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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
SEE D SEE ASEE C
A  SEE A
A 
1. WINDOW NO. 1 
WINDOW FRAME 
SEE  B  2. ALUMINUM SPACER 
WINDOW NO. 1 ASSEMBLY 
SEE  C  (LEFT SHOWN, RIGHT OPPOSITE)  3. RETAINING BOLT 
STAINLESS  B  4. ETHYLENE PROYPYLENE 
STEEL Z-CHANNEL  OR SILICONE RUBBER 
(BONDED IN POSITION)  O-RING 
1  5. ALUMINUM 
FLAT WASHER 
AERODYNAMIC SMOOTHER 
WINDOW FRAME  B 
9. NYLON CORD 

8. PRESSURE SEAL (BONDED IN 7. WIRE CLAMP POSITION) SEALANT (EXAMPLE) 6. HEX HEAD
Z-CHANNEL SELF-LOCKING
EXAMPLE FASTENER INSTALLATION ON TOP, NUT
1
BOTTOM AND FORWARD EDGE OF WINDOW NO. 1
NO. 1
WIRE MESH  A
WINDOW VINYL CORE(4 LOCATIONS)
PARTING
MEDIUM

NYLON OUTER PANEWINDOW
FRAME CORD INNERSEALANT PANE
Z-CHANNEL BOLT, 100` HEAD
PRESSURE
PHILLIPS RECESS
SEAL
A-A
1 ____RETAINING WINDOW FRAME
NOTE: REMOVED FOR CLARITY.
SPACERMETAL FLEX
1
NOT ON ALL WINDOWS
B-B
Window No. 1 Installation
Figure 401 (Sheet 1)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
Z-SEAL OUTERWINDOW13. WINDOW PANENO. 1FRAME POST
URETHANE VINYL CORE
12. RETAINING ANGLE
11. RETAINING INNER
ANGLE BOLT PANE
C
10. DOUBLER
0.03 MINIMUM CLEARANCE (WINDSHIELD WITHOUT CORK ON THE EDGE)
0.01 MINIMUM CLEARANCE
C

(WINDSHIELD WITH CORK ON THE EDGE)
(EXAMPLE, ALL BOLT LOCATIONS) EDGE OF WINDOW NO. 1 FASTENER INSTALLATION ON AFT C-C
B
17. HEX NUT, PLAIN
D  20. ALUMINUM 
SPACER 
14. ALUMINUM TERMINAL 
SPACER  INSULATOR 
SEAL WASHER 15. SILICONE RUBBER  D  BOLT 21. RETAINING 
16. ALUMINUM  22. ALUMINUM 
WASHER  WINDOW  WASHER 
WINDOW  NO. 1 
24. ETHYLENE PROPYLENE 
OR COLORED SILICONE 
RUBBER O-RING 
23. HEX HEAD 
19. RETAINING  SELF-LOCKING NUT 
BOLT 
SEAL, WASHER AND FASTENER 
FRAME WINDOW  ELECTRICAL THIN 18. HEX NUT, PLAIN  (EXAMPLE, 2 LOCATIONS) SEE  E 
D 

ELECTRICAL THIN CHECKNUT
SEAL, WASHER AND FASTENER (EXAMPLE, 2 LOCATIONS) (LOWER FASTENER SHOWN, UPPER FASTENER EQUIVALENT)
C
TPSR850308DJ
D-D
Window No. 1 Installation
Figure 401 (Sheet 2)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
WHEN USING ETHYLENE PROPYLENE O-RINGS, TRIM AS SHOWN TO OBTAIN 0.06 INCH DIMENSIONINSULATING TERMINAL
2 LOCATIONS. (NOT REQUIRED WITH NON-CONDUCTING
SEALANT
SPACER BEAD
Z-CHANNEL PRESSURE SEAL
SEAL

2

2

APPLICABLE TO SPACER APPLICABLE TO SPACER
5-89354-3044 AND -3045
5-89354-3043
F

F

2
APPLY AERODYNAMIC SMOOTHER TO THE CLEARANCE. THE SEALANT MUST NOT EXTEND MORE THAN TO +0.15 INCH OR LESS THAN 0.03 INCH FROM THE GLASS SURFACE.
Window No. 1 Installation Figure 401 (Sheet 3)
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 56-11-11
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
WINDOW NO. 1
　
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