................................................................................ |ATA Chapter-Sections | ATA TEXT | ................................................................................ |34-61 |FLIGHT MANAGEMENT (FMC/CDU) | ................................................................................ |35-11 |CREW OXYGEN | ................................................................................ |35-21 |PASSENGER, CREW REST, SUPERNUMERARY OXYGEN | ................................................................................ |36-11 |BLEED SYSTEM | ................................................................................ |36-12 |FAN AIR MODULATING VALVE and TEMP CONTROL SENSOR | ................................................................................ |36-21 |PRESSURE SENSORS | ................................................................................ |36-22 |BLEED-X TEMP SENSOR, OVERTEMP SWITCH and OVERPRESSURE | | |SWITCH | ................................................................................ |38-32 |WASTE TANK LEVEL SENSORS | ................................................................................ |45-45 |CENTRAL MAINTENANCE SYSTEM (CMC and TEST RELAYS) | ................................................................................ |49-11 |APU | ................................................................................ |49-15 |APU INLET DOOR ACTUATOR FAIL (49005) | ................................................................................ |52-31 |NOSE CARGO DOOR (FREIGHTER ONLY) | ................................................................................ |52-32 |SIDE CARGO DOOR | ................................................................................ |52-34 |AFT and FWD CARGO DOOR | ................................................................................ |52-71 |ENTRY DOORS | ................................................................................ |71-00 |POWER PLANT (ENGINES, REVERSERS, AUTOSTART, AVM) | 2.....................…........................................................1
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
45-10-00
ALL ú ú 04 Page 34 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
3) Table C shows the ATA chapter-sections (CH-SC) that you can put into the uplink request code for fault history summary (See Table B).
(d) ACARS reports look similar to printer reports except that the data is in a compressed format (Fig. 23-30).
B. Control
(1)
Show the CMC MENU on the CDU:
(a)
Push the MENU key on the CDU to show the MENU (Fig. 6).
(b)
Push the line select key (LSK) that is adjacent to <CMC to show the CMC MENU (Fig. 7).
(c)
If <RETURN shows after you push LSK, push the LSK that is adjacent to <RETURN until you see the CMC MENU.
(2)
Use the present leg faults function (Fig. 10):
(a)
Push the LSK that is adjacent to <PRESENT LEG FAULTS to show the first page of a list of FDEs.
(b)
Push the NEXT PAGE key to see more FDEs.
(c)
Push the LSK that is adjacent to an FDE that has a < symbol adjacent to it to show the first PRESENT LEG MSG page for the FDE.
NOTE: If the FDE does not have a < symbol adjacent to it,
____ there is no CMCS fault message correlated to the FDE. Thus, there is no PRESENT LEG MSG page for that FDE.
(d) If the page indication shows that there is more than one page, push the NEXT PAGE key to see a different CMCS fault message that is correlated to the same FDE.
NOTE: Each time you push the NEXT PAGE key you will see a
____ different CMCS fault message. When you see the last CMCS fault message (the two numbers in the page indication are the same), push the NEXT PAGE key to see the first message again.
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 中央維護計算機系統(17)
