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CHAPTER 56 Windows Subject/Page Date COC EFFECTIVE PAGES 1 thru 2 Oct 10/2006 56-CONTENTS 1 Jun 10/2006 2 BLANK 56-00-00 1 Oct 10/2002 2 Oct 10/2002 3 Jun 10/2006 R 4 Oct 10/2006 5 Jun 10/2006 6 Jun 10/2006 56-10-00 1 Oct 10/2002 R 2 Oct 10/2006 3 Jun 10/2006 R 4 Oct 10/2006 56-11-00 1 Oct 10/2002 2 Oct 10/2002 3 Feb 10/2003 4 Oct 10/2005 R 5 Oct 10/2006 Subject/Page Date COC 56-11-00 (cont.) 6 Oct 10/2005 7 Oct 10/2005 8 Jun 10/2006 9 Jun 10/2006 10 BLANK 56-12-00 1 Oct 10/2002 2 Oct 10/2002 3 Feb 10/2003 4 BLANK 56-21-00 R 1 Oct 10/2006 O 2 Oct 10/2006 3 Jun 10/2006 R 4 Oct 10/2006 56-22-00 R 1 Oct 10/2006 2 Jun 10/2006 3 Jun 10/2006 R 4 Oct 10/2006 56-31-00 1 Oct 10/2002 2 Oct 10/2002 A=Added, R=Revised, D=Deleted, O=Overflow, C=Customer Originated Change 56-EFFECTIVE PAGES Page 1 D633A101-GUN Oct 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL CHAPTER 56 Windows Subject/Page Date COC 56-31-00 (cont.) R 3 Oct 10/2006 4 Oct 10/2005 Subject/Page Date COC A=Added, R=Revised, D=Deleted, O=Overflow, C=Customer Originated Change 56-EFFECTIVE PAGES Page 2 D633A101-GUN Oct 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL CHAPTER 56 Windows CH-SC-SU Subject Page Effectivity 56-00-00 WINDOWS - INTRODUCTION 2 GUN ALL 56-10-00 WINDOWS - FLIGHT COMPARTMENT - INTRODUCTION 2 GUN ALL 56-11-00 WINDOWS - CONTROL CABIN FIXED WINDOWS - NO.1 WINDOW 2 GUN ALL 56-11-00 WINDOWS - CONTROL CABIN FIXED WINDOWS - NO. 3 WINDOW 4 GUN ALL 56-11-00 WINDOWS - CONTROL CABIN FIXED WINDOWS - NO. 4 and 5 WINDOWS 8 GUN 001-012, 101-108, 201-999 PRE SB 737-56-1017 56-12-00 WINDOWS - CONTROL CABIN SLIDING WINDOWS - NO. 2 OPENABLE WINDOW 1 GUN ALL 56-21-00 WINDOWS - PASSENGER CABIN WINDOWS - GENERAL DESCRIPTION 1 GUN ALL 56-22-00 WINDOWS - EMERGENCY EXIT WINDOW - GENERAL DESCRIPTION 1 GUN ALL 56-31-00 WINDOWS - DOOR-MOUNTED WINDOWS - GENERAL DESCRIPTION 2 GUN ALL 56-CONTENTS Page 1 D633A101-GUN Jun 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL CHAPTER 56 Windows THIS PAGE IS INTENTIONALLY LEFT BLANK 56-00-00 Page 1 D633A101-GUN Oct 10/2002 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL General These are the types of windows on the airplane: * Flight compartment windows (fixed and sliding) * Passenger compartment windows * Emergency exit windows * Door-mounted windows. All the windows can hold cabin pressurization loads and have fail safe properties. WINDOWS - INTRODUCTION EFFECTIVITY GUN ALL 56-00-00 Page 2 D633A101-GUN Oct 10/2002 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-00-00-001 WINDOWS - INTRODUCTION WINDOWS - INTRODUCTION EFFECTIVITY GUN 101-108 PRE SB 737-56-1017 56-00-00 Page 3 D633A101-GUN Jun 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-00-00-001 WINDOWS - INTRODUCTION WINDOWS - INTRODUCTION EFFECTIVITY GUN 109-118; GUN 101-108 POST SB 737-56-1017 56-00-00 Page 4 D633A101-GUN Oct 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-00-00-001 WINDOWS - INTRODUCTION WINDOWS - INTRODUCTION EFFECTIVITY GUN 001-012, 201-999 PRE SB 737-56-1017 56-00-00 Page 5 D633A101-GUN Jun 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-00-00-001 WINDOWS - INTRODUCTION WINDOWS - INTRODUCTION EFFECTIVITY GUN 013-099; GUN 001-012, 201-999 POST SB 737-56-1017 56-00-00 Page 6 D633A101-GUN Jun 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-00-00-001 THIS PAGE IS INTENTIONALLY LEFT BLANK WINDOWS - INTRODUCTION 56-10-00 Page 1 D633A101-GUN Oct 10/2002 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL GUN 001-012, 101-108, 201-999 PRE SB 737-56-1017 General Description There are ten windows in the flight compartment. There are five left (L) windows and five right (R) windows. Flight compartment windows No. 1, 3, 4, and 5 are fixed and do not open. Window No. 2 is a sliding window that opens. GUN 013-099, 109-118; GUN 001-012, 101-108, 201-999 POST SB 737-56-1017 General Description There are six windows in the flight