4080358 — LINER,COMBUSTION CHAMBER,AIRCRAF

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4080358: LINER,COMBUSTION CHAMBER,AIRCRAF.

LINER,COMBUSTION CHAMBER,AIRCRAF. Key specifications include material: NICKEL ALLOY OVERALL, overall_width: 1.514 INCHES NOMINAL IN, overall_length: 6.281 INCHES MINIMUM AND 6.393 INCHES MAXIMUM IN, special_features: THERMAL BARRIER COATING ADDED PER ECN 95QA006, end_item_identification: F100-PW-229 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMBUSTION CHAMBER. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-421-9741, 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

4080358

NSN: 2840-01-421-9741
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 52661 — RTX CORPORATION DIV PRATT & WHITNEY (USA)

SPECIFICATIONS

material	NICKEL ALLOY OVERALL
overall_width	1.514 INCHES NOMINAL IN
overall_length	6.281 INCHES MINIMUM AND 6.393 INCHES MAXIMUM IN
special_features	THERMAL BARRIER COATING ADDED PER ECN 95QA006
end_item_identification	F100-PW-229 AIRCRAFT GAS TURBINE ENGINE
engine_section_location	COMBUSTION CHAMBER
criticality_code_justification	STDC AND CZBJ AND ABHP AND ABMK AND FEAT
material_document_and_classification	PWA1475 MFR REF SINGLE MATERIAL RESPONSE OVERALL
part_name_assigned_by_controlling_agency	LINER SEGMENT,COMBUSTION CHAMBER DUCT, 3 OD
surface_treatment_document_and_classification	SPEC PWA 265-1 MFR REF SINGLE TREATMENT RESPONSE OVERALL
NSN	2840-01-421-9741

COMPONENT DIAGRAM

KEY FEATURES

•

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION: SPEC PWA 265-1 MFR REF SINGLE TREATMENT RESPONSE OVERALL

•

CRITICALITY CODE JUSTIFICATION: STDC AND CZBJ AND ABHP AND ABMK AND FEAT

•

MATERIAL DOCUMENT AND CLASSIFICATION: PWA1475 MFR REF SINGLE MATERIAL RESPONSE OVERALL

•

ENGINE SECTION LOCATION: COMBUSTION CHAMBER

TECHNICAL CHARACTERISTICS

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	SPEC PWA 265-1 MFR REF SINGLE TREATMENT RESPONSE OVERALL
CRITICALITY CODE JUSTIFICATION	STDC AND CZBJ AND ABHP AND ABMK AND FEAT
MATERIAL DOCUMENT AND CLASSIFICATION	PWA1475 MFR REF SINGLE MATERIAL RESPONSE OVERALL
OVERALL LENGTH	6.281 INCHES MINIMUM AND 6.393 INCHES MAXIMUM IN
OVERALL WIDTH	1.514 INCHES NOMINAL IN
ENGINE SECTION LOCATION	COMBUSTION CHAMBER
SPECIAL FEATURES	THERMAL BARRIER COATING ADDED PER ECN 95QA006
PART NAME ASSIGNED BY CONTROLLING AGENCY	LINER SEGMENT,COMBUSTION CHAMBER DUCT, 3 OD
END ITEM IDENTIFICATION	F100-PW-229 AIRCRAFT GAS TURBINE ENGINE
MATERIAL	NICKEL ALLOY OVERALL

SUBSTITUTES & CROSS-REFERENCES 2

4083063Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

2840PL0712480Reference document

Same NSN cross-reference

Reference document — Informative reference only

LIFECYCLE

NSN statusCancelled· U.S. Government catalog

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 4080358?

4080358 is a LINER,COMBUSTION CHAMBER,AIRCRAF.

What parts can replace 4080358?

There are 2 known substitutes for 4080358: 4083063, 2840PL0712480. Substitute compatibility should be verified for your specific system.

What is the NSN for 4080358?

4080358 is cataloged in the U.S. Government catalog under NSN 2840-01-421-9741. This indicates validated use in U.S. government and defense supply chains.

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4080358 — LINER,COMBUSTION CHAMBER,AIRCRAF

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