Model: 513757

Structural Beam

Properties:

Fabrication Method
Extruded
Overall Height
1.500 inches
Length
Between 10.000 feet and 12.000 feet
Left Side Top Flange Thickness
0.064 inches
Right Side Top Flange Thickness
0.064 inches
Basic Shape Style
T shape
Leg Thickness
0.064 inches
Left Side Top Flange Distance To Center Of Both Flanges
0.750 inches
Right Side Top Flange Distance To Center Of Both Flanges
0.750 inches
Fillet Radius Where Top Left Flange Joins Web Flange/leg
0.125 inches
Fillet Radius Where Top Right Flange Joins Web Flange/leg
0.125 inches
Top Flange Width
1.500 inches
Weight Per Unit Measure
0.234 pounds per linear foot
First Tip Style
Square end
Second Tip Relationship To First Tip
Identical
Third Tip Relationship To Preceding Tips
Identical w/first tip
Right Top Inside Angle
90.0 degrees
Left Top Inside Angle
90.0 degrees
Heat Treatment
T-6511 solution heat treated
Material
Aluminum alloy ams-qq-a-200/8, alloy 6061
Material
Aluminum alloy ams-qq-a-200/8, alloy 6061
Specification Data
81755-k40 manufacturers standard
Nondefinitive Specification/std Data
T6511 temper
NSN
9540-01-071-2153
Part Number
513757
Description
Beam,structural
CAGE
59616

Part 513757 NSN 9540-01-071-2153

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
37018
FIIG:
A13100
Concept No.:
App. Key:
AS
Cond. Code:
2
Status:
A

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
A
ESD:
ESD:
MMAC:
CRITL:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
0.2000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
ZZ
LVL_A:
Z
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
013455
UFC:
05820
LTL:
60.0
LCL:
--
WCC:
576
TCC:
Z
SHC:
R
ACC:
Construction Materials

End Items End applications NSN 9540-01-071-2153 is a component of

  • F-16 Aircraft

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