PartsTable TECHNICAL DATA SHEET
JULY 2026Technical Data Sheet

S1325739SBeam,structural

The Boeing Company · NSN 9540-00-555-3222 · FSC 9540 · No Item Name Available
Verified by PartsTable
NSN 9540-00-555-3222 — this item is cataloged by the U.S. Government under National Stock Number 9540-00-555-3222. Primary manufacturer part number: S1325739S.
Features
  • Beam,structural — FSC 9540
  • Right Top Inside Angle: 90.0 DEGREES NOMINAL
  • Left Top Inside Angle: 90.0 DEGREES NOMINAL
  • Top Flange Width: 4.000 INCHES NOMINAL IN
  • Right Side Top Flange Thickness: 0.094 INCHES NOMINAL IN
  • Fabrication Method: EXTRUDED
  • Fillet Radius Where Top Right Flange Joins Web Flange/leg: 0.094 INCHES NOMINAL IN
  • Material: ALUMINUM ALLOY 7075
Applications
  • Applications requiring Aluminum Alloy 7075 construction
General Description

The Beam,structural, cataloged under National Stock Number 9540-00-555-3222, is classified within Federal Supply Class 9540 (No Item Name Available) of the Metal Bars, Sheets, and Shapes group. The primary manufacturer of record is The Boeing Company. Government technical data includes 21 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 8 commercial cross-references from 6 manufacturers, enabling identification through both NSN and commercial part number lookups. 12 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.

Technical Specifications
ParameterValue
NSN9540-00-555-3222
Primary Part NumberS1325739S
Item NameBeam,structural
FSC / FSG9540 / 95 — No Item Name Available
ManufacturerThe Boeing Company
StatusACTIVE
Right Top Inside Angle90.0 DEGREES NOMINAL
Left Top Inside Angle90.0 DEGREES NOMINAL
Top Flange Width4.000 INCHES NOMINAL IN
Right Side Top Flange Thickness0.094 INCHES NOMINAL IN
Fabrication MethodEXTRUDED
Fillet Radius Where Top Right Flange Joins Web Flange/leg0.094 INCHES NOMINAL IN
MaterialALUMINUM ALLOY 7075
Fillet Radius Where Top Left Flange Joins Web Flange/leg0.094 INCHES NOMINAL IN
Basic Shape StyleT SHAPE
Second Tip Relationship to First TipIDENTICAL
Third Tip Relationship to Preceding TipsIDENTICAL W/FIRST TIP
Leg Thickness0.094 INCHES NOMINAL IN
Material Document and ClassificationAMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE
Nondefinitive Spec/std DataO TEMPER
First Tip StyleSQUARE END
Weight Per Unit Measure0.610 POUNDS PER LINEAR FOOT LBS
Left Side Top Flange Distance to Center of Both Flanges1.688 INCHES NOMINAL IN
Left Side Top Flange Thickness0.094 INCHES NOMINAL IN
Right Side Top Flange Distance to Center of Both Flanges2.312 INCHES NOMINAL IN
Heat TreatmentO-ANNEALED
Length10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT
Lifecycle & Compliance
Acquisition StatusACTIVE
HAZMATNo
Verified Substitutes 12
9540-00-148-4883 INTERCHANGEABLE
Beam,structural
5330-00-409-325460568 INTERCHANGEABLE
Seal,plain Encased
Dana Automotive Systems Group, Llc Dba Dana Sealing Products
2940-00-701-1105 INTERCHANGEABLE
Band Assembly,air Cleaner
3040-00-717-175824989 INTERCHANGEABLE
Gearshaft,spur
Honeywell International, Inc Div Aerospace-Tucson
1730-00-858-9551 INTERCHANGEABLE
Trigger,spray
5330-00-977-9951 INTERCHANGEABLE
Seal,plain Encased
9540-01-085-6800 INTERCHANGEABLE
Beam,structural
5998-01-114-5577 INTERCHANGEABLE
Support,electrical Card Holder
5330-01-128-8225808118 INTERCHANGEABLE
Gasket
Parker-Hannifin Corporation Dba Pneutronics Div Composite Sealing Systems Division
4730-01-307-139624989 INTERCHANGEABLE
Elbow,tube
Smiths Aerospace, Inc., Electronic Systems-Grand Rapids
Cross-Reference Index
Part NumberManufacturer
S1325739S The Boeing Company (USA)
60-568 Transtar Metals Corp (USA)
PA10275 Transtar Metals Corp (USA)
AMS-QQ-A-200/11 Society of Automotive Engineers Inc (USA)
24989 Aluminum Co of America (USA)
AMS-QQ-A-200/11 Sae International Dba Sae International (USA)
S1325739S The Boeing Company (USA)
QQ-A-200/11 Federal Specifications Promulgated by General Services Administration Washington DC (USA)
Related Parts
9540-00-148-4883INTERCHANGEABLE
BEAM,STRUCTURAL
5330-00-409-3254INTERCHANGEABLE
SEAL,PLAIN ENCASED
60568
2940-00-701-1105INTERCHANGEABLE
BAND ASSEMBLY,AIR CLEANER
3040-00-717-1758INTERCHANGEABLE
GEARSHAFT,SPUR
24989
1730-00-858-9551INTERCHANGEABLE
TRIGGER,SPRAY
5330-00-977-9951INTERCHANGEABLE
SEAL,PLAIN ENCASED
9540-01-085-6800INTERCHANGEABLE
BEAM,STRUCTURAL
5998-01-114-5577INTERCHANGEABLE
SUPPORT,ELECTRICAL CARD HOLDER
5330-01-128-8225INTERCHANGEABLE
GASKET
808118
4730-01-307-1396INTERCHANGEABLE
ELBOW,TUBE
24989
5340-01-509-1170INTERCHANGEABLE
STRAP,WEBBING
24989-1
5925-01-565-5783INTERCHANGEABLE
CIRCUIT BREAKER
24989

Frequently Asked Questions

What is NSN 9540-00-555-3222?

NSN 9540-00-555-3222 is a Beam,structural, manufactured by The Boeing Company, classified under FSC 9540 (No Item Name Available). Status: active.

What are the part numbers for NSN 9540-00-555-3222?

NSN 9540-00-555-3222 has 8 cross-referenced part numbers: S1325739S (The Boeing Company), 60-568 (Transtar Metals Corp), PA10275 (Transtar Metals Corp), AMS-QQ-A-200/11 (Society of Automotive Engineers Inc), 24989 (Aluminum Co of America) and 3 more.

What NSN replaces 9540-00-555-3222?

There are 12 known substitutes for 9540-00-555-3222: 9540-00-148-4883, 5330-00-409-3254, 2940-00-701-1105 and 9 more. Verify interchangeability with system specifications before substitution.

What are the specifications of S1325739S?

Key specifications for S1325739S: Right Top Inside Angle: 90.0 DEGREES NOMINAL; Left Top Inside Angle: 90.0 DEGREES NOMINAL; Top Flange Width: 4.000 INCHES NOMINAL IN; Right Side Top Flange Thickness: 0.094 INCHES NOMINAL IN. 22 total characteristics are documented in the Federal Logistics Information System.

Validated with multiple authoritative sources, including Government, OEM, and Certified sources.
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