3501310-2 — CASE,TURBINE,NONAIRCRAFT GAS TUR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

3501310-2: CASE,TURBINE,NONAIRCRAFT GAS TUR.

CASE,TURBINE,NONAIRCRAFT GAS TUR. Key specifications include diameter: 4.900 INCHES NOMINAL IN, material: ALUMINUM ALLOY OVERALL, overall_height: 1.640 INCHES NOMINAL IN, overall_length: 7.680 INCHES NOMINAL IN, surface_treatment: ANODIZE OVERALL, engine_section_location: TURBINE. This part is cataloged in the U.S.

Government catalog under NSN 2835-01-349-9013, 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

3501310-2

NSN: 2835-01-349-9013
FSC: 2835 — Gas Turbines and Jet Engines; Non-aircraft Prime Mover, Aircraft Non-prime Mover, and Components
CAGE: 59364 — HONEYWELL INTERNATIONAL INC. DBA HONEYWELL INTERNATIONAL DIV AEROSPACE - TEMPE (WEST WARNER ROAD) (USA)

SPECIFICATIONS

diameter	4.900 INCHES NOMINAL IN
material	ALUMINUM ALLOY OVERALL
overall_height	1.640 INCHES NOMINAL IN
overall_length	7.680 INCHES NOMINAL IN
surface_treatment	ANODIZE OVERALL
engine_section_location	TURBINE
material_document_and_classification	AMS4260 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
part_name_assigned_by_controlling_agency	CASE,GAS TURBINE ENGINE
surface_treatment_document_and_classification	MIL-A-8625 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL
NSN	2835-01-349-9013

COMPONENT DIAGRAM

KEY FEATURES

•

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION: MIL-A-8625 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS4260 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

DIAMETER: 4.900 INCHES NOMINAL IN

•

ENGINE SECTION LOCATION: TURBINE

•

SURFACE TREATMENT: ANODIZE OVERALL

TECHNICAL CHARACTERISTICS

OVERALL HEIGHT	1.640 INCHES NOMINAL IN
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	MIL-A-8625 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL
MATERIAL DOCUMENT AND CLASSIFICATION	AMS4260 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	4.900 INCHES NOMINAL IN
OVERALL LENGTH	7.680 INCHES NOMINAL IN
ENGINE SECTION LOCATION	TURBINE
SURFACE TREATMENT	ANODIZE OVERALL
PART NAME ASSIGNED BY CONTROLLING AGENCY	CASE,GAS TURBINE ENGINE
MATERIAL	ALUMINUM ALLOY OVERALL

OTHER ITEMS IN FSC 2835 — Gas Turbines and Jet Engines; Non-aircraft Prime Mover, Aircraft Non-prime Mover, and Components

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

2835-00-003-1224 2835-00-003-1225 2835-00-003-1226 2835-00-003-1227 2835-00-003-1228 2835-00-003-1229 2835-00-003-1230 2835-00-003-1231

SUBSTITUTES & CROSS-REFERENCES 1

3501310-1Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Normally procured from the manufacturer (OEM)Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 3501310-2?

3501310-2 is a CASE,TURBINE,NONAIRCRAFT GAS TUR.

What parts can replace 3501310-2?

There is 1 known substitute for 3501310-2: 3501310-1. Substitute compatibility should be verified for your specific system.

What is the NSN for 3501310-2?

3501310-2 is cataloged in the U.S. Government catalog under NSN 2835-01-349-9013. This indicates validated use in U.S. government and defense supply chains.

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3501310-2 — CASE,TURBINE,NONAIRCRAFT GAS TUR

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