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Catalog item

BEAM,STRUCTURAL

9540FSC
00NCB code
610-6902Item number
NIIN 00-610-6902
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DEMIL code
A

Identification

Item name code
37018
PINC
0037018
Criticality code
X
II
0
DEMIL code
A
NIIN assigned
05-FEB-75
Precious metals indicator
U
Hazardous material indicator
N
Last known source of supply
S9I

Part numbers

Part numberCAGECAGE statusRNCCRNVCDocument availability codeRNAACRNFCRNSC
1M5507-1139676301
THE BOEING COMPANY DIV DEFENSE
A315SB3D
AMS-QQA200-1381343
SOCIETY OF AUTOMOTIVE ENGINEERS INC
R59EZZB
QQA200-1381348
FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
A594SB3B
AMS-QQA200-130U583
SAE INTERNATIONAL DBA SAE INTERNATIONAL
A31EZZ

Characteristics

LEFT TOP INSIDE ANGLEDEGREES NOMINAL 90.0
RIGHT TOP INSIDE ANGLEDEGREES NOMINAL 90.0
LENGTHFEET MINIMUM 10.000 AND FEET MAXIMUM 12.000
RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGESINCHES NOMINAL 1.650
LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGESINCHES NOMINAL 1.650
THIRD TIP RELATIONSHIP TO PRECEDING TIPSIDENTICAL W/FIRST TIP
LEFT SIDE TOP FLANGE THICKNESSINCHES NOMINAL 0.062
FABRICATION METHODEXTRUDED
OVERALL HEIGHTINCHES NOMINAL 1.700
TOP FLANGE WIDTHINCHES NOMINAL 3.300
WEIGHT PER UNIT MEASUREPOUNDS PER LINEAR FOOT 0.360
FIRST TIP STYLE
SECOND TIP RELATIONSHIP TO FIRST TIPIDENTICAL
FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEGINCHES NOMINAL 0.094
FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEGINCHES NOMINAL 0.094
MATERIALALUMINUM ALLOY 7178
MATERIAL DOCUMENT AND CLASSIFICATIONFED SPEC 1ST MATERIAL RESPONSE QQ-A-200 TO 13
NONDEFINITIVE SPEC/STD DATATEMPER 0
RIGHT SIDE TOP FLANGE THICKNESSINCHES NOMINAL 0.062
BASIC SHAPE STYLE
LEG THICKNESSINCHES NOMINAL 0.062
HEAT TREATMENTO-ANNEALED

MOE rules

MOE rule
ZG01
MOE CD
ZG
Date assigned
01-APR-91
PICA
ZG
PICA LOA
81
Auth collab
ZG

Freight

ACTY CD
KZ

Related items

Standardization

Item standardization code
2
Orig stdzn dec
KZ
Dt stdzn dec
27-DEC-1979
NIIN status code
0

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