1881M21P01 — NOZZLE,TURBINE,AIRCRAFT GAS TURB

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1881M21P01: NOZZLE,TURBINE,AIRCRAFT GAS TURB.

NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include design_type: AXIAL COMPRESSOR, overall_length: 2.515 INCHES MINIMUM AND 2.535 INCHES MAXIMUM IN, special_features: MATL RENE N5, end_item_identification: F101-GE-102 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: LOW PRESSURE TURBINE, criticality_code_justification: CZBJ AND CZCJ AND ABHP AND FEAT. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-422-7703, 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

1881M21P01

NSN: 2840-01-422-7703
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

design_type	AXIAL COMPRESSOR
stage_number	1
overall_length	2.515 INCHES MINIMUM AND 2.535 INCHES MAXIMUM IN
special_features	MATL RENE N5
end_item_identification	F101-GE-102 AIRCRAFT GAS TURBINE ENGINE
engine_section_location	LOW PRESSURE TURBINE
criticality_code_justification	CZBJ AND CZCJ AND ABHP AND FEAT
NSN	2840-01-422-7703

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: CZBJ AND CZCJ AND ABHP AND FEAT

•

ENGINE SECTION LOCATION: LOW PRESSURE TURBINE

TECHNICAL CHARACTERISTICS

STAGE NUMBER	1
DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	CZBJ AND CZCJ AND ABHP AND FEAT
OVERALL LENGTH	2.515 INCHES MINIMUM AND 2.535 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	LOW PRESSURE TURBINE
SPECIAL FEATURES	MATL RENE N5
END ITEM IDENTIFICATION	F101-GE-102 AIRCRAFT GAS TURBINE ENGINE

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

1881M21P02Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

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 1881M21P01?

1881M21P01 is a NOZZLE,TURBINE,AIRCRAFT GAS TURB.

What parts can replace 1881M21P01?

There is 1 known substitute for 1881M21P01: 1881M21P02. Substitute compatibility should be verified for your specific system.

What is the NSN for 1881M21P01?

1881M21P01 is cataloged in the U.S. Government catalog under NSN 2840-01-422-7703. This indicates validated use in U.S. government and defense supply chains.

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1881M21P01 — NOZZLE,TURBINE,AIRCRAFT GAS TURB

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