L3022206-004 — SUPPORT,STRUCTURAL COMPONENT,AIR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

L3022206-004: SUPPORT,STRUCTURAL COMPONENT,AIR.

SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 5.400 INCHES NOMINAL IN, overall_length: 11.200 INCHES NOMINAL IN, special_features: FINISH:11AB;HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER NEGATIVE T62;NHA L3022045 USED ON B1-B AIRCRAFT;, aircraft_location: GUSSET,UPPER FUSELAGE, material_thickness: 0.080 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-702-6760, 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

L3022206-004

NSN: 1560-01-702-6760
FSC: 1560 — Airframe Structural Components
CAGE: 43999 — THE BOEING COMPANY DIV LEGACY AM&M (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 2024
overall_width	5.400 INCHES NOMINAL IN
overall_length	11.200 INCHES NOMINAL IN
special_features	FINISH:11AB;HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER NEGATIVE T62;NHA L3022045 USED ON B1-B AIRCRAFT;
aircraft_location	GUSSET,UPPER FUSELAGE
material_thickness	0.080 INCHES NOMINAL IN
aircraft_station_number	YF 832.50
end_item_identification	B1-B AIRCRAFT
aircraft_mission_design_series	B1-B AIRCRAFT
material_document_and_classification	QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE
part_name_assigned_by_controlling_agency	GUSSET
NSN	1560-01-702-6760

COMPONENT DIAGRAM

KEY FEATURES

•

AIRCRAFT STATION NUMBER: YF 832.50

•

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

•

MATERIAL THICKNESS: 0.080 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: GUSSET,UPPER FUSELAGE

TECHNICAL CHARACTERISTICS

AIRCRAFT STATION NUMBER	YF 832.50
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	11.200 INCHES NOMINAL IN
OVERALL WIDTH	5.400 INCHES NOMINAL IN
MATERIAL THICKNESS	0.080 INCHES NOMINAL IN
SPECIAL FEATURES	FINISH:11AB;HEAT TREAT ALUMINUM ALLOY PER ST0111LA0009 TO TEMPER NEGATIVE T62;NHA L3022045 USED ON B1-B AIRCRAFT;
AIRCRAFT LOCATION	GUSSET,UPPER FUSELAGE
PART NAME ASSIGNED BY CONTROLLING AGENCY	GUSSET
END ITEM IDENTIFICATION	B1-B AIRCRAFT
MATERIAL	ALUMINUM ALLOY 2024

SUBSTITUTES & CROSS-REFERENCES 1

L3022206Reference 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 L3022206-004?

L3022206-004 is a SUPPORT,STRUCTURAL COMPONENT,AIR.

What parts can replace L3022206-004?

There is 1 known substitute for L3022206-004: L3022206. Substitute compatibility should be verified for your specific system.

What is the NSN for L3022206-004?

L3022206-004 is cataloged in the U.S. Government catalog under NSN 1560-01-702-6760. This indicates validated use in U.S. government and defense supply chains.

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L3022206-004 — SUPPORT,STRUCTURAL COMPONENT,AIR

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