Catalog item

SHEET,METAL

9535FSC
01NCB code
532-0294Item number
NIIN 01-532-0294
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DEMIL code
A

Identification

Item name code
37015
PINC
0037015
Criticality code
X
II
0
DEMIL code
A
DEMIL integrity code
1
NIIN assigned
26-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-CD0-0,032X12X3681343
SOCIETY OF AUTOMOTIVE ENGINEERS INC
R59E9Z4D
AMS-QQ-A-250/581343
SOCIETY OF AUTOMOTIVE ENGINEERS INC
R59E9Z4B
AMS-QQ-A-250/5-O-0.032X12X3681343
SOCIETY OF AUTOMOTIVE ENGINEERS INC
R59E9Z4B
AMS-QQ-A-250/50U583
SAE INTERNATIONAL DBA SAE INTERNATIONAL
A31EZZ
AMS-QQ-A-250/5-O-0.032X12X360U583
SAE INTERNATIONAL DBA SAE INTERNATIONAL
A32EZZ

Characteristics

FABRICATION METHODROLLED
WIDTHINCHES NOMINAL 12.000
LENGTHINCHES NOMINAL 36.000
CROSS-SECTIONAL THICKNESSINCHES NOMINAL 0.0320
END ITEM IDENTIFICATIONFUSELAGE F4F JET AIRCRAFT
BASIC SHAPE STYLE
USAGE DESIGNAIRCRAFT
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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS; MAXIMUM TENSILE STRENGTH 30000.0 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000.0 POUNDS PER SQUARE INCH
HEAT TREATMENTO-ANNEALED
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
26-JUL-2005
NIIN status code
0

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