1276M30G02 — CASE,TURBINE,AIRCRAFT GAS TURBIN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1276M30G02: CASE,TURBINE,AIRCRAFT GAS TURBIN.

CASE,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include design_type: AXIAL COMPRESSOR, overall_length: 2.359 INCHES MINIMUM AND 2.383 INCHES MAXIMUM IN, special_features: USED ON THE NOZZLE ASSEMBLY AND SEGMENTS, SEALS AND SUPPORTS, end_item_identification: ACFT ENG F110GE129, engine_section_location: HIGH PRESSURE TURBINE, reference_data_and_literature: T.O. 2J-F110-14, FIG 74, IND 17.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-447-2846, 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

1276M30G02

NSN: 2840-01-447-2846
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

design_type	AXIAL COMPRESSOR
overall_length	2.359 INCHES MINIMUM AND 2.383 INCHES MAXIMUM IN
special_features	USED ON THE NOZZLE ASSEMBLY AND SEGMENTS, SEALS AND SUPPORTS
end_item_identification	ACFT ENG F110GE129
engine_section_location	HIGH PRESSURE TURBINE
reference_data_and_literature	T.O. 2J-F110-14, FIG 74, IND 17
criticality_code_justification	ABHP AND CZBJ AND FEAT
part_name_assigned_by_controlling_agency	COVER,COOLING AIR-HIGH PRESSURE TURBINE NOZZLE,OUTER
NSN	2840-01-447-2846

COMPONENT DIAGRAM

KEY FEATURES

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: ABHP AND CZBJ AND FEAT

•

REFERENCE DATA AND LITERATURE: T.O. 2J-F110-14, FIG 74, IND 17

•

ENGINE SECTION LOCATION: HIGH PRESSURE TURBINE

TECHNICAL CHARACTERISTICS

DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	ABHP AND CZBJ AND FEAT
REFERENCE DATA AND LITERATURE	T.O. 2J-F110-14, FIG 74, IND 17
OVERALL LENGTH	2.359 INCHES MINIMUM AND 2.383 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	HIGH PRESSURE TURBINE
SPECIAL FEATURES	USED ON THE NOZZLE ASSEMBLY AND SEGMENTS, SEALS AND SUPPORTS
PART NAME ASSIGNED BY CONTROLLING AGENCY	COVER,COOLING AIR-HIGH PRESSURE TURBINE NOZZLE,OUTER
END ITEM IDENTIFICATION	ACFT ENG F110GE129

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

KDS 2840-4003Reference 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 1276M30G02?

1276M30G02 is a CASE,TURBINE,AIRCRAFT GAS TURBIN.

What parts can replace 1276M30G02?

There is 1 known substitute for 1276M30G02: KDS 2840-4003. Substitute compatibility should be verified for your specific system.

What is the NSN for 1276M30G02?

1276M30G02 is cataloged in the U.S. Government catalog under NSN 2840-01-447-2846. This indicates validated use in U.S. government and defense supply chains.

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1276M30G02 — CASE,TURBINE,AIRCRAFT GAS TURBIN

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