S 485-174
(3)
Install a brake pressure gage assembly in the bleed port of the number 1 wheel brake.
S 865-173
(4)
Pressurize the right hydraulic system and reservoir (AMM 29-11-00).
S 715-175
(5)
Put the autobrake selector switch on panel P1-3 to the RTO position and make sure that it stays in that position.
S 715-176
(6)
Put the brake test switch on the Antiskid/Autobrake Control Unit, M102, to the A/B position.
(7)
Push in and hold the ENABLE/VERIFY switch.
S 715-178
(8)
Push in the VERIFY switch and release the ENABLE/VERIFY and VERIFY switches.
S 715-177
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S 715-179
(9)
Make sure that you have these indications:
(a)
The M102 display shows BRK RTO.
(b)
Pressure indication on the brake pressure gage for wheel No. 1 brake goes to 2,900 |100 psi for approximately 15 seconds, and then decreases to less than 100 psi.
(c)
The autobrake selector switch on the P1-3 panel goes to the OFF position.
S 715-180
(10)
Put the brake test rotary switch on the M102 to the NORM position.
S 715-181
(11)
Push in and release the RESET button on the M102.
S 715-182
(12)
Remove power from the right and left hydraulic system (AMM 29-11-00).
S 715-183
(13)
Remove the brake pressure gage from wheel number 1 and put the brake bleed port back to the normal configuration.
TASK 32-42-00-945-184
9. Put the Airplane Back to Its Usual Condition____________________________________________
A. References
(1)
AMM 24-22-00/201, Electrical Power - Control
(2)
AMM 06-46-00/201, Entry, Service, and Cargo Doors (Major Zone 800) Access Doors and Panels
(3)
AMM 25-50-03/401, Bulkhead
(4)
AMM 29-11-00/201, Pressurize/Depressurize Main Hydraulic System
B.
Access
(1)
Location Zones
211 Control Cabin, Left
212 Control Cabin, Right
731 Landing Gear Left
741 Landing Gear Right
120 Main Equipment Center, Right
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(2)
Access Panel
119AL Main Equipment Center
C.
Procedure
S 865-185
(1)
Put the L, R and C IRUs to the OFF position.
S 865-186
(2)
Remove the power from the left and right hydraulic systems
(AMM 29-11-00).
S 085-187
(3)
Remove the brake pressure gages, if installed, and put the brake bleed port back to its usual condition.
S 865-188
(4)
Pressurize the right hydraulic system and reservoir (AMM 29-11-00).
S 865-189
(5)
Set the parking brake.
S 865-190
(6)
Push in the RESET button on the Antiskid/Autobrake Control Unit, M102 to clear the memory (the display will show MEM CLR).
S 415-201
(7)
AIRPLANES WITH ANTISKID/AUTO BRAKE CONTROL UNIT OF THE E5 RACK (FIG. 501); Do the steps that follows:
(a)
On the forward bulkhead in the forward cargo compartment, install the access panel for the E5 rack (AMM 25-50-03/401).
(b)
Close the forward cargo door, 821.
S 865-210
(8)
Remove the power from the right hydraulic system if it is not necessary (AMM 29-11-00).
(9)
Remove the electrical power if it is not necessary (AMM 24-22-00).
S 865-211
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ANTISKID/AUTOBRAKE SYSTEM - INSPECTION/CHECK
____________________________________________
1. General_______
A. This section contains these tasks:
(1)
An operational test of the thrust lever switch for a Refused Takeoff (RTO) configuration.
(2)
A test for correct operation and indications for part of the antiskid/autobrake system as follows:
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本文鏈接地址：757 AMM 飛機維護手冊 起落架 CHAPTER 32 - LANDING GEAR 3(19)
