5901T07P02 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

5901T07P02: SEAL,AIR,AIRCRAFT GAS TURBINE EN.

SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 10.406 INCHES MINIMUM AND 10.412 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, overall_length: 0.610 INCHES MINIMUM AND 0.630 INCHES MAXIMUM IN, end_item_identification: J85-21 AIRCRAFT ENGINE, engine_section_location: TURBINE, criticality_code_justification: AGAV. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-336-2438, 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

5901T07P02

NSN: 2840-01-336-2438
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 99207 — GENERAL ELECTRIC COMPANY DBA GE AEROSPACE (USA)

SPECIFICATIONS

diameter	10.406 INCHES MINIMUM AND 10.412 INCHES MAXIMUM IN
material	NICKEL ALLOY OVERALL
stage_number	1
overall_length	0.610 INCHES MINIMUM AND 0.630 INCHES MAXIMUM IN
end_item_identification	J85-21 AIRCRAFT ENGINE
engine_section_location	TURBINE
criticality_code_justification	AGAV
material_document_and_classification	AMS5537 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-336-2438

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5537 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

DIAMETER: 10.406 INCHES MINIMUM AND 10.412 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: TURBINE

•

MATERIAL: NICKEL ALLOY OVERALL

TECHNICAL CHARACTERISTICS

STAGE NUMBER	1
CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5537 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	10.406 INCHES MINIMUM AND 10.412 INCHES MAXIMUM IN
OVERALL LENGTH	0.610 INCHES MINIMUM AND 0.630 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	TURBINE
END ITEM IDENTIFICATION	J85-21 AIRCRAFT ENGINE
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 1

5901T07P01Reference document

Same NSN cross-reference

Reference document — Secondary reference

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 5901T07P02?

5901T07P02 is a SEAL,AIR,AIRCRAFT GAS TURBINE EN.

What parts can replace 5901T07P02?

There is 1 known substitute for 5901T07P02: 5901T07P01. Substitute compatibility should be verified for your specific system.

What is the NSN for 5901T07P02?

5901T07P02 is cataloged in the U.S. Government catalog under NSN 2840-01-336-2438. This indicates validated use in U.S. government and defense supply chains.

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5901T07P02 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

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