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1  SETUP  HIGH VOLTAGE PROBE  MIT5-89354  - FROM THE INBD SIDE OF THE WINDOW ADJACENT TO THE HEAT TERMINAL. (a) WINDOW ATTACHMENT FASTENER HOLE INSERT HIGH VOLTAGE PROBE INTO 
2  SETUP  LEAD WIRE  POMONA MODEL B-4 OR EQUIVALENT  1  INSERT LEAD WIRE INTO HEAT TERMINAL. (b) 
3  TEST  DIELECTRIC TEST  - 1  DO DIELECTRIC LEAK TEST (c), (d) (NOT SHOWN) 
4  SETUP  HIGH VOLTAGE PROBE  MIT5-89354  - FROM THE INBD SIDE OF THE WINDOW ADJACENT TO THE HEAT TERMINAL. (a) WINDOW ATTACHMENT FASTENER HOLE INSERT HIGH VOLTAGE PROBE INTO 
5  SETUP  LEAD WIRE  POMONA MODEL B-4 OR EQUIVALENT  1  INSERT LEAD WIRE INTO HEAT TERMINAL. (b) 
6  TEST  DIELECTRIC TEST  - 1  DO DIELECTRIC TEST (c), (e) (NOT SHOWN) 

(a)  
SECURE PROBE IN PLACE BY USING THE EXPANDING ADJUSTMENT KNOB.

(b)  
ENSURE LEAD WIRE IS IN CONTACT WITH HEAT TERMINAL THREADS.

(c)  
DO THE DIELECTRIC LEAD TEST USING 2500 VOLTS RMS, 60Hz, HOLD VOLTAGE AT 2500 VOLTS FOR APPROXIMATELY 10 TO 15 SECONDS.

(d)  
IF LEAKAGE IS 5 MILLIAMPERES OR GREATER THE WINDOW MUST BE REPLACED.

(e)  
IF LEAKAGE IS LESS THAN 5 MILLIAMPERES CONTINUE WITH REMAINDER OF RETROFIT INSTRUCTIONS. IF LEAKAGE IS 5 MILLIAMPERES OR GREATER THE WINDOW MUST BE REPLACED.

Window No. 1 Installation
Figure 401 (Sheet 9)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
M07680
A

737-300/400/500
MAINTENANCE MANUAL

START
HERE
AIRPLANE

NO. 1 WINDSHIELD
VIEW FROM OUTSIDE
(LEFT SHOWN, RIGHT OPPOSITE)

NOTE:THIS IS AN EXAMPLE OF HOW YOU CAN TIGHTEN THE FASTENERS FOR THE WINDOW. ANY PATTERN THAT IS ALMOST THE SAME IS PERMITTED. FIRST ATTACH THE WINDOW AT AS MANY POINTS THAT ARE OPPOSITE ON THE WINDOW. DO THIS AS EARLY IN THE FASTENER TORQUE SEQUENCE AS POSSIBLE.

CONTINUE IN THIS PATTERN. ALWAYS GO TO A
FASTENER THAT IS IN THE MIDDLE OF TWO
INSTALLED FASTENERS. YOU MUST GO TO A SIDE
OTHER THAN THE SIDE ON WHICH A FASTENER WAS
JUST TIGHTENED.

Window No. 1 Retaining Bolt Torque Sequence Figure 402
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

100.0
90.0
80.0
 70.0
 60.0
50.0
40.0
30.0
20.0
10.0
 9.0
 8.0
7.0
 6.0
 5.0
 4.0
 3.0
 2.0
 1.0
(F)
50 60 70 80 90 100110 120 130140

(C)
10 15.6 21.1 26.7 32.2 37.8 43.3 48.9 54.4 60.0

TEMPERATURE IN `F
FOR SHOP HANDLING AND FLY AWAY

DO NOT CURE SEALANT BELOW 50`F (10`C)

DO NOT CURE SEALANT ABOVE 140`F (60`C)
REX A DUROMETER READING OF 30 (MINIMUM)

Sealant Cure Times Figure 403
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 WINDOW NO. 1 - INSPECTION/CHECK
_______________________________
 1.  General_______
 A.  There is one task in this procedure, an inspection of the No. 1 window.
 TASK 56-11-11-206-013-B00
 2.  Window No. 1 Inspection_______________________
 A.  References
 (1)  
AMM 30-41-00/501, Control Cabin Window Anti-Icing System

 (2)  
AMM 56-11-00/201, Control Cabin Fixed Windows

 (3)  
AMM 56-11-11/401, Window No. 1

 B.  Access
 (1)  Location Zone
　
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