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Catalog item

BEAM,STRUCTURAL

9540FSC
01NCB code
478-9730Item number
NIIN 01-478-9730
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DEMIL code
B

Identification

Item name code
37018
PINC
0037018
Criticality code
X
II
0
DEMIL code
B
DEMIL integrity code
3
NIIN assigned
04-OCT-00
Precious metals indicator
A
ADP equipment code
0
Hazardous material indicator
N
ESD/EMI code
A
Schedule B export code
7601209500

Part numbers

Part number
HS1006DD61-0708
CAGE
8V613
THE BOEING COMPANY
CAGE status
A
RNCC
3
RNVC
2
Document availability code
2
RNAAC
9Z
RNFC
4
RNSC
A

Characteristics

FABRICATION METHODEXTRUDED
OVERALL HEIGHTINCHES NOMINAL 1.180
LENGTHINCHES NOMINAL 7.250
LEFT SIDE TOP FLANGE THICKNESSINCHES NOMINAL 0.050
RIGHT SIDE TOP FLANGE THICKNESSINCHES NOMINAL 0.050
END ITEM IDENTIFICATIONAPACHE HELICOPTER
BASIC SHAPE STYLE
LEG THICKNESSINCHES NOMINAL 0.050
LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGESINCHES NOMINAL 1.000
RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGESINCHES NOMINAL 1.000
FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEGINCHES NOMINAL 0.062
FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEGINCHES NOMINAL 0.062
TOP FLANGE WIDTHINCHES NOMINAL 2.000
FIRST TIP STYLE
SECOND TIP RELATIONSHIP TO FIRST TIPIDENTICAL
THIRD TIP RELATIONSHIP TO PRECEDING TIPSIDENTICAL W/FIRST TIP
RIGHT TOP INSIDE ANGLEDEGREES NOMINAL 90.0
LEFT TOP INSIDE ANGLEDEGREES NOMINAL 90.0
PART NAME ASSIGNED BY CONTROLLING AGENCYEXTRUSION, TEE, ALUMINUM ALLOY
HEAT TREATMENTT-4 SOLUTION HEAT TREATED OR T-3511 SOLUTION HEAT TREATED
MATERIALALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATIONFED SPEC 1ST MATERIAL RESPONSE QQ-A-200 TO 3

MOE rules

MOE rule
ZK01
MOE CD
ZK
Date assigned
01-OCT-00
PICA
ZK
PICA LOA
81
Auth collab
ZK

Freight

ACTY CD
QE

Related items

Standardization

Item standardization code
5
Orig stdzn dec
97
Dt stdzn dec
04-OCT-2000
NIIN status code
0

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