4084071-01 — LINER,COMBUSTION CHAMBER,AIRCRAF

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4084071-01: LINER,COMBUSTION CHAMBER,AIRCRAF.

LINER,COMBUSTION CHAMBER,AIRCRAF. Key specifications include diameter: 33.935 INCHES NOMINAL IN, material: COBALT ALLOY OVERALL, overall_length: 9.660 INCHES MINIMUM AND 9.700 INCHES MAXIMUM IN, hardness_rating: 36.0 ROCKWELL C NOMINAL OVERALL, 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 2840-01-449-1573, 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

4084071-01

NSN: 2840-01-449-1573
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)

SPECIFICATIONS

diameter	33.935 INCHES NOMINAL IN
material	COBALT ALLOY OVERALL
overall_length	9.660 INCHES MINIMUM AND 9.700 INCHES MAXIMUM IN
hardness_rating	36.0 ROCKWELL C NOMINAL OVERALL
special_features	T.O. 2J-F100-54, FIG 65, IND 25; SERVICE REPAIR FOR P/NS 4079666-01, 4080412-01, 4081214-01, 4083169-01, 4083180-01, 4083181-01 AND 4083182-01
end_item_identification	F100-PW-229 AIRCRAFT GAS TURBINE ENGINE
engine_section_location	COMBUSTION CHAMBER
material_document_and_classification	PWA1042 MFR REF SINGLE MATERIAL RESPONSE OVERALL
part_name_assigned_by_controlling_agency	ORIGINAL NAME LINER,AUGMENTOR COMBUSTION CHAMBER ASSY
NSN	2840-01-449-1573

COMPONENT DIAGRAM

KEY FEATURES

•

HARDNESS RATING: 36.0 ROCKWELL C NOMINAL OVERALL

•

MATERIAL DOCUMENT AND CLASSIFICATION: PWA1042 MFR REF SINGLE MATERIAL RESPONSE OVERALL

•

DIAMETER: 33.935 INCHES NOMINAL IN

•

ENGINE SECTION LOCATION: COMBUSTION CHAMBER

TECHNICAL CHARACTERISTICS

HARDNESS RATING	36.0 ROCKWELL C NOMINAL OVERALL
MATERIAL DOCUMENT AND CLASSIFICATION	PWA1042 MFR REF SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	33.935 INCHES NOMINAL IN
OVERALL LENGTH	9.660 INCHES MINIMUM AND 9.700 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMBUSTION CHAMBER
SPECIAL FEATURES	T.O. 2J-F100-54, FIG 65, IND 25; SERVICE REPAIR FOR P/NS 4079666-01, 4080412-01, 4081214-01, 4083169-01, 4083180-01, 4083181-01 AND 4083182-01
PART NAME ASSIGNED BY CONTROLLING AGENCY	ORIGINAL NAME LINER,AUGMENTOR COMBUSTION CHAMBER ASSY
END ITEM IDENTIFICATION	F100-PW-229 AIRCRAFT GAS TURBINE ENGINE
MATERIAL	COBALT 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 2

2840PL1818120Reference document

Same NSN cross-reference

Reference document — Informative reference only

4084071Reference document

Same NSN cross-reference

Reference document — Drawing number reference only

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 4084071-01?

4084071-01 is a LINER,COMBUSTION CHAMBER,AIRCRAF.

What parts can replace 4084071-01?

There are 2 known substitutes for 4084071-01: 2840PL1818120, 4084071. Substitute compatibility should be verified for your specific system.

What is the NSN for 4084071-01?

4084071-01 is cataloged in the U.S. Government catalog under NSN 2840-01-449-1573. This indicates validated use in U.S. government and defense supply chains.

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4084071-01 — LINER,COMBUSTION CHAMBER,AIRCRAF

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