compartment. There are three left (L) windows and three right (R) windows. Flight compartment windows No. 1, and 3 are fixed and do not open. Window No. 2 is a sliding window that opens. GUN ALL Interface Some flight compartment windows get heat from the window anti-ice system. See the ice and rain protection chapter for more information about the window anti-ice system. (CHAPTER 30) WINDOWS - FLIGHT COMPARTMENT - INTRODUCTION EFFECTIVITY GUN ALL 56-10-00 Page 2 D633A101-GUN Oct 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-10-00-001 WINDOWS - FLIGHT COMPARTMENT - INTRODUCTION WINDOWS - FLIGHT COMPARTMENT - INTRODUCTION EFFECTIVITY GUN 001-012, 101-108, 201-999 PRE SB 737-56-1017 56-10-00 Page 3 D633A101-GUN Jun 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-10-00-001 WINDOWS - FLIGHT COMPARTMENT - INTRODUCTION WINDOWS - FLIGHT COMPARTMENT - INTRODUCTION EFFECTIVITY GUN 013-099, 109-118; GUN 001-012, 101-108, 201-999 POST SB 737-56- 1017 56-10-00 Page 4 D633A101-GUN Oct 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-10-00-001 THIS PAGE IS INTENTIONALLY LEFT BLANK WINDOWS - FLIGHT COMPARTMENT - INTRODUCTION 56-11-00 Page 1 D633A101-GUN Oct 10/2002 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL General Window No. 1 has laminated glass on each side of a plastic core. They are resistant to bird impact with or without window heat. The inner glass pane is thicker than the outer glass pane. It is the primary structural part. It holds the internal airplane pressure load. The vinyl layer is a secondary structure. It is also a fail safe device that prevents the shatter of a broken window if the inner pane breaks. The outer pane is not structural. The outer pane gives a rigid, hard, scratch resistant surface. A hydrophobic windshield coating is applied to the outer pane to improve pilot visibility during rain conditions. A conductive film on the inner face of the outer glass pane permits electrical heating for window anti-icing and defogging. Bus bars molded into the upper and lower edges of the windows make electrical contact with the conductive film and connect to electrical terminals. WARNING: BE CAREFUL WHEN YOU DO WORK ON THE WINDOW NO. 1. THE OUTPUT VOLTAGE OF THE AUTOTRANSFORMER IS 250-350 VOLTS. THIS CAN CAUSE INJURY TO PERSONS. WINDOWS - CONTROL CABIN FIXED WINDOWS - NO.1 WINDOW EFFECTIVITY GUN ALL 56-11-00 Page 2 D633A101-GUN Oct 10/2002 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-11-00-001 WINDOWS - CONTROL CABIN FIXED WINDOWS - NO.1 WINDOW WINDOWS - CONTROL CABIN FIXED WINDOWS - NO.1 WINDOW EFFECTIVITY GUN ALL 56-11-00 Page 3 D633A101-GUN Feb 10/2003 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-11-00-001 General Window No. 3 has two stretched acrylic panes. A phenolic spacer gives separation between the panes. The spacer attaches to the panes by low-tack pressure sensitive tape which also operates as an air seal. The phenolic spacer gives an insulation cavity which prevents fog on the inner surface of the windows. There is a small hole in the upper forward corner of the inner pane. This hole must be open at all times. It permits pressure in the air space to be equal to the pressure in the cabin. GUN 201-999 WARNING: BE CAREFUL WHEN YOU DO WORK ON THE WINDOW NO. 3. THE OUTPUT VOLTAGE OF THE AUTOTRANSFORMER IS 250-350 VOLTS. THIS CAN CAUSE INJURY TO PERSONS. The window has a thermal switch bracket that you must align with the thermal switch location on the glass. GUN ALL WINDOWS - CONTROL CABIN FIXED WINDOWS - NO. 3 WINDOW EFFECTIVITY GUN ALL 56-11-00 Page 4 D633A101-GUN Oct 10/2005 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-11-00-005 WINDOWS - CONTROL CABIN FIXED WINDOWS - NO. 3 WINDOW WINDOWS - CONTROL CABIN FIXED WINDOWS - NO. 3 WINDOW EFFECTIVITY GUN 001-099, 101-118 56-11-00 Page 5 D633A101-GUN Oct 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-11-00-005 WINDOWS - CONTROL CABIN FIXED WINDOWS - NO. 3 WINDOW WINDOWS - CONTROL CABIN