on EICAS
Provided the anti skid system is armed when does it become operational
@35 Knots wheel spin up signal and WOW after 5 seconds delay
the steering tiller nose wheel turn how many degrees
80 L eft and 80 right of center
the strike indicator located in the FWD end of the tail bumper assembly is there for
a visual indication of a tail strike
Flex take offs aren’t allowed if
anot skid is inop
