(a)  
Output flow capacity - 120-130 PPM (55-60 KGPM)

 (b)  
Temperature - 300-325°F (150-165°C)

 (c)  
Supply pressure - 30-45 psi (210-310 kPa)

 (4)  
Hoses (2 necessary) and related clamps -approved for temperatures of 325°F (165°C) and
 air pressures of 45 psi (310 kPa):
 one hose must be approved to connect to the hot
 air source outlet and air filter inlet,
 the other hose must be approved to connect to
 the air filter outlet and engine exhaust plug
 exit (dry-out procedure) or relubrication
 manifold (relubrication procedure) - locally
 available

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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(5)  
Gloves, Heavy Protective - Local purchase

 (6)  
Mat (2 necessary)
 Rubber Manufacturer's Association - Grade SC43,
 neoprene sponge, 1 inch thick, approximately
 3x4 feet with warning streamers attached

 C.
Consumable Materials

 (1)  
Oil - Engine (AMM 70-10-01/201)

 (2)  
Oil - Preservative
 (containing a corrosion inhibitor),
 MIL-L-6085, CP2259 (AMM 70-10-01/201)

 (3)  
Oil, Additive - Anti-Corrosion,
 CP2309 (AMM 70-10-01/201)

 D.
References

 (1)  
AMM 72-00-00/201, Engine

 (2)  
AMM 79-21-05/201, Magnetic Chip Detectors

 E.
Access

 (1)  
Location Zones
 506 Engine No. 1
 606 Engine No. 2

 F.
Prepare for the Dry-Out and Lubrication Procedure (Fig. 202)

 S 842-128-C00
 CAUTION: IF THE ENGINE WILL NOT BE OPERATED FOR 24 HOURS AFTER A LANDING
_______ AND THE ENGINE HAD AN IN-FLIGHT SHUTDOWN, THE ENGINE DRY-OUT PROCEDURE MUST BE DONE AS QUICKLY AS POSSIBLE. IF THE ENGINE DRY-OUT PROCEDURE IS NOT DONE IMMEDIATELY AFTER LANDING, CORROSION DAMAGE DUE TO CONDENSATION ON THE COMPONENTS WET WITH OIL (BEARINGS, GEARS, ETC.) CAN OCCUR.
 (1)  Do the dry-out procedure as quickly as possible.
 S 862-089-C00
 WARNING:_______DO THE DRY-OUT PROCEDURE IN AN AREA WITH A GOOD AIRFLOW. KEEP CLEAR OF THE ENGINE EXHAUST AREA. IF YOU BREATHE THE OIL MIST FROM THE ENGINE EXHAUST. IF YOU DO NOT OBEY THESE PRECAUTIONS, INJURY TO PERSONS CAN OCCUR.
 (2)  If the engine is on-wing, make sure the applicable start lever is in the CUTOFF position and install a DO-NOT-OPERATE tag.
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 ú ú  ú C01.101 ú BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.  Page 230Jul 12/02 

////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE B
SEE A
ACCESSORY FWD
GEARBOX TGB/AGB CHIP DETECTOR FORWARD SUMP LUBRICATION
AFT SUMP
CHIP DETECTOR  UNIT
CHIP DETECTOR
A
Engine Sumps Relubrication Manifold Tool Set InstallationFigure 202 (Sheet 1)
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 ALL  ú ú C02 Page 231 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
FORWARD
LUBRICATION
SUMP
UNIT

LINE
Engine Sumps Relubrication Manifold Tool Set Installation
Figure 202 (Sheet 2)
　
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