9992M65G08 — SHROUD SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9992M65G08: SHROUD SEGMENT,TURBINE,AIRCRAFT.

SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include material: ALUMINUM ALLOY 2219 OVERALL, design_type: COMPRESSOR, overall_width: 1.024 INCHES NOMINAL IN, overall_length: 8.630 INCHES NOMINAL IN, surface_treatment: ANODIZE OVERALL, end_item_identification: ACFT ENG F108. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-264-2253, 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

9992M65G08

NSN: 2840-01-264-2253
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 2219 OVERALL
design_type	COMPRESSOR
stage_number	1
overall_width	1.024 INCHES NOMINAL IN
overall_length	8.630 INCHES NOMINAL IN
surface_treatment	ANODIZE OVERALL
end_item_identification	ACFT ENG F108
engine_section_location	LOW PRESSURE COMPRESSOR
criticality_code_justification	MATT
material_document_and_classification	AMS4143 ASSN STD 1ST MATERIAL RESPONSE AND AMS4162 ASSN STD 2ND MATERIAL RESPONSE OVERALL
NSN	2840-01-264-2253

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

DESIGN TYPE: COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: MATT

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS4143 ASSN STD 1ST MATERIAL RESPONSE AND AMS4162 ASSN STD 2ND MATERIAL RESPONSE OVERALL

•

ENGINE SECTION LOCATION: LOW PRESSURE COMPRESSOR

•

SURFACE TREATMENT: ANODIZE OVERALL

TECHNICAL CHARACTERISTICS

STAGE NUMBER	1
DESIGN TYPE	COMPRESSOR
CRITICALITY CODE JUSTIFICATION	MATT
MATERIAL DOCUMENT AND CLASSIFICATION	AMS4143 ASSN STD 1ST MATERIAL RESPONSE AND AMS4162 ASSN STD 2ND MATERIAL RESPONSE OVERALL
OVERALL LENGTH	8.630 INCHES NOMINAL IN
OVERALL WIDTH	1.024 INCHES NOMINAL IN
ENGINE SECTION LOCATION	LOW PRESSURE COMPRESSOR
SURFACE TREATMENT	ANODIZE OVERALL
END ITEM IDENTIFICATION	ACFT ENG F108
MATERIAL	ALUMINUM ALLOY 2219 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 1

9992M65G10Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Insurance item — stocked against contingency demandDemilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 9992M65G08?

9992M65G08 is a SHROUD SEGMENT,TURBINE,AIRCRAFT.

What parts can replace 9992M65G08?

There is 1 known substitute for 9992M65G08: 9992M65G10. Substitute compatibility should be verified for your specific system.

What is the NSN for 9992M65G08?

9992M65G08 is cataloged in the U.S. Government catalog under NSN 2840-01-264-2253. This indicates validated use in U.S. government and defense supply chains.

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9992M65G08 — SHROUD SEGMENT,TURBINE,AIRCRAFT

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