Boeing 747 - Page 44

TRANSDUCER GUIDE
TRANSDUCER
DIAGONAL BRACE
(ADJACENT STRUCTURE
IS NOT SHOWN)
FUSE PIN WITH
INSERT REMOVED
1
3
2
3
1
2
80%
4
2
6
8
0
10
100%
20%
40%
60%
%
10
8
6
4
2
0
0 2
10
864
/
P
OFF
1
5
2.25
+1
+5
A
U
D
E
60
4020
0
0
10N
10P
OFF
ON
_____ NOTES:
FOR THE CORRECT SCREEN POSITION.
BACK SURFACE SIGNAL FOLLOWED BY MODE CONVERSION SIGNALS. SEE TABLE 2
MONITOR FROM 10 TO 30 PERCENT OF THE FULL SCREEN WIDTH DURING THE INSPECTION
INITIAL PULSE SIGNAL
2130654 S0000459168_V1
Fuse Pin Inspection Area
Figure 9
747
NONDESTRUCTIVE TEST MANUAL
PART 4 54-30-06
Page 14
Nov 15/2015D6-7170
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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