L3022017-095 — SUPPORT,STRUCTURAL COMPONENT,AIR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

L3022017-095: SUPPORT,STRUCTURAL COMPONENT,AIR.

SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_length: 13.200 INCHES NOMINAL IN, aircraft_location: PANEL,UPPER FUSELAGE, aircraft_station_number: YF542.00 TO YF932.00, end_item_identification: B1-B AIRCRAFT, aircraft_mission_design_series: B1-B AIRCRAFT. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-718-0198, 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

L3022017-095

NSN: 1560-01-718-0198
FSC: 1560 — Airframe Structural Components
CAGE: 43999 — THE BOEING COMPANY DIV LEGACY AM&M (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 7075
overall_length	13.200 INCHES NOMINAL IN
special_features	THIS DRAWING CONTAINS HARDNESS CRITICAL ITEMS(HCI)OR HARDNESS CRITICAL PROCESSES(HCP)ALL CHANGES TO ITEMS OR PROCESSES ANNOTATED ON THE DRAWING OR PARTS LIST MUST BE EVALUATED FOR HARDNESS IMPACTS;
aircraft_location	PANEL,UPPER FUSELAGE
aircraft_station_number	YF542.00 TO YF932.00
end_item_identification	B1-B AIRCRAFT
aircraft_mission_design_series	B1-B AIRCRAFT
criticality_code_justification	FEAT
material_document_and_classification	QQ-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE
part_name_assigned_by_controlling_agency	TEE
NSN	1560-01-718-0198

COMPONENT DIAGRAM

KEY FEATURES

•

AIRCRAFT STATION NUMBER: YF542.00 TO YF932.00

•

CRITICALITY CODE JUSTIFICATION: FEAT

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE

•

AIRCRAFT LOCATION: PANEL,UPPER FUSELAGE

TECHNICAL CHARACTERISTICS

AIRCRAFT STATION NUMBER	YF542.00 TO YF932.00
CRITICALITY CODE JUSTIFICATION	FEAT
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH	13.200 INCHES NOMINAL IN
SPECIAL FEATURES	THIS DRAWING CONTAINS HARDNESS CRITICAL ITEMS(HCI)OR HARDNESS CRITICAL PROCESSES(HCP)ALL CHANGES TO ITEMS OR PROCESSES ANNOTATED ON THE DRAWING OR PARTS LIST MUST BE EVALUATED FOR HARDNESS IMPACTS;
AIRCRAFT LOCATION	PANEL,UPPER FUSELAGE
PART NAME ASSIGNED BY CONTROLLING AGENCY	TEE
END ITEM IDENTIFICATION	B1-B AIRCRAFT
MATERIAL	ALUMINUM ALLOY 7075
AIRCRAFT MISSION DESIGN SERIES	B1-B AIRCRAFT

SUBSTITUTES & CROSS-REFERENCES 2

L3022017Reference document

Same NSN cross-reference

Reference document — Drawing number reference only

PLL3022017Reference 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

Ready to buy L3022017-095?

Compare prices from verified sellers on eBay

Buy on eBay →

As an eBay Partner, PartsTable may earn a commission. Your price is not affected.

FREQUENTLY ASKED QUESTIONS

What is L3022017-095?

L3022017-095 is a SUPPORT,STRUCTURAL COMPONENT,AIR.

What parts can replace L3022017-095?

There are 2 known substitutes for L3022017-095: L3022017, PLL3022017. Substitute compatibility should be verified for your specific system.

What is the NSN for L3022017-095?

L3022017-095 is cataloged in the U.S. Government catalog under NSN 1560-01-718-0198. This indicates validated use in U.S. government and defense supply chains.

Community Feedback

L3022017-095 — SUPPORT,STRUCTURAL COMPONENT,AIR

Request a Quote — L3022017-095