(2)  
Antiskid System Operational Test - Brake Application
 (3)  
Antiskid System Operational Test - Transducer Spinup
 (4)  
Autobrake System Operational Test - Control, Speedbrake Switch, Landing Gear Down and Locked
 (5)  
Autobrake System Operational Test - Autobrake Application
 (6)  
Autobrake System Operational Test - RTO (Refused Take Off)
 B.  
Each of the tests can be done separately as necessary to do an operational check of that part of the system. All of the tests can be done to do a complete operational check of the system.
 C.  
It is necessary to operate test switches on the Antiskid/Autobrake Control Unit (M102) in the Main Equipment Center to do this test. You can get access to the control unit through the electronics access door, 119AL (AMM 06-41-00).
 D.  
These indicator lights and EICAS displays give fault indications for the system:
 (1)  
An ANTISKID light on the pilot's overhead panel P5.
 (2)  
An AUTOBRAKES light on the pilot's center instrument panel (P1-3).
 (3)  
Two EICAS display units on panel P2 to give the caution and advisory message, and the status and maintenance formats.
 TASK 32-42-00-945-213
 2.  Prepare for the Tests______________________
 A.  References
 (1)  
AMM 06-46-00/201, Entry, Service, and Cargo Doors (Major Zone 800) Access Doors and Panels
 (2)  
AMM 24-22-00/201, Electrical Power - Control
 (3)  
AMM 25-50-03/401, Bulkhead Lining
 (4)  
AMM 29-11-00/201, Pressurize/Depressurize Main Hydraulic System
 (5)  
AMM 32-00-20/201, Landing Gear Down Locks
 (6)  
AMM 34-21-00/501, Inertial Reference System
 
 32-42-00
 ALL  ú ú 02 Page 501 ú May 28/00 
 
A
757 
MAINTENANCE MANUAL
SEE C P11 PANEL 
SEE  B  P5 PANEL  PANEL MAINTENANCE EICAS  ALTN  w  
SEE  A  PANEL P61  w  
SEL SWITCH ON P1-1, AND P3-3 IRS INSTR SOURCE  
SEE  E  SEE  D  A  
FLT COMPT  
L a aDC FAIL ON DC FAULT ALIGNw a NAV ATT OFF ALIGN  C a aDC FAIL ON DC FAULT ALIGNw a NAV ATT OFF ALIGN  ATT R a aDC FAIL ON DC FAULT ALIGNw a NAV OFF ALIGN  WARNING & CAUTION  1 327 EGT 327 1.0 97.5 N EPR 1.4 1.8 1.28 CLB 1.65 1.0 1.4 1.8 1.28 97.5 1.65 TAT +12C  LIGHT AUTOBRAKES BRAKES AUTO AUTOBRAKES AUTO MAX 4 321 DISARM OFF 
IRS MODE SELECT  
SWITCH ON P5  RTO  
B  
AUTOBRAKE SELECTOR  
PANEL ON PILOTS' CENTER  
INSTRUMENT PANEL (P1-3)  
E  
ENTRY EMER  CARGO  ACCESS  
DOORS  DOORS  DOORS  DOORS  
CAPT PITOT  PITOT F/O  L AOA  R AOA  
PITOT L AUX  PITOT R AUX  TAT  
TRIM STAB  SPOILERS  SPD BRK AUTO  SPD TRIM MACH/  EICAS DISPLAY UNITS ON P2  
STAB UNSCHED TRIM  RATIO RUDDER  SKID ANTI  PRESS ELEV  D  
ANTISKID  
MISC ANNUNCIATOR ON P5  LIGHT  
C 
Antiskid/Autobrake System Adjustment/Test 
Figure 501 (Sheet 1)
 32-42-00
 ALL  ú ú 04 Page 502 ú Jun 15/85 
 
A 
757 
MAINTENANCE MANUAL
CONTROL UNITE5 RACK ACCESS PANEL SEE
ANTISKID/AUTOBRAKE CONTROL UNIT, M102 
CONTROL PANEL
Antiskid/Autobrake System Adjustment/Test 
Figure 501 (Sheet 2)
 32-42-00
 ALL  ú ú 11 Page 503 ú May 28/99 
 
A
757 
MAINTENANCE MANUAL
HYDRAULIC LINE 
HYDRAULIC BLEED PORT 
MAIN GEAR BRAKE 
AXLE 
FWD HYDRAULIC BRAKE BLEED EXAMPLE BRAKE BLEED ANTISKID PORT 
A 
TRANSDUCER SEE A 
SEE B 
ANTISKID 
ANTISKID 
TRANSDUCER 
TRANSDUSER 
ASSEMBLY 
SPINUP EQUIPMENT WHEEL 
DOG 
ANTISKID TRANSDUCER 
AND SPIN-UP EQUIPMENT
B
Brake Bleed Ports and Antiskid Transducer 
Figure 502
 32-42-00
 ALL  ú ú 01 Page 504 ú Dec 20/90 
 
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:757 AMM 飞机维护手册 起落架 CHAPTER 32 - LANDING GEAR 3(10)