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L3022080-013 — SUPPORT,STRUCTURAL COMPONENT,AIR

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

L3022080-013: SUPPORT,STRUCTURAL COMPONENT,AIR.

SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 2.750 INCHES NOMINAL IN, overall_length: 10.100 INCHES NOMINAL IN, special_features: FINISH:10BA;HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T76;, aircraft_location: FRAME,SIDE,FUSELAGE, material_thickness: 0.050 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-706-1802, 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
L3022080-013
NSN: 1560-01-706-1802
FSC: 1560 — Airframe Structural Components
CAGE: 43999 — THE BOEING COMPANY DIV LEGACY AM&M (USA)
SPECIFICATIONS
materialALUMINUM ALLOY 7075
overall_width2.750 INCHES NOMINAL IN
overall_length10.100 INCHES NOMINAL IN
special_featuresFINISH:10BA;HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T76;
aircraft_locationFRAME,SIDE,FUSELAGE
material_thickness0.050 INCHES NOMINAL IN
aircraft_station_numberYF875.50
end_item_identificationB1-B AIRCRAFT
aircraft_mission_design_seriesB1-B AIRCRAFT
part_name_assigned_by_controlling_agencyZEE
NSN1560-01-706-1802
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available SUPPORT,STRUCTURAL COMPONENT,AIR TITLE COMPONENT PN L3022080-013 MFR SUPPORT,STRUCTURAL COM
KEY FEATURES
•
AIRCRAFT STATION NUMBER: YF875.50
•
MATERIAL THICKNESS: 0.050 INCHES NOMINAL IN
•
AIRCRAFT LOCATION: FRAME,SIDE,FUSELAGE
TECHNICAL CHARACTERISTICS
AIRCRAFT STATION NUMBERYF875.50
OVERALL LENGTH10.100 INCHES NOMINAL IN
OVERALL WIDTH2.750 INCHES NOMINAL IN
MATERIAL THICKNESS0.050 INCHES NOMINAL IN
SPECIAL FEATURESFINISH:10BA;HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T76;
AIRCRAFT LOCATIONFRAME,SIDE,FUSELAGE
PART NAME ASSIGNED BY CONTROLLING AGENCYZEE
END ITEM IDENTIFICATIONB1-B AIRCRAFT
MATERIALALUMINUM ALLOY 7075
AIRCRAFT MISSION DESIGN SERIESB1-B AIRCRAFT
SUBSTITUTES & CROSS-REFERENCES 1
L3022080Reference document
Same NSN cross-reference
Reference document — Drawing number reference only
LIFECYCLE
NSN statusActive· U.S. Government catalog
Acquisition advice: Insurance item — stocked against contingency demandDemilitarization required — mutilation + specific procedure
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FREQUENTLY ASKED QUESTIONS
What is L3022080-013?
L3022080-013 is a SUPPORT,STRUCTURAL COMPONENT,AIR.
What parts can replace L3022080-013?
There is 1 known substitute for L3022080-013: L3022080. Substitute compatibility should be verified for your specific system.
What is the NSN for L3022080-013?
L3022080-013 is cataloged in the U.S. Government catalog under NSN 1560-01-706-1802. This indicates validated use in U.S. government and defense supply chains.
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