9608M40P02 — NOZZLE,LUBRICATING,AIRCRAFT GAS

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9608M40P02: NOZZLE,LUBRICATING,AIRCRAFT GAS.

NOZZLE,LUBRICATING,AIRCRAFT GAS. Key specifications include material: ALUMINUM ALLOY OVERALL, overall_length: 0.260 INCHES MINIMUM AND 0.280 INCHES MAXIMUM IN, surface_treatment: ANODIZE OVERALL, end_item_identification: ACFT ENG TF-39, engine_section_location: TURBINE, material_document_and_classification: AMS4121 ASSN STD SINGLE MATERIAL RESPONSE OVERALL. This part is cataloged in the U.S.

Government catalog under NSN 2840-00-107-8844, 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

9608M40P02

NSN: 2840-00-107-8844
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY OVERALL
overall_length	0.260 INCHES MINIMUM AND 0.280 INCHES MAXIMUM IN
surface_treatment	ANODIZE OVERALL
end_item_identification	ACFT ENG TF-39
engine_section_location	TURBINE
material_document_and_classification	AMS4121 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
surface_treatment_document_and_classification	AMS2470 ASSN STD SINGLE TREATMENT RESPONSE OVERALL
NSN	2840-00-107-8844

COMPONENT DIAGRAM

KEY FEATURES

•

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION: AMS2470 ASSN STD SINGLE TREATMENT RESPONSE OVERALL

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS4121 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

ENGINE SECTION LOCATION: TURBINE

•

SURFACE TREATMENT: ANODIZE OVERALL

•

MATERIAL: ALUMINUM ALLOY OVERALL

TECHNICAL CHARACTERISTICS

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	AMS2470 ASSN STD SINGLE TREATMENT RESPONSE OVERALL
MATERIAL DOCUMENT AND CLASSIFICATION	AMS4121 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
OVERALL LENGTH	0.260 INCHES MINIMUM AND 0.280 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	TURBINE
SURFACE TREATMENT	ANODIZE OVERALL
END ITEM IDENTIFICATION	ACFT ENG TF-39
MATERIAL	ALUMINUM 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.

2840-00-004-4242 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

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

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FREQUENTLY ASKED QUESTIONS

What is 9608M40P02?

9608M40P02 is a NOZZLE,LUBRICATING,AIRCRAFT GAS.

What is the NSN for 9608M40P02?

9608M40P02 is cataloged in the U.S. Government catalog under NSN 2840-00-107-8844. This indicates validated use in U.S. government and defense supply chains.

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9608M40P02 — NOZZLE,LUBRICATING,AIRCRAFT GAS

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