(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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A

C.
D.
E.
F.
757
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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本文鏈接地址：757 AMM 飛機維護手冊 儀表 CHAPTER 31 - INSTRUMENTS 2(101)