2840PL0712526 — LINER,COMBUSTION CHAMBER,AIRCRAF

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

2840PL0712526: LINER,COMBUSTION CHAMBER,AIRCRAF.

LINER,COMBUSTION CHAMBER,AIRCRAF. Key specifications include material: NICKEL ALLOY OVERALL, overall_width: 1.456 INCHES NOMINAL IN, overall_length: 6.157 INCHES MINIMUM AND 6.269 INCHES MAXIMUM IN, end_item_identification: F100-PW-229 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMBUSTION CHAMBER, criticality_code_justification: ABHP AND ABMK AND FEAT. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-448-7036, 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

2840PL0712526

NSN: 2840-01-448-7036
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 9009H — JEDNOLITY INDEKS MATERIALOWY - UNIFORM MATERIAL INDEX (POL)

SPECIFICATIONS

material	NICKEL ALLOY OVERALL
overall_width	1.456 INCHES NOMINAL IN
overall_length	6.157 INCHES MINIMUM AND 6.269 INCHES MAXIMUM IN
special_features	T.O. 2J-F100-54, FIG 100, IND 21; USE ONLY ON P/N 4084089 AND 4083194; 96QA074 IMPROVED DURABLILITY LINER SEGMENT THRU NORMAL ATTRITION OF PARTS
end_item_identification	F100-PW-229 AIRCRAFT GAS TURBINE ENGINE
engine_section_location	COMBUSTION CHAMBER
criticality_code_justification	ABHP AND ABMK AND FEAT
material_document_and_classification	PWA1475 MFR REF SINGLE MATERIAL RESPONSE OVERALL
part_name_assigned_by_controlling_agency	ORIGINAL NAME LINER SEGMENT,COMBUSTION CHAMBER
NSN	2840-01-448-7036

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: ABHP AND ABMK AND FEAT

•

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

•

ENGINE SECTION LOCATION: COMBUSTION CHAMBER

TECHNICAL CHARACTERISTICS

CRITICALITY CODE JUSTIFICATION	ABHP AND ABMK AND FEAT
MATERIAL DOCUMENT AND CLASSIFICATION	PWA1475 MFR REF SINGLE MATERIAL RESPONSE OVERALL
OVERALL LENGTH	6.157 INCHES MINIMUM AND 6.269 INCHES MAXIMUM IN
OVERALL WIDTH	1.456 INCHES NOMINAL IN
ENGINE SECTION LOCATION	COMBUSTION CHAMBER
SPECIAL FEATURES	T.O. 2J-F100-54, FIG 100, IND 21; USE ONLY ON P/N 4084089 AND 4083194; 96QA074 IMPROVED DURABLILITY LINER SEGMENT THRU NORMAL ATTRITION OF PARTS
PART NAME ASSIGNED BY CONTROLLING AGENCY	ORIGINAL NAME LINER SEGMENT,COMBUSTION CHAMBER
END ITEM IDENTIFICATION	F100-PW-229 AIRCRAFT GAS TURBINE ENGINE
MATERIAL	NICKEL ALLOY OVERALL

OTHER ITEMS IN FSC 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components

Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.

2840-00-004-4242 2840-00-021-4702 2840-00-043-0981 2840-00-043-0982 2840-00-048-5261 2840-00-407-9165 2840-01-171-0875

SUBSTITUTES & CROSS-REFERENCES 1

4084087Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Insurance item — stocked against contingency demandDemilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 2840PL0712526?

2840PL0712526 is a LINER,COMBUSTION CHAMBER,AIRCRAF.

What parts can replace 2840PL0712526?

There is 1 known substitute for 2840PL0712526: 4084087. Substitute compatibility should be verified for your specific system.

What is the NSN for 2840PL0712526?

2840PL0712526 is cataloged in the U.S. Government catalog under NSN 2840-01-448-7036. This indicates validated use in U.S. government and defense supply chains.

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2840PL0712526 — LINER,COMBUSTION CHAMBER,AIRCRAF

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