NSN 9540-00-119-2133

Structural Beam

FSC: 9540     NIIN: 001192133
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Product Characteristics

NSN:
9540001192133
Demilitarization:
NO
INC:
37018
Shelf Life:
N/A
Fabrication Method:
Extruded
Overall Height:
1.000 inches
Length:
Between 10.000 feet and 12.000 feet
Left Side Top Flange Thickness:
0.094 inches
Right Side Top Flange Thickness:
0.094 inches
Basic Shape Style:
T shape
First Tip Radius:
0.094 inches
Leg Thickness:
0.094 inches
Left Side Top Flange Distance To Center Of Both Flanges:
0.938 inches
Right Side Top Flange Distance To Center Of Both Flanges:
0.938 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:
1.876 inches
Weight Per Unit Measure:
0.320 pounds per linear foot
First Tip Style:
Lower radius
Third Tip Radius:
0.094 inches
Second Tip Relationship To First Tip:
Identical
Third Tip Relationship To Preceding Tips:
Not identical
Third Tip Style:
Full radius
Right Top Inside Angle:
90.0 degrees
Left Top 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 and temper t3511

Part Numbers

  • AMS-QQ-A-200/3
    SOCIETY OF AUTOMOTIVE ENGINEERS INC
  • AND10136-1702
    AIRFORCE-NAVY AERONAUTICAL DESIGN
  • ASTM B221
    AMERICAN SOCIETY FOR TESTING AND
  • QQA200-3
    FEDERAL SPECIFICATIONS
  • S318
    CESSNA AIRCRAFT COMPANY

Shipping & Handling

HMIRS:

No MSDS. No hazardous material.

ESD:

No known electrostatic discharge.

Professional Distribution

  •   ITAR Registered
  •   DDTC Registered
  •   HAZMAT Certified
  •   AS9120 Quality Standards
  •   100% Quality Inspections
ITAR registered supplier

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Cage Codes
SOCIETY OF AUTOMOTIVE ENGINEERS INC - 81343
AIRFORCE-NAVY AERONAUTICAL DESIGN - 99237
AMERICAN SOCIETY FOR TESTING AND - 81346
FEDERAL SPECIFICATIONS - 81348
CESSNA AIRCRAFT COMPANY - 71379