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L3022078-060 — Technical Data Sheet

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— · COMPONENT
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

SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 1.800 INCHES NOMINAL IN, overall_length: 3.350 INCHES NOMINAL IN, special_features: HEAT TREAT ALUMINUM ALLOYS PER ST0111LA0009 TO TEMPER T76;, aircraft_location: FRAME SIDE,FUSELAGE, material_thickness: 0.080 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 1560-01-706-2467, 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
L3022078-060
NSN: 1560-01-706-2467
FSC: 1560
CAGE: 43999 — THE BOEING COMPANY DIV LEGACY AM&M (USA)
SPECIFICATIONS
materialALUMINUM ALLOY 7075
overall_width1.800 INCHES NOMINAL IN
overall_length3.350 INCHES NOMINAL IN
special_featuresHEAT TREAT ALUMINUM ALLOYS PER ST0111LA0009 TO TEMPER T76;
aircraft_locationFRAME SIDE,FUSELAGE
material_thickness0.080 INCHES NOMINAL IN
aircraft_station_numberYF853.500
end_item_identificationB1-B AIRCRAFT
aircraft_mission_design_seriesB1-B AIRCRAFT
part_name_assigned_by_controlling_agencyGUSSET
NSN1560-01-706-2467
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available SUPPORT,STRUCTURAL COMPONENT,AIR TITLE COMPONENT PN L3022078-060 MFR SUPPORT,STRUCTURAL COM
KEY FEATURES
•
MATERIAL: ALUMINUM ALLOY 7075
•
AIRCRAFT LOCATION: FRAME SIDE,FUSELAGE
•
AIRCRAFT STATION NUMBER: YF853.500
•
AIRCRAFT MISSION DESIGN SERIES: B1-B AIRCRAFT
TECHNICAL CHARACTERISTICS (FLIS)
SPECIAL FEATURESHEAT TREAT ALUMINUM ALLOYS PER ST0111LA0009 TO TEMPER T76;
MATERIALALUMINUM ALLOY 7075
AIRCRAFT LOCATIONFRAME SIDE,FUSELAGE
OVERALL LENGTH3.350 INCHES NOMINAL IN
OVERALL WIDTH1.800 INCHES NOMINAL IN
END ITEM IDENTIFICATIONB1-B AIRCRAFT
AIRCRAFT STATION NUMBERYF853.500
AIRCRAFT MISSION DESIGN SERIESB1-B AIRCRAFT
MATERIAL THICKNESS0.080 INCHES NOMINAL IN
PART NAME ASSIGNED BY CONTROLLING AGENCYGUSSET
VERIFIED SUBSTITUTES & CROSS-REFERENCES 5
L3022078-005Interchangeable
interchangeable cross-reference
interchangeable
L3022078Interchangeable
interchangeable cross-reference
interchangeable
PLL3022078Interchangeable
interchangeable cross-reference
interchangeable
L3022078-006Interchangeable
interchangeable cross-reference
interchangeable
L3022078-059Interchangeable
interchangeable cross-reference
interchangeable
LIFECYCLE
StatusACTIVE
AvailabilityOEM and secondary market
RoHS CompliantEAR99Not HAZMAT
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FREQUENTLY ASKED QUESTIONS
What is L3022078-060?
L3022078-060 is a SUPPORT,STRUCTURAL COMPONENT,AIR.
What parts can replace L3022078-060?
There are 5 known substitutes for L3022078-060: L3022078-005, L3022078, PLL3022078 and 2 more. Substitute compatibility should be verified for your specific system.
What is the NSN for L3022078-060?
L3022078-060 is cataloged in the Federal Logistics Information System (FLIS) under NSN 1560-01-706-2467. This indicates validated use in U.S. government and defense supply chains.
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Last verified: August 2026