9502M33P01 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9502M33P01: SEAL,AIR,AIRCRAFT GAS TURBINE EN.

SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 7.545 INCHES MINIMUM AND 7.555 INCHES MAXIMUM IN, material: STEEL COMP 630 OVERALL, overall_length: 0.900 INCHES MINIMUM AND 0.910 INCHES MAXIMUM IN, hardness_rating: 28.0 ROCKWELL C MINIMUM AND 37.0 ROCKWELL C MAXIMUM OVERALL, special_features: T.O. 2J-F110-14; FAN FRAM ASSY; NO.

3 BEARING; 2ND END DIA. 7.400-7.401, surface_treatment: NICKEL OVERALL. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-146-5653, 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

9502M33P01

NSN: 2840-01-146-5653
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

diameter	7.545 INCHES MINIMUM AND 7.555 INCHES MAXIMUM IN
material	STEEL COMP 630 OVERALL
overall_length	0.900 INCHES MINIMUM AND 0.910 INCHES MAXIMUM IN
hardness_rating	28.0 ROCKWELL C MINIMUM AND 37.0 ROCKWELL C MAXIMUM OVERALL
special_features	T.O. 2J-F110-14; FAN FRAM ASSY; NO. 3 BEARING; 2ND END DIA. 7.400-7.401
surface_treatment	NICKEL OVERALL
end_item_identification	F110-GE-110 AIRCRAFT ENGINE
engine_section_location	TURBINE
criticality_code_justification	AGAV
material_document_and_classification	AMS5643 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-146-5653

COMPONENT DIAGRAM

KEY FEATURES

•

HARDNESS RATING: 28.0 ROCKWELL C MINIMUM AND 37.0 ROCKWELL C MAXIMUM OVERALL

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5643 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

DIAMETER: 7.545 INCHES MINIMUM AND 7.555 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: TURBINE

•

SURFACE TREATMENT: NICKEL OVERALL

TECHNICAL CHARACTERISTICS

HARDNESS RATING	28.0 ROCKWELL C MINIMUM AND 37.0 ROCKWELL C MAXIMUM OVERALL
CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5643 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	7.545 INCHES MINIMUM AND 7.555 INCHES MAXIMUM IN
OVERALL LENGTH	0.900 INCHES MINIMUM AND 0.910 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	TURBINE
SPECIAL FEATURES	T.O. 2J-F110-14; FAN FRAM ASSY; NO. 3 BEARING; 2ND END DIA. 7.400-7.401
SURFACE TREATMENT	NICKEL OVERALL
END ITEM IDENTIFICATION	F110-GE-110 AIRCRAFT ENGINE
MATERIAL	STEEL COMP 630 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.

2840-00-004-4242 2840-00-021-4702 2840-00-043-0981 2840-00-043-0982 2840-00-048-5261 2840-00-407-9165 2840-01-171-0875

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 9502M33P01?

9502M33P01 is a SEAL,AIR,AIRCRAFT GAS TURBINE EN.

What is the NSN for 9502M33P01?

9502M33P01 is cataloged in the U.S. Government catalog under NSN 2840-01-146-5653. This indicates validated use in U.S. government and defense supply chains.

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9502M33P01 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

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