L3022017-049 — SUPPORT,STRUCTURAL COMPONENT,AIR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

L3022017-049: SUPPORT,STRUCTURAL COMPONENT,AIR.

SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 1.30 INCHES NOMINAL IN, overall_length: 6.20 INCHES NOMINAL IN, aircraft_location: UPPER, FUSELAGE, material_thickness: 0.050 INCHES NOMINAL IN, aircraft_station_number: YF542.00TO YF932.00. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-717-1018, 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

L3022017-049

NSN: 1560-01-717-1018
FSC: 1560 — Airframe Structural Components
CAGE: 43999 — THE BOEING COMPANY DIV LEGACY AM&M (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 2024
overall_width	1.30 INCHES NOMINAL IN
overall_length	6.20 INCHES NOMINAL IN
special_features	THIS DRAWING CONTAINS HARDNESS CRITICAL ITEMS OR HARDNESS CRITICAL PROCESS. ALL CHANGES TO ITEMS OR PROCESS ANNOTATED ON THE DRAWING OR PARTS LIST MUST BE EVALUATED FOR HARDNESS IMPACT
aircraft_location	UPPER, FUSELAGE
material_thickness	0.050 INCHES NOMINAL IN
aircraft_station_number	YF542.00TO YF932.00
end_item_identification	B1-B AIRCRAFT
aircraft_mission_design_series	B1-B
criticality_code_justification	FEAT
material_document_and_classification	QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE
part_name_assigned_by_controlling_agency	FILLER
NSN	1560-01-717-1018

COMPONENT DIAGRAM

KEY FEATURES

•

AIRCRAFT STATION NUMBER: YF542.00TO YF932.00

•

CRITICALITY CODE JUSTIFICATION: FEAT

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.050 INCHES NOMINAL IN

•

AIRCRAFT LOCATION: UPPER, FUSELAGE

TECHNICAL CHARACTERISTICS

AIRCRAFT STATION NUMBER	YF542.00TO YF932.00
CRITICALITY CODE JUSTIFICATION	FEAT
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	6.20 INCHES NOMINAL IN
OVERALL WIDTH	1.30 INCHES NOMINAL IN
MATERIAL THICKNESS	0.050 INCHES NOMINAL IN
SPECIAL FEATURES	THIS DRAWING CONTAINS HARDNESS CRITICAL ITEMS OR HARDNESS CRITICAL PROCESS. ALL CHANGES TO ITEMS OR PROCESS ANNOTATED ON THE DRAWING OR PARTS LIST MUST BE EVALUATED FOR HARDNESS IMPACT
AIRCRAFT LOCATION	UPPER, FUSELAGE
PART NAME ASSIGNED BY CONTROLLING AGENCY	FILLER
END ITEM IDENTIFICATION	B1-B AIRCRAFT

SUBSTITUTES & CROSS-REFERENCES 2

PLL3022017Reference document

Same NSN cross-reference

Reference document — Drawing number reference only

L3022017Reference 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 L3022017-049?

L3022017-049 is a SUPPORT,STRUCTURAL COMPONENT,AIR.

What parts can replace L3022017-049?

There are 2 known substitutes for L3022017-049: PLL3022017, L3022017. Substitute compatibility should be verified for your specific system.

What is the NSN for L3022017-049?

L3022017-049 is cataloged in the U.S. Government catalog under NSN 1560-01-717-1018. This indicates validated use in U.S. government and defense supply chains.

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L3022017-049 — SUPPORT,STRUCTURAL COMPONENT,AIR

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