Model: CVC10012-119CEX144
Structural BeamProperties:
Fabrication Method
Extruded
Overall Height
1.500 inches
Length
12.000 feet
Left Side Top Flange Thickness
0.063 inches
Right Side Top Flange Thickness
0.063 inches
End Application
B-2 bomber
Basic Shape Style
T shape
Leg Thickness
0.063 inches
Left Side Top Flange Distance To Center Of Both Flanges
0.838 inches
Right Side Top Flange Distance To Center Of Both Flanges
1.850 inches
Fillet Radius Where Top Left Flange Joins Web Flange/leg
0.090 inches
Fillet Radius Where Top Right Flange Joins Web Flange/leg
0.090 inches
Top Flange Width
2.688 inches
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
51.0 degrees
Left Top Inside Angle
129.0 degrees
Heat Treatment
T-6511 solution heat treated
Material
Aluminum alloy ams-qq-a-200/11, alloy 7075
Material
Aluminum alloy ams-qq-a-200/11, alloy 7075
Nondefinitive Specification/std Data
Alloy 7075 and temper t6511
NSN
9540-01-428-2772
Part Number
CVC10012-119CEX144
Description
Beam,structural
CAGE
Part CVC10012-119CEX144 NSN 9540-01-428-2772
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 indicatorsHMIC:
N
PMIC:
A
ESD:
ESD:
MMAC:
CRITL:
X Packaging & Shipping
Pack Size:
-- Paclk Weight:
1.1000lbs Item Weight:
-- Item Dim:
-- OPI:
M SPI No.:
SPI Rev.:
SPC Mkg:
00 LVL_A:
Z LVL_B:
Freight Classification
NMFC:
104420 UFC:
53800 LTL:
50.0 LCL:
-- WCC:
574 TCC:
Z SHC:
9 ACC:
Trailers/Vehicles End Items End applications NSN 9540-01-428-2772 is a component of
- B-2 Bomber
- Ch-47 Chinook Helicopter
- Galaxy C-5 Aircraft
- Hc-130) Ec-130e Mc-130h Sof ( Ac-130h Aircraft
- B-2 Bomber (atb) Aircraft
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