L3002139-027 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

L3002139-027: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 4.900 INCHES NOMINAL IN, overall_length: 9.600 INCHES NOMINAL IN, special_features: HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T62;NHA L3002101 AND L3022017;, aircraft_location: FUSELAGE, material_thickness: 0.063 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-718-1880, 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

L3002139-027

NSN: 1560-01-718-1880
FSC: 1560 — Airframe Structural Components
CAGE: 43999 — THE BOEING COMPANY DIV LEGACY AM&M (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 2024
overall_width	4.900 INCHES NOMINAL IN
overall_length	9.600 INCHES NOMINAL IN
special_features	HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T62;NHA L3002101 AND L3022017;
aircraft_location	FUSELAGE
material_thickness	0.063 INCHES NOMINAL IN
aircraft_station_number	YF655.50,YF740.00,YF823.50 AND YF906.50
end_item_identification	B1-B AIRCRAFT
aircraft_mission_design_series	B1-B
material_document_and_classification	QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE
part_name_assigned_by_controlling_agency	DOUBLER
NSN	1560-01-718-1880

COMPONENT DIAGRAM

KEY FEATURES

•

AIRCRAFT STATION NUMBER: YF655.50,YF740.00,YF823.50 AND YF906.50

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.063 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: FUSELAGE

TECHNICAL CHARACTERISTICS

AIRCRAFT STATION NUMBER	YF655.50,YF740.00,YF823.50 AND YF906.50
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	9.600 INCHES NOMINAL IN
OVERALL WIDTH	4.900 INCHES NOMINAL IN
MATERIAL THICKNESS	0.063 INCHES NOMINAL IN
SPECIAL FEATURES	HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER T62;NHA L3002101 AND L3022017;
AIRCRAFT LOCATION	FUSELAGE
PART NAME ASSIGNED BY CONTROLLING AGENCY	DOUBLER
END ITEM IDENTIFICATION	B1-B AIRCRAFT
MATERIAL	ALUMINUM ALLOY 2024

SUBSTITUTES & CROSS-REFERENCES 2

L3002139Reference document

Same NSN cross-reference

Reference document — Drawing number reference only

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 demandDemilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is L3002139-027?

L3002139-027 is a PLATE,STRUCTURAL,AIRCRAFT.

What parts can replace L3002139-027?

There are 2 known substitutes for L3002139-027: L3002139, PLL3002139. Substitute compatibility should be verified for your specific system.

What is the NSN for L3002139-027?

L3002139-027 is cataloged in the U.S. Government catalog under NSN 1560-01-718-1880. This indicates validated use in U.S. government and defense supply chains.

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L3002139-027 — PLATE,STRUCTURAL,AIRCRAFT

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