................................................................................ |ATA Chapter-Sections | ATA TEXT | ................................................................................ |24-23 |SYSTEM PROTECTION: DIFF FAULT, OF/UF, OE/UE, DIFF | | |CURRENT, OPEN PHASE | ................................................................................ |24-27 |BCU/GCU/CMC/EIU DATA BUS COMMUNICATIONS | ................................................................................ |24-29 |MAIN STANDBY TRANSFER RELAY/WIRING FAIL (24723) | ................................................................................ |24-31 |UTILITY and GALLEY ELCU | ................................................................................ |24-32 |DCIR-1 and MAIN TRU | ................................................................................ |24-33 |MAIN, APU STATIC INVERTER and DC CURRENT SENSOR | ................................................................................ |24-34 |BATTERY CHARGER, DC CURRENT SENSOR, DC ISOLATION RELAY | ................................................................................ |24-41 |EXT POWER PROTECTION, BCU GST/BITE MONITOR, BCU POWER | | |INPUTS, GCU FREQ REF | ................................................................................ |24-51 |GROUND HANDLING RELAYS, CAPTAINS and FIRST OFFICERS | | |TRANSFER RELAYS | ................................................................................ |24-60 |REMOTE CONTROL CIRCUIT BREAKERS | ................................................................................ |26-11 |ENGINE FIRE LOOPS, NAC OVERHET LOOPS, TURB OVHT LOOPS, | | |NAC TAMP DETECTOR | ................................................................................ |26-12 |ENGINE STRUT OVERHEAT LOOPS | ................................................................................ |26-15 |APU FIRE LOOP A and B | ................................................................................ |26-16 |CARGO LOOPS, CARGO SMOKE DETECTION EJECTORS | ................................................................................ |26-17 |WHEEL WELL (GROUND TEST ONLY) | ................................................................................ |26-18 |BLEED DUCT LEAK LOOPS | ................................................................................ |26-21 |ENGINE BOTTLES LOW PRESSURE | ................................................................................ |26-22 |APU BOTTLE LOW PRESSURE (26043) | ................................................................................ |26-23 |CARGO BOTTLES LOW PRESSURE | ................................................................................ |27-09 |FLIGHT CONTROLS POWER SUPPLY MODULE (PSM), CONTROL SPD |
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
45-10-00
ALL ú ú 02 Page 30 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 | ................................................................................ |27-11 |AILERON LOCKOUT | ................................................................................ |27-18 |FORWARD SPD | ................................................................................ |27-21 |UPPER and LOWER RUDDER RATIO CHANGER | ................................................................................ |27-28 |UPPER and LOWER RUDDER SYNCHRO (AFT SPD) | ................................................................................ |27-30 |ELEVATOR FEEL COMPUTER FAIL (27401) | ................................................................................ |27-32 |LEFT and RIGHT STALL WARNING | ................................................................................ |27-38 |AFT SPD | ................................................................................ |27-41 |SRM'S | ................................................................................ |27-51 |FLAP CONTROL | ................................................................................ |27-58 |FCU INTERFACE | ................................................................................ |27-62 |AUTO SPEEDBRAKE SYSTEM FAIL (27965) | ................................................................................ |27-68 |#4 and #12 SPOILER SYNCHRO FAIL, FWD SPD PROGRAM | | |PIN/PARITY | ................................................................................ |27-81 |GROUP B PNEUMATIC DISABLE RELAY FAULT (27873) | ................................................................................ |27-88 |LE LX and RX (X = 1-4) | ................................................................................ |28-15 |SCAVENGE PUMP FAIL (28620) | ................................................................................ |28-16 |RESERVE TANK TRANSFER VALVES, MAIN TANK 1 and 4 JETT | | |GRAVITY TRANSFER VLV | ................................................................................ |28-21 |HORZ STAB PUMPS AND VLV, CENTER WING REFUEL and | | |ISOLATION VLV | ................................................................................ |28-22 |FSMC'S, ENGINE FUEL, SHUTOFF VALVES (SPAR), CROSSFEED | | |VALVES, BOOST PUMPS, BALLAST | ................................................................................ |28-25 |APU PUMPS AND VALVES | ................................................................................ |28-31 |FJCC'S, JETTISON TRANSFER VALVES, OVERRIDE/JETT PUMPS | 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：747-400 AMM 飞机维护手册 中央维护计算机系统(15)
