4064666 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4064666: SEAL,AIR,AIRCRAFT GAS TURBINE EN.

SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 13.495 INCHES MINIMUM AND 13.505 INCHES MAXIMUM IN, material: TITANIUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 0.989 INCHES MINIMUM AND 1.349 INCHES MAXIMUM IN, special_features: T.O. 2J-F100-4, FIG 104, IND 3; REOP AND REID OF 4064666; FRONT COMPRESSOR INLET, end_item_identification: ACFT ENG F100.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-184-8573, 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

4064666

NSN: 2840-01-184-8573
NIINs: 011848573, 013298621
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	13.495 INCHES MINIMUM AND 13.505 INCHES MAXIMUM IN
material	TITANIUM ALLOY OVERALL
design_type	AXIAL COMPRESSOR
stage_number	1
overall_length	0.989 INCHES MINIMUM AND 1.349 INCHES MAXIMUM IN
special_features	T.O. 2J-F100-4, FIG 104, IND 3; REOP AND REID OF 4064666; FRONT COMPRESSOR INLET
end_item_identification	ACFT ENG F100
engine_section_location	COMPRESSOR
material_document_and_classification	PWA1216 MFR REF SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-184-8573

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

DESIGN TYPE: AXIAL COMPRESSOR

•

MATERIAL DOCUMENT AND CLASSIFICATION: PWA1216 MFR REF SINGLE MATERIAL RESPONSE OVERALL

•

DIAMETER: 13.495 INCHES MINIMUM AND 13.505 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: COMPRESSOR

TECHNICAL CHARACTERISTICS

STAGE NUMBER	1
DESIGN TYPE	AXIAL COMPRESSOR
MATERIAL DOCUMENT AND CLASSIFICATION	PWA1216 MFR REF SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	13.495 INCHES MINIMUM AND 13.505 INCHES MAXIMUM IN
OVERALL LENGTH	0.989 INCHES MINIMUM AND 1.349 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMPRESSOR
SPECIAL FEATURES	T.O. 2J-F100-4, FIG 104, IND 3; BODY 11.907-11.917 OD; FLANGES 12.093-12.097 OD; HUB 11.780-11.790 OD; BORE 10.468-10.472 OD; FRONT COMPRESSOR INLET; TCTO 2J-F100(I)-512
END ITEM IDENTIFICATION	ACFT ENG F-100
MATERIAL	TITANIUM ALLOY OVERALL

SUBSTITUTES & CROSS-REFERENCES 1

4079076Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

No demilitarization required

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FREQUENTLY ASKED QUESTIONS

What is 4064666?

4064666 is a SEAL,AIR,AIRCRAFT GAS TURBINE EN.

What parts can replace 4064666?

There is 1 known substitute for 4064666: 4079076. Substitute compatibility should be verified for your specific system.

What is the NSN for 4064666?

4064666 is cataloged in the U.S. Government catalog under NSN 2840-01-184-8573. This indicates validated use in U.S. government and defense supply chains.

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4064666 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

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