FIXED WINDOWS - NO. 3 WINDOW EFFECTIVITY GUN 201-999 56-11-00 Page 6 D633A101-GUN Oct 10/2005 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-11-00-005 THIS PAGE IS INTENTIONALLY LEFT BLANK WINDOWS - CONTROL CABIN FIXED WINDOWS - NO. 3 WINDOW 56-11-00 Page 7 D633A101-GUN Oct 10/2005 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL General Windows No. 4 and 5 are almost the same. Windows No. 4 and 5 have laminated glass on each side of a polyvinyl butyral (vinyl) core. Window No. 4 has one more vinyl layer to prevent the shatter of broken glass if there is a bird strike. The inner vinyl layer is not structural. A conductive strip on the outer face of the inner glass pane permits electrical heating for window anti-ice and window fog conditions. WINDOWS - CONTROL CABIN FIXED WINDOWS - NO. 4 and 5 WINDOWS EFFECTIVITY GUN 001-012, 101-108, 201-999 PRE SB 737-56-1017 56-11-00 Page 8 D633A101-GUN Jun 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-11-00-010 WINDOWS - CONTROL CABIN FIXED WINDOWS - NO. 4 and 5 WINDOWS WINDOWS - CONTROL CABIN FIXED WINDOWS - NO. 4 and 5 WINDOWS EFFECTIVITY GUN 001-012, 101-108, 201-999 PRE SB 737-56-1017 56-11-00 Page 9 D633A101-GUN Jun 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-11-00-010 Purpose The No. 2 window is on tracks so that it may be rolled back to permit ventilation and communication during ground handling operations. You can operate the right window from outside of the airplane as an emergency exit. Physical Description The No. 2 openable window has these parts: * Handle with trigger * Bellcranks * Pushrods * Clothes guard protector * Link * Springs * Window open latch plate * Upper roller * Upper track * Lower roller * Lower track * Latch mechanism rod * External access door * External release handle. Window No. 2 has laminated glass on each side of a polyvinyl butyral (vinyl) core. The window is resistant to bird impact with or without window heat. The inner glass pane is thicker than the outer pane. It is the primary structure. It holds the internal airplane pressure load. The vinyl layer is the secondary structure. It is also a fail-safe device that prevents the shatter of the window if the inner pane breaks. The outer pane is not structural. The outer pane gives a rigid, hard, scratch-resistant surface. A conductive strip on the inner face of the outer glass pane permits electrical heating for window anti-icing and defogging. Functional Description To open the window, operate the handle. This turns a bellcrank, which is connected to other bellcranks at the rear, top, and bottom of the window. This moves the window inboard. The forward roller prevents backward movement of the window until there is sufficient clearance. This lets free movement back to the latched open position. When the window is moved to the rear, the lower aft roller moves to the window open latch plate. The window open latch plate is spring-loaded to lock the window in the open position. WINDOWS - CONTROL CABIN SLIDING WINDOWS - NO. 2 OPENABLE WINDOW EFFECTIVITY GUN ALL 56-12-00 Page 1 D633A101-GUN Oct 10/2002 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-12-00-001 The window is unlocked from its locked open position when you pull forward on the latch mechanism rod. This releases the window open latch plate and lets the window move forward. While the window moves forward, it resets the window open latch plate. Move the window forward by its handle until it touches the forward stops. As the handle is turned, the window is moved outboard, guided by a guide pin in the track, until the window is closed against the window frame. When you release the handle, a trigger bolt latches the window closed. Normal Operation To open the window, hold the trigger and turn the handle back and inboard. After the window moves inboard, move it back until it locks it in the open position. To close the window, pull forward on the latch mechanism rod to unlock the