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1864M32G01 — NOZZLE,TURBINE,AIRCRAFT GAS TURB

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

1864M32G01: NOZZLE,TURBINE,AIRCRAFT GAS TURB.

NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include material: NICKEL OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 4.117 INCHES NOMINAL IN, end_item_identification: ACFT ENG TF39, engine_section_location: HIGH PRESSURE TURBINE, criticality_code_justification: AGAV. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-444-6553, 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
1864M32G01
NSN: 2840-01-444-6553
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
materialNICKEL OVERALL
design_typeAXIAL COMPRESSOR
stage_number2
overall_length4.117 INCHES NOMINAL IN
end_item_identificationACFT ENG TF39
engine_section_locationHIGH PRESSURE TURBINE
criticality_code_justificationAGAV
NSN2840-01-444-6553
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available NOZZLE,TURBINE,AIRCRAFT GAS TURB TITLE COMPONENT PN 1864M32G01 MFR NOZZLE,TURBINE,AIRCRAF
KEY FEATURES
•
STAGE NUMBER: 2
•
DESIGN TYPE: AXIAL COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
ENGINE SECTION LOCATION: HIGH PRESSURE TURBINE
•
MATERIAL: NICKEL OVERALL
TECHNICAL CHARACTERISTICS
STAGE NUMBER2
DESIGN TYPEAXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATIONAGAV
OVERALL LENGTH4.117 INCHES NOMINAL IN
ENGINE SECTION LOCATIONHIGH PRESSURE TURBINE
SPECIAL FEATURESDIFFERENT FROM 1864M32G02 NOTE LOCATION OF HOLES DRILLED ON STACKING AXIS OF AIRFOILS, ALSO NOTE THIS IS PART OF THE HT90 MOD FOR THE TF39 ENGINE, ALSO NOTE THE DRAWING NAME IS NOZZLE, HIGH PRESSURE TURBINE-STAGE 2 MACHINING, AND NOZZLE IS COATED WITH NICKEL PLATING, ALSO LENGTH IS 4.11745
END ITEM IDENTIFICATIONACFT ENG TF39
MATERIALNICKEL 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
1864M32Reference document
Same NSN cross-reference
Reference document — Drawing number reference only
LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — mutilation + specific procedure
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FREQUENTLY ASKED QUESTIONS
What is 1864M32G01?
1864M32G01 is a NOZZLE,TURBINE,AIRCRAFT GAS TURB.
What parts can replace 1864M32G01?
There is 1 known substitute for 1864M32G01: 1864M32. Substitute compatibility should be verified for your specific system.
What is the NSN for 1864M32G01?
1864M32G01 is cataloged in the U.S. Government catalog under NSN 2840-01-444-6553. This indicates validated use in U.S. government and defense supply chains.
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