L3010212 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

L3010212: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_length: 31.680 INCHES NOMINAL IN, aircraft_location: UPPER, AIRCRAFT, AVIONICS DOOR, end_item_identification: B1-B AIRCRAFT, side_for_which_designed: LEFT SIDE, aircraft_mission_design_series: B1 AIRCRAFT. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-706-6354, 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

L3010212

NSN: 1560-01-706-6354
NIINs: 017066354, 017066360, 017082106, 017082110, 017082406, 017082545, 017082576, 017082580, 017082613, 017082880, 017082914, 017082924, 017083465, 017083521, 017148727
FSC: 1560 — Airframe Structural Components
CAGE: 43999 — THE BOEING COMPANY DIV LEGACY AM&M (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 2024
overall_length	31.680 INCHES NOMINAL IN
aircraft_location	UPPER, AIRCRAFT, AVIONICS DOOR
end_item_identification	B1-B AIRCRAFT
side_for_which_designed	LEFT SIDE
aircraft_mission_design_series	B1 AIRCRAFT
criticality_code_justification	FEAT
relationship_to_similar_equipment	OPPOSITE OF -102
material_document_and_classification	MIL-T-9046 FED SPEC SINGLE MATERIAL RESPONSE OR AMS4901-T FED SPEC SINGLE MATERIAL RESPONSE
part_name_assigned_by_controlling_agency	RETAINER
NSN	1560-01-706-6354

COMPONENT DIAGRAM

KEY FEATURES

•

RELATIONSHIP TO SIMILAR EQUIPMENT: OPPOSITE OF -102

•

CRITICALITY CODE JUSTIFICATION: FEAT

•

MATERIAL DOCUMENT AND CLASSIFICATION: MIL-T-9046 MIL SPEC SINGLE MATERIAL RESPONSE

•

AIRCRAFT LOCATION: AIRFRAME UPPER,AFT, AVIONICS COMPARTMENT

•

MATERIAL: ALUMINUM ALLOY 2024 AND TITANIUM

TECHNICAL CHARACTERISTICS

RELATIONSHIP TO SIMILAR EQUIPMENT	OPPOSITE OF -102
CRITICALITY CODE JUSTIFICATION	FEAT
MATERIAL DOCUMENT AND CLASSIFICATION	MIL-T-9046 MIL SPEC SINGLE MATERIAL RESPONSE
SPECIAL FEATURES	HARDNESS CRITICAL ITEM
AIRCRAFT LOCATION	AIRFRAME UPPER,AFT, AVIONICS COMPARTMENT
PART NAME ASSIGNED BY CONTROLLING AGENCY	RETAINER
END ITEM IDENTIFICATION	B1-B AIRCRAFT
MATERIAL	ALUMINUM ALLOY 2024 AND TITANIUM
SIDE FOR WHICH DESIGNED	LEFT SIDE
AIRCRAFT MISSION DESIGN SERIES	B1 AIRCRAFT

SUBSTITUTES & CROSS-REFERENCES 1

PL3010212Reference 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 L3010212?

L3010212 is a PLATE,STRUCTURAL,AIRCRAFT.

What parts can replace L3010212?

There is 1 known substitute for L3010212: PL3010212. Substitute compatibility should be verified for your specific system.

What is the NSN for L3010212?

L3010212 is cataloged in the U.S. Government catalog under NSN 1560-01-706-6354. This indicates validated use in U.S. government and defense supply chains.

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L3010212 — PLATE,STRUCTURAL,AIRCRAFT

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