2-02295W121010 — SHAFT ASSEMBLY,TURBINE

✓ Government record, cited

— · HOSE FITTING

PRODUCT OVERVIEW

2-02295W121010: SHAFT ASSEMBLY,TURBINE.

The SHAFT ASSEMBLY,TURBINE is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075 OVERALL, leg_length: 1.940 INCHES NOMINAL SECOND END IN, seat_angle: 12.0 DEGREES FIRST END, thread_class: 3A SECOND END A, surface_treatment: ANODIZE OVERALL, operating_pressure: 1500.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM SINGLE RESPONSE LBS. This part is cataloged in the U.S.

Government catalog under NSN 4730-01-199-6551, 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

2-02295W121010

NSN: 4730-01-199-6551
FSC: 4730 — Hose, Pipe, Tube, Lubrication, and Railing Fittings
CAGE: 00624 — EATON AEROQUIP LLC DBA JACKSON NORTH 1 DIV FLUID AND ELECTRICAL DISTRIBUTION (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 7075 OVERALL
leg_length	1.940 INCHES NOMINAL SECOND END IN
seat_angle	12.0 DEGREES FIRST END
thread_class	3A SECOND END A
surface_treatment	ANODIZE OVERALL
operating_pressure	1500.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM SINGLE RESPONSE LBS
nominal_thread_size	1.312 INCHES SECOND END IN
thread_quantity_per_inch	12A SECOND END A
thread_series_designator	UN SECOND END
material_document_and_classification	QQ-A-367,T73 FED SPEC SINGLE MATERIAL RESPONSE OVERALL
surface_treatment_document_and_classification	MIL-A-8625,TY 2,CL 1 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL
NSN	4730-01-199-6551

COMPONENT DIAGRAM

KEY FEATURES

•

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION: MIL-A-8625,TY 2,CL 1 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-367,T73 FED SPEC SINGLE MATERIAL RESPONSE OVERALL

•

OPERATING PRESSURE: 1500.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM SINGLE RESPONSE LBS

•

LEG LENGTH: 1.940 INCHES NOMINAL SECOND END IN

•

NOMINAL THREAD SIZE: 0.875 INCHES FIRST END IN

TECHNICAL CHARACTERISTICS

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	MIL-A-8625,TY 2,CL 1 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-367,T73 FED SPEC SINGLE MATERIAL RESPONSE OVERALL
OPERATING PRESSURE	1500.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM SINGLE RESPONSE LBS
LEG LENGTH	1.940 INCHES NOMINAL SECOND END IN
LEG LENGTH	1.267 INCHES NOMINAL FIRST END IN
LEG LENGTH	1.267 INCHES NOMINAL THIRD END IN
NOMINAL THREAD SIZE	0.875 INCHES FIRST END IN
NOMINAL THREAD SIZE	1.312 INCHES SECOND END IN
SEAT ANGLE	12.0 DEGREES FIRST END
SURFACE TREATMENT	ANODIZE OVERALL

SUBSTITUTES & CROSS-REFERENCES 2

DLE231W1210Reference document

Same NSN cross-reference

Reference document — Secondary reference

2-02295Reference document

Same NSN cross-reference

Reference document — Drawing number reference only

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Normally procured from the manufacturer (OEM)No demilitarization required

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FREQUENTLY ASKED QUESTIONS

What is 2-02295W121010?

2-02295W121010 is a SHAFT ASSEMBLY,TURBINE.

What parts can replace 2-02295W121010?

There are 2 known substitutes for 2-02295W121010: DLE231W1210, 2-02295. Substitute compatibility should be verified for your specific system.

What is the NSN for 2-02295W121010?

2-02295W121010 is cataloged in the U.S. Government catalog under NSN 4730-01-199-6551. This indicates validated use in U.S. government and defense supply chains.

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