Model: ASTM B221

Structural Angle

Properties:

Fabrication Method
Extruded
Overall Height
1.000 inches
Overall Width
2.000 inches
Left Side Flange Thickness
0.125 inches
Basic Shape Style
Angle
Fillet Radius Where Left Flange Joins Base Flange
0.156 inches
Base Flange Thickness
0.125 inches
First Tip Radius
0.125 inches
Weight Per Unit Measure
0.430 pounds per linear foot
First Tip Style
Right quarter radius
Second Tip Radius
0.125 inches
Second Tip Relationship To First Tip
Not identical
Second Tip Style
Upper radius
Left Inside Angle
90.0 degrees
Heat Treatment
T-3511 solution heat treated
Material
Aluminum alloy ams-qq-a-200/3, alloy 2024
Material
Aluminum alloy ams-qq-a-200/3, alloy 2024
Nondefinitive Specification/std Data
Alloy 2024, temper t3511
NSN
9540-01-071-8248
Part Number
ASTM B221
Description
Angle,structural
CAGE
81346

Part ASTM B221 NSN 9540-01-071-8248

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
37017
FIIG:
A13100
Concept No.:
App. Key:
AB
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:
0.4000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
Z
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
013140
UFC:
05390
LTL:
60.0
LCL:
--
WCC:
576
TCC:
Z
SHC:
R
ACC:
Construction Materials

End Items End applications NSN 9540-01-071-8248 is a component of

  • Stratofortress B-52 Aircraft
  • F-111 (fms Only) Aircraft
  • E-3a Awacs Aircraft
  • F-16 Aircraft

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