window. Hold the trigger and move the window forward until you can turn the handle forward and outboard. When you release the trigger, the window latches. Emergency Operation To open the window, push the external access door, and pull the external release handle. This will position the window inwards. Then move the window to the rear. Training Information Point WARNING: BE CAREFUL WHEN YOU DO WORK ON THE WINDOW NO. 2. THE OUTPUT VOLTAGE OF THE AUTOTRANSFORMER IS 250-350 VOLTS. THIS CAN CAUSE INJURY TO PERSONS. WINDOWS - CONTROL CABIN SLIDING WINDOWS - NO. 2 OPENABLE WINDOW EFFECTIVITY GUN ALL 56-12-00 Page 2 D633A101-GUN Oct 10/2002 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-12-00-001 WINDOWS - CONTROL CABIN SLIDING WINDOWS - NO. 2 OPENABLE WINDOW WINDOWS - CONTROL CABIN SLIDING WINDOWS - NO. 2 OPENABLE WINDOW EFFECTIVITY GUN ALL 56-12-00 Page 3 D633A101-GUN Feb 10/2003 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-12-00-001 GUN 001-019, 101-110, 201-999 PRE SL 737-56-012 General The passenger compartment windows have these components: * Outer pane * Middle pane * Inner pane. The outer and middle panes are structural. The windows are plug type windows. The outer pane is made of stretched acrylic plastic. It is rectangular with rounded corners and a beveled outer edge to fit with the window frame. The shape of the pane is curved to align with the fuselage contour. The middle pane gives the structural fail-safe function. It can hold 1.5 times the normal pressure load. The middle pane is made of cast acrylic and has a shape like the outer pane, but with an edge not beveled. The middle pane is contained in the window seal. A small breather hole is near the bottom of the middle pane. The inner pane is not structural. GUN 020-099, 111-118; GUN 001-019, 101-110, 201-999 POST SL 737-56-012 General The passenger compartment windows have these components: * Outer pane * Middle pane * Airflow dampener * Inner pane. The outer and middle panes are structural. The windows are plug type windows. The outer pane is made of stretched acrylic plastic. It is rectangular with rounded corners and a beveled outer edge to fit with the window frame. The shape of the pane is curved to align with the fuselage contour. The middle pane gives the structural fail-safe function. It can hold 1.5 times the normal pressure load. The middle pane is made of cast acrylic and has a shape like the outer pane, but with an edge not beveled. The middle pane is contained in the window seal. A small breather hole is near the top of the middle pane. WINDOWS - PASSENGER CABIN WINDOWS - GENERAL DESCRIPTION EFFECTIVITY GUN ALL 56-21-00 Page 1 D633A101-GUN Oct 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-21-00-001 GUN 020-099, 111-118; GUN 001-019, 101-110, 201-999 POST SL 737-56-012 (Continued) The airflow dampener helps to prevent the window from fogging during flight. The airflow dampener is made of injected molded white colored polycarbonate. The airflow dampener is attached above the breather hole on the middle pane. The inner pane is not structural. GUN ALL Location The passenger compartment windows are between the fuselage frames in the passenger compartment. WINDOWS - PASSENGER CABIN WINDOWS - GENERAL DESCRIPTION EFFECTIVITY GUN ALL 56-21-00 Page 2 D633A101-GUN Oct 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-21-00-001 WINDOWS - PASSENGER CABIN WINDOWS - GENERAL DESCRIPTION WINDOWS - PASSENGER CABIN WINDOWS - GENERAL DESCRIPTION EFFECTIVITY GUN 001-019, 101-110, 201-999 PRE SL 737-56-012 56-21-00 Page 3 D633A101-GUN Jun 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-21-00-001 WINDOWS - PASSENGER CABIN WINDOWS - GENERAL DESCRIPTION WINDOWS - PASSENGER CABIN WINDOWS - GENERAL DESCRIPTION EFFECTIVITY GUN 020-099, 111-118; GUN 001-019, 101-110, 201-999 POST SL 737-56-012 56-21-00 Page 4 D633A101-GUN Oct 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-21-00-001 GUN 001-019, 101-110, 201-999 PRE