1284M82G01 — SHROUD SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1284M82G01: SHROUD SEGMENT,TURBINE,AIRCRAFT.

SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include material: ALUMINUM ALLOY 2618 OVERALL, overall_width: 1.890 INCHES NOMINAL IN, overall_length: 12.233 INCHES NOMINAL IN, surface_treatment: ANODIZE OVERALL, end_item_identification: F110 ACFT ENGINE, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-200-6464, 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

1284M82G01

NSN: 2840-01-200-6464
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY 2618 OVERALL
stage_number	2
overall_width	1.890 INCHES NOMINAL IN
overall_length	12.233 INCHES NOMINAL IN
surface_treatment	ANODIZE OVERALL
end_item_identification	F110 ACFT ENGINE
engine_section_location	COMPRESSOR
criticality_code_justification	AGAV
material_document_and_classification	AMS4132 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-200-6464

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 2

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

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

•

ENGINE SECTION LOCATION: COMPRESSOR

•

SURFACE TREATMENT: ANODIZE OVERALL

TECHNICAL CHARACTERISTICS

STAGE NUMBER	2
CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS4132 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
OVERALL LENGTH	12.233 INCHES NOMINAL IN
OVERALL WIDTH	1.890 INCHES NOMINAL IN
ENGINE SECTION LOCATION	COMPRESSOR
SPECIAL FEATURES	OUTER RADIUS 2ND END 11.908 IN.; INNER RADIUS 1ST END 11.393 IN.; INNER RADIUS 2ND END 11.14 IN.; FORMED SHAPE 45 DEG. 57 MIN. 27 SEC.; 11 HOLES 0.3535 IN. DIA. COUNTERBORE 0.520 IN. DIA. W/2 CUTTER RUN OUTS PER EA HOLE IN
SURFACE TREATMENT	ANODIZE OVERALL
END ITEM IDENTIFICATION	F110 ACFT ENGINE
MATERIAL	ALUMINUM ALLOY 2618 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

1284M82G05Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 1284M82G01?

1284M82G01 is a SHROUD SEGMENT,TURBINE,AIRCRAFT.

What parts can replace 1284M82G01?

There is 1 known substitute for 1284M82G01: 1284M82G05. Substitute compatibility should be verified for your specific system.

What is the NSN for 1284M82G01?

1284M82G01 is cataloged in the U.S. Government catalog under NSN 2840-01-200-6464. This indicates validated use in U.S. government and defense supply chains.

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1284M82G01 — SHROUD SEGMENT,TURBINE,AIRCRAFT

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