Catalog item

PLATE,METAL

9535FSC
01NCB code
531-7803Item number
NIIN 01-531-7803
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DEMIL code
A

Identification

Item name code
37013
PINC
0037013
Criticality code
X
II
0
DEMIL code
A
DEMIL integrity code
1
NIIN assigned
21-JUL-05
Precious metals indicator
A
ADP equipment code
0
Hazardous material indicator
N
ESD/EMI code
A

Part numbers

Part numberCAGECAGE statusRNCCRNVCDocument availability codeRNAACRNFCRNSC
AMS-QQ-A-250/5-T351-0.250X12X4881343
SOCIETY OF AUTOMOTIVE ENGINEERS INC
R59E9Z4B
AMS-QQ-A-250/5-CDT351-0,25X12X4881343
SOCIETY OF AUTOMOTIVE ENGINEERS INC
R59E9Z4D
AMS-QQ-A-250/581343
SOCIETY OF AUTOMOTIVE ENGINEERS INC
R59E9Z4B
AMS-QQ-A-250/50U583
SAE INTERNATIONAL DBA SAE INTERNATIONAL
A31EZZ
AMS-QQ-A-250/5-T351-0.250X12X480U583
SAE INTERNATIONAL DBA SAE INTERNATIONAL
A32EZZ

Characteristics

FABRICATION METHODROLLED
WIDTHINCHES NOMINAL 12.000
LENGTHINCHES NOMINAL 48.000
CROSS-SECTIONAL THICKNESSINCHES NOMINAL 0.2500
END ITEM IDENTIFICATIONFUSELAGE F4F JET AIRCRAFT
BASIC SHAPE STYLE
USAGE DESIGNAIRCRAFT
MINIMUM TENSILE STRENGTHPOUNDS PER SQUARE INCH 62000
MINIMUM YIELD STRENGTHPOUNDS PER SQUARE INCH 40000
SPECIAL FEATURESTHIN LAYERS APPROXIMATELY EQUAL THICKNESS, OF ALUMINUM ALLOY 1230 ANODIC TO THE CORE ARE BONDED TO BOTH SURFACES; NOMINAL CLADDING THICKNESS FOR EACH LAYER TO BE 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED PLATE THICKNESS
HEAT TREATMENTT-351 SOLUTION HEAT TREATED
MATERIALALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATIONFED SPEC 1ST MATERIAL RESPONSE QQ-A-250 TO 5

MOE rules

MOE ruleMOE CDDate assignedPICAPICA LOAAuth collab
ZF01ZF01-JUL-18ZF81ZF
ZG01ZG01-JUL-05ZG81ZG

Freight

ACTY CD
LI

Related items

Standardization

Item standardization code
5
Orig stdzn dec
97
Dt stdzn dec
21-JUL-2005
NIIN status code
0

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Your request goes to A-DEFENSE, a US Defense supplier in Texas, who will reply by email.