9395M66P01 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9395M66P01: SEAL,AIR,AIRCRAFT GAS TURBINE EN.

SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include material: NICKEL ALLOY OVERALL, overall_length: 0.989 INCHES MINIMUM AND 1.014 INCHES MAXIMUM IN, material_thickness: 0.052 INCHES MINIMUM AND 0.062 INCHES MAXIMUM IN, end_item_identification: ACFT ENG TF39, engine_section_location: LOW PRESSURE TURBINE, criticality_code_justification: AGAV. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-163-4384, 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

9395M66P01

NSN: 2840-01-163-4384
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	NICKEL ALLOY OVERALL
stage_number	4
overall_length	0.989 INCHES MINIMUM AND 1.014 INCHES MAXIMUM IN
material_thickness	0.052 INCHES MINIMUM AND 0.062 INCHES MAXIMUM IN
end_item_identification	ACFT ENG TF39
engine_section_location	LOW PRESSURE TURBINE
criticality_code_justification	AGAV
material_document_and_classification	INCONEL MFR REF SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-163-4384

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 4

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

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

•

ENGINE SECTION LOCATION: LOW PRESSURE TURBINE

•

MATERIAL THICKNESS: 0.052 INCHES MINIMUM AND 0.062 INCHES MAXIMUM IN

•

MATERIAL: NICKEL ALLOY OVERALL

TECHNICAL CHARACTERISTICS

STAGE NUMBER	4
CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	INCONEL MFR REF SINGLE MATERIAL RESPONSE OVERALL
OVERALL LENGTH	0.989 INCHES MINIMUM AND 1.014 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	LOW PRESSURE TURBINE
MATERIAL THICKNESS	0.052 INCHES MINIMUM AND 0.062 INCHES MAXIMUM IN
END ITEM IDENTIFICATION	ACFT ENG TF39
MATERIAL	NICKEL ALLOY OVERALL

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.

2840-00-000-0048 2840-00-000-0049 2840-00-001-1741 2840-00-001-1743 2840-00-001-2117 2840-00-001-2284 2840-00-001-3922 2840-00-001-4903

SUBSTITUTES & CROSS-REFERENCES

No substitute or cross-reference records for this part.

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 9395M66P01?

9395M66P01 is a SEAL,AIR,AIRCRAFT GAS TURBINE EN.

What is the NSN for 9395M66P01?

9395M66P01 is cataloged in the U.S. Government catalog under NSN 2840-01-163-4384. This indicates validated use in U.S. government and defense supply chains.

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9395M66P01 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

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