rickyrhodesii
Well-Known Member
I posted this in a different forum, but this is probably the most appropriate place for it.
Could anyone elaborate or point me to a reference on the C172 brake system?
The only information I can find on the brake system in the information manual. I understand the 172's hydraulic system is comprised of a hydraulically-actuated brake on each main landing gear. You push on the top of either rudder pedal and the brake discs engage and slow the plane.
How much pressure can the system withstand? What is the normal operating pressure range? Schematics anyone?
Any help would be greatly appreciated!
Could anyone elaborate or point me to a reference on the C172 brake system?
The only information I can find on the brake system in the information manual. I understand the 172's hydraulic system is comprised of a hydraulically-actuated brake on each main landing gear. You push on the top of either rudder pedal and the brake discs engage and slow the plane.
How much pressure can the system withstand? What is the normal operating pressure range? Schematics anyone?
Any help would be greatly appreciated!