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Boeing 747
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2
3
4
3
1
1
2
4
0
1
2
3
4
5 6 7
10
98
NOTCH
1
SIGNAL
WITH
THE
TRANSDUCER
AT
POSITION
Y
NOTCH
2
SIGNAL
WITH
THE
TRANSDUCER
AT
POSITION
Z
POSITIONS
FOR
OTHER
FUSE PINS THAT
ARE
LONGITUDINAL
WAVE
SHEAR
WAVE
SOUND
PATH
OF
INTERNAL
REFLECTIONS
DETAIL
I
REFERENCE
STANDARD
BACK
SURFACE
SIGNAL
WITH
THE
TRANSDUCER
AT
POSITION
X
INTERNAL
REFLECTIONS
THIS
FIGURE
SHOWS
SIGNAL
POSITIONS
FOR
REFERENCE
STANDARD NDT4115.
SEE
TABLE
1
FOR THE
SPECIFIED
SIGNAL
NOT THE
SAME
AS
THIS
REFERENCE STANDARD.
NOTE:
____
NOTCH
1
POSITION
Y
POSITION
X
POSITION
Z
NOTCH
2
2130665 S0000459174_V1
Reference Standard Calibration
Figure 5
747
NONDESTRUCTIVE TEST MANUAL
PART 4 54-30-07
Page 10
Nov 15/2015D6-7170
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ALL

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