1864M32G02 — NOZZLE,TURBINE,AIRCRAFT GAS TURB

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1864M32G02: NOZZLE,TURBINE,AIRCRAFT GAS TURB.

NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include diameter: 34.568 INCHES NOMINAL IN, material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_height: 4.482 INCHES MINIMUM AND 4.505 INCHES MAXIMUM IN, overall_length: 2.013 INCHES MINIMUM AND 2.087 INCHES MAXIMUM IN, end_item_identification: TF-39 AIRCRAFT GAS TURBINE ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-444-7693, 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

1864M32G02

NSN: 2840-01-444-7693
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

diameter	34.568 INCHES NOMINAL IN
material	NICKEL ALLOY OVERALL
design_type	AXIAL COMPRESSOR
stage_number	2
overall_height	4.482 INCHES MINIMUM AND 4.505 INCHES MAXIMUM IN
overall_length	2.013 INCHES MINIMUM AND 2.087 INCHES MAXIMUM IN
end_item_identification	TF-39 AIRCRAFT GAS TURBINE ENGINE
engine_section_location	HIGH PRESSURE TURBINE
criticality_code_justification	ABHP AND ABKW AND ABMZ AND FEAT
NSN	2840-01-444-7693

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 2

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: ABHP AND ABKW AND ABMZ AND FEAT

•

DIAMETER: 34.568 INCHES NOMINAL IN

•

ENGINE SECTION LOCATION: HIGH PRESSURE TURBINE

TECHNICAL CHARACTERISTICS

OVERALL HEIGHT	4.482 INCHES MINIMUM AND 4.505 INCHES MAXIMUM IN
STAGE NUMBER	2
DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	ABHP AND ABKW AND ABMZ AND FEAT
DIAMETER	34.568 INCHES NOMINAL IN
OVERALL LENGTH	2.013 INCHES MINIMUM AND 2.087 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	HIGH PRESSURE TURBINE
SPECIAL FEATURES	T.O. 2J-TF39-4, FIG 62 IND 22; BOROSCOPE LOCATION; REPL P/N 9022M16G26; WHOLE NEW CONFIG BASED ON ECP 369, DCN 97-37; NEW MATL AND DESIGN CHANGES; NOT TO BE GRPD TO OLD CONFIG; WHEN OLD CONFIG COMES IN AND REPL BY TCTO KITS WITH NEW PARTS, OLD CONFIG IS THROWN AWAY, NOT MODIFIED, NOT I&SABLE; QTY 1 PER ASSY
END ITEM IDENTIFICATION	TF-39 AIRCRAFT GAS TURBINE ENGINE
MATERIAL	NICKEL 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

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 1864M32G02?

1864M32G02 is a NOZZLE,TURBINE,AIRCRAFT GAS TURB.

What is the NSN for 1864M32G02?

1864M32G02 is cataloged in the U.S. Government catalog under NSN 2840-01-444-7693. This indicates validated use in U.S. government and defense supply chains.

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1864M32G02 — NOZZLE,TURBINE,AIRCRAFT GAS TURB

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