SL 737-56-012 General The emergency exit window has these components: * Outer pane * Middle pane * Inner pane. The outer and middle panes are structural. The windows are plug type windows. The outer pane is made of stretched acrylic plastic. It is rectangular in shape with rounded corners and a beveled outer edge to fit with the window frame. The shape the pane is curved to align with the fuselage contour. The middle pane gives the structural fail-safe function. It can hold 1.5 times the normal pressure load. The middle pane is made of cast acrylic and has a shape like the outer pane, but with an edge not beveled. The middle pane is contained in the window seal. A small breather hole is near the bottom of the middle pane. The inner pane is not structural. GUN 020-099, 111-118; GUN 001-019, 101-110, 201-999 POST SL 737-56-012 General The emergency exit window has these components: * Outer pane * Middle pane * Inner pane. The outer and middle panes are structural. The windows are plug type windows. The outer pane is made of stretched acrylic plastic. It is rectangular in shape with rounded corners and a beveled outer edge to fit with the window frame. The shape the pane is curved to align with the fuselage contour. The middle pane gives the structural fail-safe function. It can hold 1.5 times the normal pressure load. The middle pane is made of cast acrylic and has a shape like the outer pane, but with an edge not beveled. The middle pane is contained in the window seal. A small breather hole is near the top of the middle pane. The inner pane is not structural. GUN ALL WINDOWS - EMERGENCY EXIT WINDOW - GENERAL DESCRIPTION EFFECTIVITY GUN ALL 56-22-00 Page 1 D633A101-GUN Oct 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-22-00-001 Location The emergency exit windows are in each emergency exit in the passenger compartment. WINDOWS - EMERGENCY EXIT WINDOW - GENERAL DESCRIPTION EFFECTIVITY GUN ALL 56-22-00 Page 2 D633A101-GUN Jun 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-22-00-001 WINDOWS - EMERGENCY EXIT WINDOW - GENERAL DESCRIPTION WINDOWS - EMERGENCY EXIT WINDOW - GENERAL DESCRIPTION EFFECTIVITY GUN 001-019, 101-110, 201-999 PRE SL 737-56-012 56-22-00 Page 3 D633A101-GUN Jun 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-22-00-001 WINDOWS - EMERGENCY EXIT WINDOW - GENERAL DESCRIPTION WINDOWS - EMERGENCY EXIT WINDOW - GENERAL DESCRIPTION EFFECTIVITY GUN 020-099, 111-118; GUN 001-019, 101-110, 201-999 POST SL 737-56-012 56-22-00 Page 4 D633A101-GUN Oct 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-22-00-001 THIS PAGE IS INTENTIONALLY LEFT BLANK WINDOWS - EMERGENCY EXIT WINDOW - GENERAL DESCRIPTION 56-31-00 Page 1 D633A101-GUN Oct 10/2002 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL General The door-mounted windows have these components: * Outer pane * Middle pane * Inner pane. The outer and middle panes are structural. The outer and middle panes are resistant to 1.5 times the normal pressure loads at a temperature of 70F. The outer pane is made of stretched acrylic for more strength. The middle pane is made of a cast acrylic. The inner pane is not structural. It connects to the cabin sidewall panel. The inner pane is made from polycarbonate. WINDOWS - DOOR-MOUNTED WINDOWS - GENERAL DESCRIPTION EFFECTIVITY GUN ALL 56-31-00 Page 2 D633A101-GUN Oct 10/2002 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-31-00-001 WINDOWS - DOOR-MOUNTED WINDOWS - GENERAL DESCRIPTION WINDOWS - DOOR-MOUNTED WINDOWS - GENERAL DESCRIPTION EFFECTIVITY GUN 001-099, 101-118 56-31-00 Page 3 D633A101-GUN Oct 10/2006 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-31-00-001 WINDOWS - DOOR-MOUNTED WINDOWS - GENERAL DESCRIPTION WINDOWS - DOOR-MOUNTED WINDOWS - GENERAL DESCRIPTION EFFECTIVITY GUN 201-999 56-31-00 Page 4 D633A101-GUN Oct 10/2005 BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details. 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL 56-31-00-001
