33.
OVERSPEED LIGHT

34.
DC VOLTMETER

35.
OIL TEMPERATURE INDICATOR (INOP)

36.
TACHOMETER GENERATOR

37.
ELECTRICAL PLUG FOR THE TACHOMETER GENERATOR

38.
OIL PRESSURE HOSE

39.
TEST PORT FOR THE OIL PRESSURE

40.
CONTROL-AIR PRESSURE HOSE

41.
CONTROL-AIR PRESSURE TEST PORT

42.
HI-FUEL PRESSURE HOSE

43.
HI-FUEL PRESSURE TEST PORT

44.
ELECTRONIC SPEED SWITCH

45.
ELECTRICAL PLUG FOR THE ELECTRONIC

SPEED SWITCH 46.ELECTRICAL CABLE ASSEMBLY P/N 834367-1

46.
TEST CABLE ASSEMBLY P/N 294110-1 AND ADAPTER CABLE ASSEMBLY P/N 2024498-1 (THIS IS AN ALTERNATIVE TO THE ELECTRICAL CABLE ASSEMBLY.)

47.
APU ELECTRICAL PLUG

Gas Turbine Engine Tester and Connections
Figure 503 (Sheet 4)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH THE ETC ú

 49-11-00
 ú ú 02 Page 514 ú Jul 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
(2)  Access Panels
 1201 Electronic Equipment Access Door
 3804 APU Cowl Door

 F. Procedure
 S 865-011
 (1)  Set the switch and the circuit breaker:
 (a)  
Set the APU master switch on the P5 forward overhead panel to the OFF position and attach a DO-NOT-CLOSE tag.

 (b)  
Open this circuit breaker and attach a DO-NOT-CLOSE tag: 1) E3-3 Electrical Shelf, APU Control Unit

 S 015-012
 (2)  Open the APU cowl door:
 (a)  
Open the latches for the APU cowl door.

 (b)  
Open the APU cowl door.

 (c)  
Connect the door support rods.

 S 015-013
 CAUTION:_______BE CAREFUL WHEN YOU MOVE THE LOWER SHROUD. DAMAGE TO THE SHROUD DRAIN LINES CAN OCCUR.
 (3)  Remove the lower shroud:
 (a)  
Hold the lower shroud and open the shroud latches.

 (b)  
Remove the lower shroud.

 S 485-014
 (4)  Install the turbine engine tester on the engine:
 (a)  
Disconnect the electrical connector D1252 on the APU harness (47) from the receptacle D452 in the upper shroud.

 (b)  
Connect the electrical cable or test cable assembly (46) to the electrical connector D1252 and the receptacle D452.

 NOTE: The connectors on the electrical cable or test cable
____ assembly are identified by aluminum markers.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 49-11-00
 ALL  ú ú 12 Page 515 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES/MAINTENANCE MANUAL ////////////////////////
(c)  AIRPLANES WITHOUT THE ETC;
 Disconnect the leads of the thermocouple harness from the
 terminals of the EGT thermocouple probe.
 (d)  AIRPLANES WITH THE ETC;
 Disconnect the leads of the thermocouple harness from the studs
 of the ETC thermocouple probe.
 (e)  AIRPLANES WITHOUT THE ETC;
 Connect the leads of the electrical cable or adapter cable
 assembly (46) to the terminals of the EGT thermocouple probe.
 NOTE: If the adapter cable assembly is used, the test cable____
 assembly must be connected to the adapter cable
 assembly.
 (f)  AIRPLANES WITH THE ETC;
 Connect the leads of the electrical cable or adapter cable
 assembly (46) to the studs of the ETC thermocouple probe.
 NOTE: If the adapter cable assembly is used, the test cable____
 assembly must be connected to the adapter cable
 assembly.
 (g)  Connect the electrical cable or test cable assembly (46) to
 the electronic speed switch (44) and the electrical
 connectors (45).
 (h)  When you use the tester for the first time, do a check of the
 EGT loop resistance as follows:
 1) Remove the screws that attach the instrument panel to the
 temperature indication circuit.
　
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