747-400 AMM 飞机维护手册 中央维护计算机系统(36)

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 |  <OVBD VALVE SYSTEM  |  AMM 21-31-00/501 |
 |  <FWD CARGO OVBD  |  AMM 21-26-00/501 |
 |  <LOWER CARGO VENT  |  AMM 21-26-00/501 |
 |  <SHUTOFF/DUMP VLV  |  AMM 21-23-03/401 |
 |  <CARGO HEAT SYSTEM  |  AMM 21-44-00/501 |
 |  <PTC-A/PACK-1  |  AMM 21-51-00/501 |
 |  <PTC-A/PACK-2  |  AMM 21-51-00/501 |
 |  <PTC-A/PACK-3  |  AMM 21-51-00/501 |
 |  <PTC-A/ALL PACKS  |  AMM 21-51-00/501 |
 |  <PTC-B/PACK-1  |  AMM 21-51-00/501 |
 |  <PTC-B/PACK-2  |  AMM 21-51-00/501 |
 |  <PTC-B/PACK-3  |  AMM 21-51-00/501 |
 |  <PTC-B/ALL PACKS  |  AMM 21-51-00/501 |
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 2.............................…...................1
 Table I - Ground Tests

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 45-10-00
 ALL  ú ú 25 Page 220 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE/CMCS BITE MANUAL
 ~................................................. | GROUND TESTS MENU PROMPT | AMM REFERENCE | ................................................... | <TRIM AIR SYSTEM | AMM 21-61-00/501| | | | | <21 CABIN PRESSURE| | | <CPCS-A | AMM 21-31-00/501| | <CPCS-B | AMM 21-31-00/501| | | | | <21 EQUIPMENT COOLING| | | <EQUIPMENT COOLING | AMM 21-58-00/501| | | | | <22 AUTOPILOT FLT DIR| | | <FCC-L | AMM 22-10-00/501| | <FCC-C | AMM 22-10-00/501| | <FCC-R | AMM 22-10-00/501| | <MODE CONTL PANEL | AMM 22-10-00/501| | <SERVO-AILERON | AMM 22-10-00/501| | <SERVO-ELEVATOR | AMM 22-10-00/501| | <SERVO-RUDDER | AMM 22-10-00/501| | <A/P DISC SWITCH | AMM 22-10-00/501| | <GO AROUND SWITCH | AMM 22-10-00/501| | <AUTOLAND UNIQUE | AMM 22-10-00/501| | <AIR/GROUND RELAY | AMM 22-10-00/501| | <FCC CONFIGURATION | AMM 22-10-00/501| | <FCC INSTRUMENTS | AMM 22-10-00/501| | <SPEED BRK XDUCER | AMM 22-10-00/501| | <FLAP XDUCER | AMM 22-10-00/501| | <STAB TRIM | AMM 22-10-00/501| | <XDUCER OUTPUTS | AMM 22-10-00/501| | <AIL SURFACE LIMIT | AMM 22-10-00/501| | <ELV SURFACE LIMIT | AMM 22-10-00/501| | <RUD SURFACE LIMIT | AMM 22-10-00/501| | | | | <22 YAW DAMPER| | | <UPPER YDM TEST | AMM 22-21-00/501| | <LOWER YDM TEST | AMM 22-21-00/501| | <UPR YDM ACTUATOR | AMM 22-21-00/501| | <LWR YDM ACTUATOR | AMM 22-21-00/501| | | | | <23 COMMUNICATIONS| | | | | | | | | | | | | | | | | | | | | | | 2.............................…...................1
 Table I - Ground Tests
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 45-10-00
 ALL  ú ú 16 Page 221 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE/CMCS BITE MANUAL
 ~................................................. | GROUND TESTS MENU PROMPT | AMM REFERENCE | ................................................... | <HF-L | AMM 23-11-00/501| | <HF-R | AMM 23-11-00/501| | <VHF-L | AMM 23-12-00/501| | <VHF-R | AMM 23-12-00/501| | <VHF-C | AMM 23-12-00/501| | <SATCOM | AMM 23-25-00/501| | | | | <24 ELECTRICAL POWER| | | <EPGS (BCU1) | AMM 24-23-01/501| | <EPGS (BCU2) | AMM 24-23-01/501| | | | | <26 FIRE PROTECTION| | | <FIRE SYSTEM TEST | AMM 26-11-00/501| | | | | <27 AILERON LOCKOUT| | | <AIL LO ACTUATORS | AMM 27-11-00/501| | | | | <27 RUDDER RATIO| | | <RUD RATIO ACTR | AMM 27-21-00/501| | <RUD RATIO EXTEND| | | | | | <27 FLAP CONTROL| | | <FLAP CONTROL-L | AMM 27-51-00/501| | <FLAP CONTROL-C | AMM 27-51-00/501| | <FLAP CONTROL-R | AMM 27-51-00/501| | | | | <27 STALL WARNING| | | <STALL LEFT | AMM 27-32-00/501| | <STALL RIGHT | AMM 27-32-00/501| | | | | <28 FUEL| | | <RESERVE VALVE | AMM 28-16-01/501| | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | 2.............................…...................1
　
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