1276M66G01 — SHROUD SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1276M66G01: SHROUD SEGMENT,TURBINE,AIRCRAFT.

SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include diameter: 8.465 INCHES NOMINAL IN, material: ALUMINUM ALLOY OVERALL, design_type: COMPRESSOR, overall_width: 2.204 INCHES NOMINAL IN, overall_length: 2.354 INCHES NOMINAL IN, surface_treatment: ANODIZE OVERALL. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-146-9391, 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

1276M66G01

NSN: 2840-01-146-9391
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

diameter	8.465 INCHES NOMINAL IN
material	ALUMINUM ALLOY OVERALL
design_type	COMPRESSOR
overall_width	2.204 INCHES NOMINAL IN
overall_length	2.354 INCHES NOMINAL IN
special_features	180 DEG. 7.998-8.002 IN. ID BASED ON 360 DEG; 21 SLOTS 0.352-0.354 IN. WIDE BY 0.477-0.481 IN DEEP; 21 HOLES 0.186-0.187 IN
surface_treatment	ANODIZE OVERALL
end_item_identification	F101-GE-100,F108-CF-100,F110-GE-100
engine_section_location	LOW PRESSURE COMPRESSOR
criticality_code_justification	ABHP AND ABMK AND APGF AND CZBJ AND FEAT
material_document_and_classification	AMS4143 ASSN STD 1ST MATERIAL RESPONSE OR AMS4162 ASSN STD 2ND MATERIAL RESPONSE OVERALL
surface_treatment_document_and_classification	AMS2469 ASSN STD SINGLE TREATMENT RESPONSE OVERALL
NSN	2840-01-146-9391

COMPONENT DIAGRAM

KEY FEATURES

•

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION: AMS2469 ASSN STD SINGLE TREATMENT RESPONSE OVERALL

•

DESIGN TYPE: COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: ABHP AND ABMK AND APGF AND CZBJ AND FEAT

•

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

•

DIAMETER: 8.465 INCHES NOMINAL IN

•

ENGINE SECTION LOCATION: LOW PRESSURE COMPRESSOR

TECHNICAL CHARACTERISTICS

SURFACE TREATMENT DOCUMENT AND CLASSIFICATION	AMS2469 ASSN STD SINGLE TREATMENT RESPONSE OVERALL
DESIGN TYPE	COMPRESSOR
CRITICALITY CODE JUSTIFICATION	ABHP AND ABMK AND APGF AND CZBJ AND FEAT
MATERIAL DOCUMENT AND CLASSIFICATION	AMS4143 ASSN STD 1ST MATERIAL RESPONSE OR AMS4162 ASSN STD 2ND MATERIAL RESPONSE OVERALL
DIAMETER	8.465 INCHES NOMINAL IN
OVERALL LENGTH	2.354 INCHES NOMINAL IN
OVERALL WIDTH	2.204 INCHES NOMINAL IN
ENGINE SECTION LOCATION	LOW PRESSURE COMPRESSOR
SPECIAL FEATURES	180 DEG. 7.998-8.002 IN. ID BASED ON 360 DEG; 21 SLOTS 0.352-0.354 IN. WIDE BY 0.477-0.481 IN DEEP; 21 HOLES 0.186-0.187 IN
SURFACE TREATMENT	ANODIZE 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

9969M97G04Reference 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 1276M66G01?

1276M66G01 is a SHROUD SEGMENT,TURBINE,AIRCRAFT.

What parts can replace 1276M66G01?

There is 1 known substitute for 1276M66G01: 9969M97G04. Substitute compatibility should be verified for your specific system.

What is the NSN for 1276M66G01?

1276M66G01 is cataloged in the U.S. Government catalog under NSN 2840-01-146-9391. This indicates validated use in U.S. government and defense supply chains.

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