9526M39G02 — CASE,TURBINE,AIRCRAFT GAS TURBIN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9526M39G02: CASE,TURBINE,AIRCRAFT GAS TURBIN.

CASE,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include diameter: 27.062 INCHES MINIMUM AND 27.082 INCHES MAXIMUM IN, material: ALUMINUM ALLOY OVERALL, overall_length: 5.262 INCHES NOMINAL IN, special_features: ORIGINALLY CASE,TURBINE ROTOR,TURBINE ENGINE; 1ST STAGE, end_item_identification: ACFT ENG F101, engine_section_location: TURBINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-147-2695, 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

9526M39G02

NSN: 2840-01-147-2695
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

diameter	27.062 INCHES MINIMUM AND 27.082 INCHES MAXIMUM IN
material	ALUMINUM ALLOY OVERALL
overall_length	5.262 INCHES NOMINAL IN
special_features	ORIGINALLY CASE,TURBINE ROTOR,TURBINE ENGINE; 1ST STAGE
end_item_identification	ACFT ENG F101
engine_section_location	TURBINE
criticality_code_justification	AGAV
material_document_and_classification	AMS4132 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-147-2695

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS4132 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

DIAMETER: 27.062 INCHES MINIMUM AND 27.082 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: TURBINE

•

MATERIAL: ALUMINUM ALLOY OVERALL

TECHNICAL CHARACTERISTICS

CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS4132 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	27.062 INCHES MINIMUM AND 27.082 INCHES MAXIMUM IN
OVERALL LENGTH	5.262 INCHES NOMINAL IN
ENGINE SECTION LOCATION	TURBINE
SPECIAL FEATURES	ORIGINALLY CASE,TURBINE ROTOR,TURBINE ENGINE; 1ST STAGE
END ITEM IDENTIFICATION	ACFT ENG F101
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 — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 9526M39G02?

9526M39G02 is a CASE,TURBINE,AIRCRAFT GAS TURBIN.

What is the NSN for 9526M39G02?

9526M39G02 is cataloged in the U.S. Government catalog under NSN 2840-01-147-2695. This indicates validated use in U.S. government and defense supply chains.

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9526M39G02 — CASE,TURBINE,AIRCRAFT GAS TURBIN

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