(8)  
AMM 23-43-00/501, Ground Crew Call System
 (9)  
AMM 24-22-00/201, Electrical Power - Control
 (10)
 AMM 26-11-00/501, Engine Fire Detection System
 (11)
 AMM 26-15-00/501, APU Fire Detection System
 (12)
 AMM 26-16-00/501, Lower Cargo Compartment Smoke Detection System
 (13)
 AMM 27-48-00/501, Stabilizer Trim Position Indicating System
 (14)
 AMM 27-61-00/201, Spoiler/Speedbrakes System
 (15)
 AMM 29-11-00/201, Pressurize/Depressurize Main Hydraulic System
 (16)
 AMM 31-41-00/201, Engine Indication and Crew Alerting System
 (17)
 AMM 31-51-04/401, Warning Electronics Unit Card Modules
 (18)
 AMM 32-09-02/201, Air/Ground Relays
 (19)
 AMM 34-11-00/201, Pitot-Static System
 (20)
 AMM 34-12-00/501, Air Data Computing System or 34-26-00/501
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C. 
D. 
E. 
F. 
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MAINTENANCE MANUAL
 (21)
 AMM 34-33-00/201, Radio Altimeter System
 (22)
 AMM 34-46-00/501, Ground Proximity Warning SystemAccess
 (1)  
Location Zones 211/212 Flight Compartment
Prepare for Test
 S 865-580
 (1)  
Supply electrical power (AMM 24-22-00/201).
S 865-152
 (2)  
Make sure that the six EICAS circuit breakers are closed.
S 865-004
 (3)  
Do the procedure for the removal of the EICAS Engine Shutdown Inhibit (AMM 31-41-00/201).
S 485-005
 (4)  
Connect the RA test set to the left radio altimeter transceiver in
 the E/E compartment (AMM 34-33-00/201).Master Warning/Caution Light Test
 S 865-007
 (1)  
On the right overhead light control panel, push the TEST switch.
S 755-026
 (2)  
On the glareshield, make sure that the captain's and first officer's WARNING and CAUTION lights come on.
S 755-027
 (3)  
On the instrument panel, make sure that the red CONFIG light comes on.
S 865-010
 (4)  
On the right overhead light control panel, push the TEST switch to
 remove the electrical power from the test circuits.Power Supply Fault Indicators Test
 S 865-153
 (1)  Open these P11 panel circuit breakers:
 (a)  
11B18, WARN ELEX B
 (b)  
11J33, WARN ELEX A
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本文链接地址:757 AMM 飞机维护手册 仪表 CHAPTER 31 - INSTRUMENTS 2(101)