Adjustment/Test 501 [*]
[*] AIRPLANES WITH THE ETC
Inspection/Check 601 [*]
[*] AIRPLANES WITH THE ETC
GENERATOR - TACHOMETER 49-61-61
Removal/Installation 401 ALL
SENSOR - COMPRESSOR INLET 49-61-32
TEMPERATURE
Removal/Installation 401 [*]
[*] AIRPLANES WITH THE ETC
SWITCH - ELECTRONIC SPEED 49-61-22
Removal/Installation 401 ALL
SWITCH - LOW OIL PRESSURE 49-61-51
Removal/Installation 401 ALL
SWITCH - SEQUENCING OIL PRESSURE 49-61-41
Removal/Installation 401 ALL
UNIT - APU CONTROL 49-61-11
Removal/Installation 401 ALL
INDICATING 49-70-00
__________ EXHAUST GAS TEMPERATURE INDICATING 49-71-00 SYSTEM
Description and Operation 1 CONFIG 1 [*] General 1 Indicator - EGT 5 Probe - Thermocouple 1 Resistor - EGT 1 Resistor - Harness Balancing 1 Operation 5
[*] AIRPLANES WITHOUT THE ETC
49-CONTENTS
BEJ Page 10 Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
CHAPTER 49 - AIRBORNE AUXILIARY POWER
TABLE OF CONTENTS
_________________
Chapter Section Subject_______ Subject ____ Effectivity
_______ Page ___________
Description and Operation 1 CONFIG 2 [*]
General 1
Indicator - EGT 1
Probe - ETC Thermocouple 1
Resistor - EGT 1
Operation 1
[*] AIRPLANES WITH THE ETC
Adjustment/Test 501 ALL
General 501
Functional Test - EGT Resistor 505
Test - Insulation Resistance 501
(Airplanes with the ETC)
Test - Insulation Resistance 503
(Airplanes without the ETC)
INDICATOR - EXHAUST GAS 49-71-11
TEMPERATURE
Removal/Installation 401 ALL
PROBE - ETC THERMOCOUPLE 49-71-31
Removal/Installation 401 [*]
[*] AIRPLANES WITH THE ETC
Adjustment/Test 501 [*]
[*] AIRPLANES WITH THE ETC
PROBE - EXHAUST GAS TEMPERATURE 49-71-21
THERMOCOUPLE
Removal/Installation 401 [*]
[*] AIRPLANES WITHOUT THE ETC
Adjustment/Test 501 [*]
[*] AIRPLANES WITHOUT THE ETC
APU INDICATING SYSTEM 49-72-00
Description and Operation 1 ALL
General 1
Indicator - Elapsed Time 1
Light - OVER SPEED 1
APU ELAPSED TIME INDICATOR 49-72-11
Removal/Installation 401 ALL
EXHAUST 49-80-00
_______
49-CONTENTS
BEJ Page 11 Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES/MAINTENANCE MANUAL ////////////////////////
CHAPTER 49 - AIRBORNE AUXILIARY POWER
TABLE OF CONTENTS
_________________
Chapter Section
Subject_______ Subject ____ Effectivity_______ Page ___________
APU EXHAUST SYSTEM 49-81-00
Description and Operation 1 ALL General 1 Aft Fairing 1 Exhaust Duct 1 Operation 1
ASSEMBLY - AFT FAIRING 49-81-31
Removal/Installation 401 ALL General 401 Installation (With the APU 409
in Position) Installation (With the APU 411 Removed) Removal (With the APU in 401 Position) Removal (With the APU 407 Removed)
MUFFLER - EXHAUST DUCT 49-81-11 Removal/Installation 401 ALL Inspection/Check 601 ALL Cleaning/Painting 701 ALL
SHIELD - EXHAUST DUCT HEAT 49-81-21 Removal/Installation 401 ALL
OIL 49-90-00
___ APU LUBRICATION SYSTEM 49-91-00 Description and Operation 1 ALL General 1 Cooler - Oil 1 Pump - Oil 1 Tank - Oil 3 Operation 3 COOLER - OIL 49-91-41 Removal/Installation 401 ALL Inspection/Check 601 ALL FILTER - OIL PUMP 49-91-12 Removal/Installation 401 ALL LINE - OIL TANK VENT 49-91-61 Inspection/Check 601 ALL PUMP - OIL 49-91-11 Removal/Installation 401 ALL Adjustment/Test 501 ALL Inspection/Check 601 ALL
49-CONTENTS
BEJ Page 12 Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
CHAPTER 49 - AIRBORNE AUXILIARY POWER
TABLE OF CONTENTS
_________________
Chapter Section Subject_______ Subject ____ Effectivity
_______ Page ___________
SEAL - OIL PUMP DRIVE SHAFT 49-91-51 Removal/Installation 401 ALL TANK - OIL 49-91-31
Servicing 301 ALL General 301 Drain the Oil Tank 301 Fill the Oil Tank 304
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