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Catalog item

SHEET,METAL

9535FSC

01NCB code

531-6284Item number

NIIN 01-531-6284

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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: 15-JUL-05
Precious metals indicator: A
ADP equipment code: 0
Hazardous material indicator: N
ESD/EMI code: A

Part numbers

Part number	CAGE	CAGE status	RNCC	RNVC	Document availability code	RNAAC	RNFC	RNSC
AMS-QQ-A-250/4-CDT3-0,14X12X48	81343 SOCIETY OF AUTOMOTIVE ENGINEERS INC	R	5	9	E	9Z	4	D
AMS-QQ-A-250/4-T3-0.140X12X48	81343 SOCIETY OF AUTOMOTIVE ENGINEERS INC	R	5	9	E	9Z	4	B
AMS-QQ-A-250/4	81343 SOCIETY OF AUTOMOTIVE ENGINEERS INC	R	5	9	E	9Z	4	B
AMS-QQ-A-250/4	0U583 SAE INTERNATIONAL DBA SAE INTERNATIONAL	A	3	1	E	ZZ
AMS-QQ-A-250/4-T3-0.140X12X48	0U583 SAE INTERNATIONAL DBA SAE INTERNATIONAL	A	3	2	E	ZZ

Characteristics

FABRICATION METHOD	ROLLED
WIDTH	INCHES NOMINAL 12.000
LENGTH	INCHES NOMINAL 48.000
CROSS-SECTIONAL THICKNESS	INCHES NOMINAL 0.1400
END ITEM IDENTIFICATION	FUSELAGE F4F JET AIRCRAFT
BASIC SHAPE STYLE
USAGE DESIGN	AIRCRAFT
MINIMUM TENSILE STRENGTH	POUNDS PER SQUARE INCH 64000
MINIMUM YIELD STRENGTH	POUNDS PER SQUARE INCH 42000
HEAT TREATMENT	T-3 SOLUTION HEAT TREATED
MATERIAL	ALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATION	FED SPEC 1ST MATERIAL RESPONSE QQ-A-250 TO 4

MOE rules

MOE rule	MOE CD	Date assigned	PICA	PICA LOA	Auth collab
ZF01	ZF	01-JUL-18	ZF	81	ZF
ZG01	ZG	01-JUL-05	ZG	81	ZG

Freight

ACTY CD: LI

Related items

Standardization

Item standardization code: 5
Orig stdzn dec: 97
Dt stdzn dec: 15-JUL-2005
NIIN status code: 0

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