EffectivityALL
ALL
ALL
ALLALL
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30-CONTENTS
BEJ Page 3 Mar 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL CHAPTER 30 - ICE AND RAIN PROTECTION TABLE OF CONTENTS
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Subject
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Trouble Shooting Adjustment/Test DRIVE ASSEMBLY - WINDSHIELD
WIPER Removal/Installation
WINDSHIELD WIPER ASSEMBLY Removal/Installation Adjustment/Test
RAIN REPELLENT SYSTEM
Description and Operation General Container and Receptacle Module - Time Delay Solenoid and Spray Nozzles Visual Reservoir and Plumbing Operation
Trouble Shooting Maintenance Practices Clean Dried Rain Repellent Fluid from Windshield Depressurization - Rain Repellent System Flush the Rain Repellent System Replacement - Rain Repellent Container Maintenance Practices
Chapter SectionSubject_______ Page
101 501
30-42-21
401
30-42-11401 501
30-43-001 134446101 201 203
203
204
201
201
Effectivity
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ALLCONFIG 1 ALL
CONFIG 2 [*]
[*] AIRPLANES WITH HYDROPHOBIC COATING ON THE NUMBER 1 WINDOWS
Adjustment/Test 501 ALL
NOZZLE - RAIN REPELLENT SPRAY 30-43-11
Removal/Installation 401 ALL
Cleaning/Painting 701 ALL
VALVE - RAIN REPELLENT SOLENOID 30-43-21
Removal/Installation 401 ALL
WATER LINES___________ 30-70-00
WATER AND TOILET DRAIN ANTI-ICING 30-71-00
SYSTEM
Description and Operation 1 ALL
General 1
Heaters - Toilet Drain 1
Trouble Shooting 101 ALL
30-CONTENTS
BEJ Page 4 Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL CHAPTER 30 - ICE AND RAIN PROTECTION TABLE OF CONTENTS
_________________
Chapter
Section
Subject_______ Subject_______ Page____ Effectivity___________
Adjustment/Test 501 ALL
RIBBON HEATER 30-71-11
Removal/Installation 401 ALL
30-CONTENTS
BEJ Page 5 Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
1.
2.
3.
4.
A
737-300/400/500MAINTENANCE MANUAL
ICE AND RAIN PROTECTION - DESCRIPTION AND OPERATION
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General
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A. The following systems (Fig. 1) are used to protect the airplane and aid the pilots when operating under ice and rain conditions:
(1)
Thermal anti-icing (TAI) systems using engine bleed air are provided for the wing, engine, and engine cowls.
(2)
Electrical anti-icing systems are provided for the control cabin windows, pitot and temperature probe sensors, and the alpha vanes.
(a) There is also anti-icing provided for the toilet drains.
(3)
Rain removal is provided for the No. 1 control cabin windows by a windshield wiper system. A rain repellent system is also provided to be used in conjunction with the wiper system.
Thermal Anti-Icing (TAI) Systems
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A. The wing thermal anti-icing (TAI) system de-ices the leading edge slats. The air for the TAI system is supplied from engine bleed air (Ref Chapter 36, Engine Bleed Air Distribution System).
B. The engine thermal anti-ice (TAI) system de-ices the engine nose dome and
engine inlet cowl.Electrical Anti-Icing Systems
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A. The control cabin window anti-icing system de-ices and provides birdproofing of the No. 1, 2, 4, and 5 control cabin windows on each side of the control cabin. The windows are heated by the use of a transparent electrical resistance coating incorporated as an integral part of the windows.
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