9540-00-241-2712

Description: Structural Beam

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MILSPEC: Nonferrous Base Metal Structural Shapes

 Export Restrictions

Any part(s) quoted or sold by MilSpec.parts and re-sold (to a third party) CANNOT be sold to a USA embargoed country, company, entity, or person(s). Depending on the ECCN, these commodities may require export license or exception. Diversion contrary to U.S. law is prohibited. Unless otherwise noted, this sale, order or quote may include Munitions List Items (MLI) or Commerce Controlled List Items (CCLI). MLI/CCLI property is controlled by the US Government and in many cases cannot be transferred (exported, sold or given) to a foreign country, a non-US Citizen/National or a non- Permanent US Resident without a valid State/Commerce Department export authorization. It is the responsibility of (the Purchaser) to determine what the applicable requirements may be, to obtain all necessary authorizations, licenses or approvals and are subject to both review and acceptance by MilSpec.parts. The use, disposition, export and re-export of the property covered or included in this sale, order or quote is subject to the provisions of law referenced in End-Use Certificate DLA form 1822, DEC 2001, including, but not limited to, the Arms Export Control Act (22 USC 2751 et seq.); Export Administration Act of 1979 (50 USC App. 2401 et seq.) as contained under Executive Order 12924; International Traffic in Arms Regulations (22 CFR 120 et seq.); Export Administration Regulations (15 CFR 730 et seq.); Foreign Assets Control Regulations (31 CFR 500 et seq.) and the Espionage Act (18 USC 793 et seq.)

9540-00-241-2712 Properties

  • NSN:
    9540-00-241-2712
  • Description:
    Structural Beam
  • Shelf Life:
    N/A
  • DEMIL:
    NO
  • UOM:
    1 FT
  • Fabrication Method:
    Extruded
  • Overall Height:
    4.000 inches
  • Length:
    Between 10.000 feet and 12.000 feet
  • Left Side Top Flange Thickness:
    0.250 inches
  • Right Side Top Flange Thickness:
    0.250 inches
  • Basic Shape Style:
    I shape
  • First Tip Radius:
    0.250 inches
  • Right Side Bottom Flange Thickness:
    0.250 inches
  • Left Side Bottom Flange Thickness:
    0.250 inches
  • Left Side Top Flange Distance To Center Of Both Flanges:
    1.750 inches
  • Left Side Bottom Flange Distance To Center Of Both Flanges:
    1.750 inches
  • Right Side Top Flange Distance To Center Of Both Flanges:
    1.750 inches
  • Right Side Bottom Flange Distance To Center Of Both Flanges:
    1.750 inches
  • Fillet Radius Where Top Left Flange Joins Web Flange/leg:
    0.188 inches
  • Fillet Radius Where Bottom Left Flange Joins Web Flange/leg:
    0.188 inches
  • Fillet Radius Where Top Right Flange Joins Web Flange/leg:
    0.188 inches
  • Fillet Radius Where Bottom Right Flange Joins Web Flange/leg:
    0.188 inches
  • Web Flange Thickness:
    0.250 inches
  • Top Flange Width:
    3.500 inches
  • Bottom Flange Width:
    3.500 inches
  • Weight Per Unit Measure:
    3.120 pounds per linear foot
  • First Tip Style:
    Lower radius
  • Third Tip Radius:
    0.250 inches
  • Second Tip Relationship To First Tip:
    Identical
  • Third Tip Relationship To Preceding Tips:
    Not identical
  • Third Tip Style:
    Upper radius
  • Fourth Tip Relationship To Preceding Tips:
    Identical w/third tip
  • Right Top Inside Angle:
    90.0 degrees
  • Left Top Inside Angle:
    90.0 degrees
  • Left Bottom Inside Angle:
    90.0 degrees
  • Right Bottom Inside Angle:
    90.0 degrees
  • Heat Treatment:
    T-6 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:
    T-6 temper
Manufacturers and Part Numbers
Part Number
Brand
H199
Kaiser Aluminum And Chemical Corp
AMS-QQ-A-200/11
Society Of Automotive Engineers
35302
Aluminum Co Of America
AMS10134-3002
Society Of Automotive Engineers
10081
Reynolds Metals Co
AND10140-4006
Airforce-navy Aeronautical Design
QQ-A-200/11
Federal Specifications
Major Organizational Entities (MOE)
Entity
MOE Code
MOE Rule
PICA
DSOR
User:
DEPARTMENT OF THE AIR FORCE Dept. of the Air Force
MOE_CD:
DF
MOE_RL:
FGGI
PICA:
GX
DSOR:
User:
DEPARTMENT OF THE NAVY Dept. of the Navy
MOE_CD:
DN
MOE_RL:
N9BZ
PICA:
GX
DSOR:
Part Identification
INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
37018
FIIG:
A13100
Concept No.:
App. Key:
AS
Cond. Code:
2
Status:
A
Material and Special Handling
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
Hazmat (HMIC): N
Indicates there is no data in the hmirs and the nsn is in a fsc not generally suspected of containing hazardous materials.
Precious Metals (PMIC): A
Item does not contain precious metal.
Criticality (CRITL): X
The item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application.
Packaging and Dimensions
Package Size
Package Weight
Part Weight
Part Dimensions (approx.)
Pack Size:
--
Pack Weight:
3.3000lbs
Item Weight:
--
Item Dim:
--
Container
OPI
SPI No.
SPI Rev.
Container:
00
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg.
LVL A
LVL B
LVL C
SPC Mkg.:
00
LVL A:
Z
LVL B:
LVL C:
CUSH
MOP
CATEG.
PRESS MAT
CUSH:
XX
MOP:
ZZ
CATEG.:
37ZZ
PRESS MAT:
XX
WRAP MAT
ICQ
THK
TOS
UCL
WRAP MAT:
XX
ICQ:
000
THK:
X
TOS:
UCL:
Packaging Code Definitions
LVL A Code (LVL_A):Z
Special requirement. see specific instructions or drawings provided.
LVL B Code (LVL_B):
Procedure Indicator Code (OPI): M
All packaging data is mandatory for compliance and no substitutions are permitted. fast packs should be included in this category.
Special Markings Code (SPC MKG): 00
No special marking.
Method of Preservation (MOP): ZZ
See j.4.1.B.
Cushion Material (CUSH): XX
Preservation Material (PRESS MAT): XX