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 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 71-00-00
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
~................................................................ | Power Plant Test Reference Table | .................................................................. | Component Repaired or Replaced | Necessary Test | .................................................................. | BASIC ENGINE COMPONENTS | | .................................................................. | - Fan Rotor Blades | 7 | .................................................................. | - N1 Speed Sensor | *[C] | .................................................................. | - N2 Control Alternator | *[C] | ..................................................................
 | - EGT Thermocouple Harness and Probe  | System check  |
 |  | (AMM 77-21-00/501)  |
 |  | and 3  |

 .................................................................. | - 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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 71-00-00
 ALL  ú ú C01 Page 503 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
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
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 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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