................................................................................ |ATA Chapter-Sections | ATA TEXT | ................................................................................ |28-41 |FUEL QUANTITY INDICATING SYSTEM (FQIS) | ................................................................................ |28-42 |FSMC CENTER WING PUMPS LOW PRESSURE DUAL INPUTS | | |DISAGREE | ................................................................................ |28-43 |FSEIC | ................................................................................ |28-44 |SINGLE POINT SENSORS (GROUND TEST RESULTS ONLY) | ................................................................................ |29-11 |HYDIM 1-4 | ................................................................................ |29-21 |HYD AUXILIARY PUMPS | ................................................................................ |29-31 |HYD-X SYSTEM PRESSURE TRANSMITTER FAIL (X = 1-4) | ................................................................................ |29-32 |HYD-X TEMPERATURE TRANSMITTER 1 FAIL (X = 1-4) | ................................................................................ |29-33 |HYQUIM | ................................................................................ |29-34 |HYD-X DEMAND and ENGINE PUMP INDICATING CIRCUITS | | |(X = 1-4) | ................................................................................ |30-11 |WING ANTI-ICE | ................................................................................ |30-21 |ENGINE COWL OVERHEAT and THERMAL ANTI-ICE VALVE DISAGREE| ................................................................................ |30-31 |PROBE HEAT | ................................................................................ |30-32 |AOA HEAT (GROUND TEST ONLY) | ................................................................................ |30-41 |WINDOW HEAT | ................................................................................ |30-71 |DRAIN MAST HEATERS | ................................................................................ |30-81 |ICE DETECTOR(S) | ................................................................................ |31-25 |CAPTAINS CLOCK | ................................................................................ |31-31 |FLIGHT RECORDER and DFDAC | ................................................................................ |31-35 |ACMS DMU | ................................................................................ |31-41 |WEIGHT BALANCE |
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
45-10-00
ALL ú ú 03 Page 32 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
~..............................................................................
| CH-SC |
| Table C - ATA Chapter-Sections |
| for Fault History Summary Report by ACARS Uplink Request |
................................................................................ |ATA Chapter-Sections | ATA TEXT | ................................................................................ |31-51 |MAWEA CARDS | ................................................................................ |31-61 |INTEGRATED DISPLAY SYSTEM (IDS) | ................................................................................ |32-42 |BRAKES (BSCU and ANTISKID) | ................................................................................ |32-44 |PARKING BRAKE VALVE/HANDLE DISAGREE (32893) | ................................................................................ |32-45 |TIRE PRESSURE (OPTION) | ................................................................................ |32-46 |BRAKE TEMPERATURE | ................................................................................ |32-53 |BODY GEAR STEERING | ................................................................................ |32-61 |PSEU | ................................................................................ |34-12 |AIR DATA SYSTEM | ................................................................................ |34-21 |INERTIAL REFERENCE SYSTEM | ................................................................................ |34-31 |ILS/MMR/MMR-GNSS | ................................................................................ |34-33 |RADIO ALTIMETERS | ................................................................................ |34-34 |MLS (FUTURE OPTION) | ................................................................................ |34-35 |PARA-VISUAL DISPLAY (PVD) | ................................................................................ |34-43 |WEATHER RADAR (WXR) | ................................................................................ |34-45 |TCAS | ................................................................................ |34-46 |GROUND PROXIMITY WARNING COMPUTER (GPWC) | ................................................................................ |34-51 |VOR-L/MARKER BEACON, VOR-R | ................................................................................ |34-53 |ATC | ................................................................................ |34-55 |DME | ................................................................................ |34-57 |ADF | ................................................................................ |34-58 |GPSSU (STANDALONE GPS SENSOR UNIT) | 中國(guó)航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊(cè) 中央維護(hù)計(jì)算機(jī)系統(tǒng)(16)
