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L3002139 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

L3002139: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 5.50 INCHES NOMINAL IN, overall_length: 2.12 INCHES NOMINAL IN, special_features: NHA L3002101 AND L3022017;HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T62;, style_designator: SQUARE, aircraft_location: SAFETY HARNESS,ATTACHMENT FUSELAGE. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-717-7526, 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
L3002139
NSN: 1560-01-717-7526
NIINs: 017177526, 017181880, 017182249, 017186267, 017222679
FSC: 1560 — Airframe Structural Components
CAGE: 43999 — THE BOEING COMPANY DIV LEGACY AM&M (USA)
SPECIFICATIONS
materialALUMINUM ALLOY 2024
overall_width5.50 INCHES NOMINAL IN
overall_length2.12 INCHES NOMINAL IN
special_featuresNHA L3002101 AND L3022017;HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T62;
style_designatorSQUARE
aircraft_locationSAFETY HARNESS,ATTACHMENT FUSELAGE
overall_thickness0.020 INCHES NOMINAL IN
material_thickness0.063 INCHES NOMINAL IN
aircraft_station_numberYF655.50, YF740.00, YF823.50, YF906.50
end_item_identificationB1-BACFT
aircraft_mission_design_seriesB1-B AIRCRAFT
material_document_and_classificationQQ-A-750/5 FED SPEC SINGLE MATERIAL RESPONSE
NSN1560-01-717-7526
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available PLATE,STRUCTURAL,AIRCRAFT TITLE COMPONENT PN L3002139 MFR PLATE,STRUCTURAL,AIRCR
KEY FEATURES
•
AIRCRAFT STATION NUMBER: YF655.50, YF740.00, YF823.50, YF906.50
•
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-750/5 FED SPEC SINGLE MATERIAL RESPONSE
•
MATERIAL THICKNESS: 0.063 INCHES NOMINAL IN
•
AIRCRAFT LOCATION: SAFETY HARNESS,ATTACHMENT FUSELAGE
TECHNICAL CHARACTERISTICS
AIRCRAFT STATION NUMBERYF655.50, YF740.00, YF823.50, YF906.50
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-750/5 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH11.60 INCHES NOMINAL IN
OVERALL WIDTH5.50 INCHES NOMINAL IN
MATERIAL THICKNESS0.063 INCHES NOMINAL IN
AIRCRAFT LOCATIONSAFETY HARNESS,ATTACHMENT FUSELAGE
PART NAME ASSIGNED BY CONTROLLING AGENCYDOUBLER, SAFETY HARNESS,ATTACHMENT
END ITEM IDENTIFICATIONB1-B AIRCRAFT
MATERIALALUMINUM ALLOY 2024
AIRCRAFT MISSION DESIGN SERIESB1-B AIRCRAFT
SUBSTITUTES & CROSS-REFERENCES 1
PLL3002139Reference 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 demandNo demilitarization required
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FREQUENTLY ASKED QUESTIONS
What is L3002139?
L3002139 is a PLATE,STRUCTURAL,AIRCRAFT.
What parts can replace L3002139?
There is 1 known substitute for L3002139: PLL3002139. Substitute compatibility should be verified for your specific system.
What is the NSN for L3002139?
L3002139 is cataloged in the U.S. Government catalog under NSN 1560-01-717-7526. This indicates validated use in U.S. government and defense supply chains.
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