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Technical Data Sheet

74A328408-2053 — Technical Data Sheet

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WHAT YOU NEED TO KNOW
Verify manufacturer and server generation compatibility Check if Option PN or Spare PN — same part, different channel
Confirm exact part number — similar PNs may be different parts
PRODUCT OVERVIEW

WEB,STRUCTURAL COMPONENT,AIRCRAF. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 12.000 INCHES NOMINAL IN, overall_length: 19.000 INCHES NOMINAL IN, special_features: ITEM KNOWN AS:DP WEB-ANTI-CHAFE CONOTESN;TEMPER T76;, aircraft_location: FUEL FLOOR,OUTBOARD Y453.000 TO Y555.500, material_thickness: 0.090 INCHES NOMINAL IN. This product is currently in active production with full OEM support.

This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 1560-01-696-9674, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.

Verify compatibility with your specific system configuration before ordering.

WHERE IT FITS
74A328408-2053
NSN: 1560-01-696-9674
FSC: 1560
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)
SPECIFICATIONS
materialALUMINUM ALLOY 7075
overall_width12.000 INCHES NOMINAL IN
overall_length19.000 INCHES NOMINAL IN
special_featuresITEM KNOWN AS:DP WEB-ANTI-CHAFE CONOTESN;TEMPER T76;
aircraft_locationFUEL FLOOR,OUTBOARD Y453.000 TO Y555.500
material_thickness0.090 INCHES NOMINAL IN
end_item_identificationF/A-18E/F AIRCRAFT
aircraft_mission_design_seriesF/A-18E/F AIRCRAFT
material_document_and_classificationQQ-A-250/12 FLAT STR ASSN STD SINGLE MATERIAL RESPONSE
part_name_assigned_by_controlling_agencyPANEL,FUEL FLOOR
NSN1560-01-696-9674
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available WEB,STRUCTURAL COMPONENT,AIRCRAF TITLE COMPONENT PN 74A328408-2053 MFR WEB,STRUCTURAL COMPONE
KEY FEATURES
MATERIAL THICKNESS: 0.090 INCHES NOMINAL IN
AIRCRAFT LOCATION: FUEL FLOOR,OUTBOARD Y453.000 TO Y555.500
AIRCRAFT MISSION DESIGN SERIES: F/A-18E/F AIRCRAFT
MATERIAL: ALUMINUM ALLOY 7075
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/12 FLAT STR ASSN STD SINGLE MATERIAL RESPONSE
TECHNICAL CHARACTERISTICS (FLIS)
MATERIAL THICKNESS0.090 INCHES NOMINAL IN
AIRCRAFT LOCATIONFUEL FLOOR,OUTBOARD Y453.000 TO Y555.500
OVERALL LENGTH19.000 INCHES NOMINAL IN
AIRCRAFT MISSION DESIGN SERIESF/A-18E/F AIRCRAFT
PART NAME ASSIGNED BY CONTROLLING AGENCYPANEL,FUEL FLOOR
MATERIALALUMINUM ALLOY 7075
END ITEM IDENTIFICATIONF/A-18E/F AIRCRAFT
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250/12 FLAT STR ASSN STD SINGLE MATERIAL RESPONSE
OVERALL WIDTH12.000 INCHES NOMINAL IN
SPECIAL FEATURESITEM KNOWN AS:DP WEB-ANTI-CHAFE CONOTESN;TEMPER T76;
VERIFIED SUBSTITUTES & CROSS-REFERENCES 6
74A328408-2058Interchangeable
interchangeable cross-reference
interchangeable
74A328408Interchangeable
interchangeable cross-reference
interchangeable
74A328408-2059Interchangeable
interchangeable cross-reference
interchangeable
74A328408-2057Interchangeable
interchangeable cross-reference
interchangeable
74A328408-2055Interchangeable
interchangeable cross-reference
interchangeable
74A328408-2060Interchangeable
interchangeable cross-reference
interchangeable
LIFECYCLE
StatusACTIVE
AvailabilityOEM and secondary market
RoHS CompliantEAR99Not HAZMAT
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FREQUENTLY ASKED QUESTIONS
What is 74A328408-2053?
74A328408-2053 is a WEB,STRUCTURAL COMPONENT,AIRCRAF.
What parts can replace 74A328408-2053?
There are 6 known substitutes for 74A328408-2053: 74A328408-2058, 74A328408, 74A328408-2059 and 3 more. Substitute compatibility should be verified for your specific system.
What is the NSN for 74A328408-2053?
74A328408-2053 is cataloged in the Federal Logistics Information System (FLIS) under NSN 1560-01-696-9674. This indicates validated use in U.S. government and defense supply chains.
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