BAC1506 885 With NSN 9540-01-230-0477 - The Boeing Company

Mfg Part Number: BAC1506 885	Alternate P/N: BAC1506885	NSN : 9540-01-230-0477
NIIN : 012300477	CAGE Code : 81205	Manufacturer: The Boeing Company
Item Name : Beam Structural	FSC : 9540 Structural Shapes Nonferrous Base Metal

Thank you for your interest in BAC1506 885, the Part number listed alongside the NSN 9540-01-230-0477. This particular BAC1506 885 is manufactured by The Boeing Company, and we have current availability on our website now. If you are interested in this particular item, please fill out and submit the RFQ form as provided below at your earliest convenience. Once our team members receive a completed form, they will rapidly create a competitive quote that has been tailored with your individual needs and requirements in mind. With team members always available for customers 24/7x365, responses will be given in just 15 minutes or less.

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Characteristics Data of NSN 9540-01-230-0477, 9540012300477

MRC	Criteria	Characteristic
AARN	FABRICATION METHOD	EXTRUDED
ABKW	OVERALL HEIGHT	1.800 INCHES MINIMUM AND 1.802 INCHES MAXIMUM
ABRY	LENGTH	0.670 FEET NOMINAL
ADXR	LEFT SIDE TOP FLANGE THICKNESS	0.250 INCHES NOMINAL
ADXS	RIGHT SIDE TOP FLANGE THICKNESS	0.250 INCHES NOMINAL
AGTA	BASIC SHAPE STYLE	T SHAPE
AJJP	LEG THICKNESS	0.330 INCHES NOMINAL
BPXD	LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES	1.160 INCHES NOMINAL
BPXG	RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES	1.160 INCHES NOMINAL
BPXJ	FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG	0.130 INCHES NOMINAL
BPXL	FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG	0.130 INCHES NOMINAL
BQJG	TOP FLANGE WIDTH	2.320 INCHES NOMINAL
BRFD	WEIGHT PER UNIT MEASURE	1.316 POUNDS PER LINEAR FOOT
CMZY	FIRST TIP STYLE	SQUARE END
CNQJ	SECOND TIP RELATIONSHIP TO FIRST TIP	IDENTICAL
CNQL	THIRD TIP RELATIONSHIP TO PRECEDING TIPS	IDENTICAL W/FIRST TIP
CRZC	RIGHT TOP INSIDE ANGLE	96.50 DEGREES NOMINAL
CSMZ	LEFT TOP INSIDE ANGLE	83.5 DEGREES NOMINAL
MATT	MATERIAL	ALUMINUM ALLOY 7075
MDCL	MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-367, ALLOY 7075 FED SPEC 1ST MATERIAL RESPONSE