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时间:2011-10-30 09:57来源:蓝天飞行翻译 作者:航空
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___________________________________________
 1.  General_______
 A.  This procedure contains the following tasks:
 (1)  
Antiskid System Operational Test - Power Distribution and Indication

 (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


 

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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 

AUTOBRAKE SELECTOR 
PANEL ON PILOTS' CENTER 
INSTRUMENT PANEL (P1-3) 

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 

Antiskid/Autobrake System Adjustment/Test
Figure 501 (Sheet 1)

 

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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)

 

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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

 

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