38400082 — BLADE,TURBINE ROTOR,NONAIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

38400082: BLADE,TURBINE ROTOR,NONAIRCRAFT.

BLADE,TURBINE ROTOR,NONAIRCRAFT. Key specifications include material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_width: 1.044 INCHES NOMINAL IN, overall_length: 1.489 INCHES NOMINAL IN, blade_attachment_method: LOCK, end_item_identification: 2G-GTCP331-4 C17 ACFT G. This part is cataloged in the U.S.

Government catalog under NSN 2835-01-356-3687, 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

38400082

NSN: 2835-01-356-3687
NIINs: 013563687, 016565390
FSC: 2835 — Gas Turbines and Jet Engines; Non-aircraft Prime Mover, Aircraft Non-prime Mover, and Components
CAGE: 99193 — HONEYWELL INTERNATIONAL INC. DBA HONEYWELL INTERNATIONAL DIV AEROSPACE - PHOENIX (USA)

SPECIFICATIONS

material	NICKEL ALLOY OVERALL
design_type	AXIAL COMPRESSOR
stage_number	2
overall_width	1.044 INCHES NOMINAL IN
overall_length	1.489 INCHES NOMINAL IN
blade_attachment_method	LOCK
end_item_identification	2G-GTCP331-4 C17 ACFT G
engine_section_location	HIGH PRESSURE TURBINE
material_document_and_classification	IN792 AND HF PER AIRSEARCH EMS 55450 MFR REF ALL MATERIAL RESPONSES OVERALL
surface_treatment_document_and_classification	AIRSEARCH EMS52460 CATAGORY M,TYPE 1,CLASS 2 MFR REF ALL TREATMENT RESPONSES OVERALL
NSN	2835-01-356-3687

COMPONENT DIAGRAM

KEY FEATURES

•

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION: AIRSEARCH EMS52460 CATAGORY M,TYPE 1,CLASS 2 MFR REF ALL TREATMENT RESPONSES OVERALL

•

STAGE NUMBER: 2

•

DESIGN TYPE: AXIAL COMPRESSOR

•

BLADE ATTACHMENT METHOD: LOCK

•

MATERIAL DOCUMENT AND CLASSIFICATION: IN792 AND HF PER AIRSEARCH EMS 55450 MFR REF ALL MATERIAL RESPONSES OVERALL

•

ENGINE SECTION LOCATION: HIGH PRESSURE TURBINE

TECHNICAL CHARACTERISTICS

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	AIRSEARCH EMS52460 CATAGORY M,TYPE 1,CLASS 2 MFR REF ALL TREATMENT RESPONSES OVERALL
STAGE NUMBER	2
DESIGN TYPE	AXIAL COMPRESSOR
BLADE ATTACHMENT METHOD	LOCK
MATERIAL DOCUMENT AND CLASSIFICATION	IN792 AND HF PER AIRSEARCH EMS 55450 MFR REF ALL MATERIAL RESPONSES OVERALL
OVERALL LENGTH	1.489 INCHES NOMINAL IN
OVERALL WIDTH	1.044 INCHES NOMINAL IN
ENGINE SECTION LOCATION	HIGH PRESSURE TURBINE
END ITEM IDENTIFICATION	2G-GTCP331-4 C17 ACFT G
MATERIAL	NICKEL ALLOY OVERALL

SUBSTITUTES & CROSS-REFERENCES 1

E3840008-2Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

LIFECYCLE

NSN statusActive· U.S. Government catalog

No demilitarization required

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FREQUENTLY ASKED QUESTIONS

What is 38400082?

38400082 is a BLADE,TURBINE ROTOR,NONAIRCRAFT.

What parts can replace 38400082?

There is 1 known substitute for 38400082: E3840008-2. Substitute compatibility should be verified for your specific system.

What is the NSN for 38400082?

38400082 is cataloged in the U.S. Government catalog under NSN 2835-01-356-3687. This indicates validated use in U.S. government and defense supply chains.

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38400082 — BLADE,TURBINE ROTOR,NONAIRCRAFT

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