4073476-01 — DUCT,EXHAUST,AIRCRAFT GAS TURBIN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4073476-01: DUCT,EXHAUST,AIRCRAFT GAS TURBIN.

DUCT,EXHAUST,AIRCRAFT GAS TURBIN. Key specifications include diameter: 39.374 INCHES MINIMUM AND 39.394 INCHES MAXIMUM IN, material: TITANIUM ALLOY DUCT, overall_length: 7.300 INCHES MINIMUM AND 7.320 INCHES MAXIMUM IN, special_features: AUGMENTOR,COMBUSTION CHAMBER,REAR, end_item_identification: F100PW0229 ENG/AUG MOD, engine_section_location: COMBUSTION CHAMBER. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-319-8757, 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

4073476-01

NSN: 2840-01-319-8757
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	39.374 INCHES MINIMUM AND 39.394 INCHES MAXIMUM IN
material	TITANIUM ALLOY DUCT
overall_length	7.300 INCHES MINIMUM AND 7.320 INCHES MAXIMUM IN
special_features	AUGMENTOR,COMBUSTION CHAMBER,REAR
end_item_identification	F100PW0229 ENG/AUG MOD
engine_section_location	COMBUSTION CHAMBER
criticality_code_justification	AGAV
material_document_and_classification	AMS4911 ASSN STD SINGLE MATERIAL RESPONSE DUCT
NSN	2840-01-319-8757

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS4911 ASSN STD SINGLE MATERIAL RESPONSE DUCT

•

DIAMETER: 39.374 INCHES MINIMUM AND 39.394 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: COMBUSTION CHAMBER

•

MATERIAL: TITANIUM ALLOY DUCT

TECHNICAL CHARACTERISTICS

CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS4911 ASSN STD SINGLE MATERIAL RESPONSE DUCT
DIAMETER	39.374 INCHES MINIMUM AND 39.394 INCHES MAXIMUM IN
OVERALL LENGTH	7.300 INCHES MINIMUM AND 7.320 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMBUSTION CHAMBER
SPECIAL FEATURES	AUGMENTOR,COMBUSTION CHAMBER,REAR
END ITEM IDENTIFICATION	F100PW0229 ENG/AUG MOD
MATERIAL	TITANIUM ALLOY DUCT

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

No substitute or cross-reference records for this part.

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 4073476-01?

4073476-01 is a DUCT,EXHAUST,AIRCRAFT GAS TURBIN.

What is the NSN for 4073476-01?

4073476-01 is cataloged in the U.S. Government catalog under NSN 2840-01-319-8757. This indicates validated use in U.S. government and defense supply chains.

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4073476-01 — DUCT,EXHAUST,AIRCRAFT GAS TURBIN

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