.................................................................. | - Transfer Gearbox | *[C] | .................................................................. | - Starter Drive Seal | *[B] | .................................................................. | - Constant Speed Drive Seal | *[B] | .................................................................. | - Hydraulic Pump Drive Seal | *[B] | .................................................................. | - Fuel Pump Drive Seal | 6 | .................................................................. | - N2 Rotor Rotation Pad Cover | 3 | | (Necessary after borescope inspection) | | 2..........................................….....................1
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
~................................................................ | Power Plant Test Reference Table | .................................................................. | Component Repaired or Replaced | Necessary Test | .................................................................. | ENGINE FUEL SYSTEM COMPONENTS | | .................................................................. | - Fuel Pump | 6 | .................................................................. | - Fuel Filter Cartridge | 3 | .................................................................. | - Servo Fuel Heater | 3 | .................................................................. | - Fuel Nozzle | 3 | .................................................................. | - Main Engine Control (MEC) | 6 | .................................................................. | - CIT Sensor | 3 | .................................................................. | - CBP Sensor/Filter | 3 | .................................................................. | - VBV Reset Solenoid | 3 | .................................................................. | - Idle Reset Solenoid | 4 | .................................................................. | - Power Management Control (PMC) | PLA transducer gain | | | adjustment | | | (AMM 73-21-00/501) | | | and 6 (part power | | | trim check) | .................................................................. | - T12 Temperature Sensor | No Test Required | .................................................................. | - T2 Temperature Sensor | 3 | .................................................................. | - Fuel Flow Transmitter | 3 | .................................................................. | - Fuel Filter Differential | 3 | | Pressure Switch | | 2..........................................….....................1
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71-00-00
ALL ú ú C01 Page 504 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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本文链接地址：737-300 400 500 AMM 飞机维护手册 动力装置 POWER PLANT 1(46)
