(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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ALL ú ú 01 Page 501 ú May 28/02
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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ALL ú ú 01 Page 502 ú Jan 20/99
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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)