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9395M67P01 — NOZZLE,TURBINE,AIRCRAFT GAS TURB

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

9395M67P01: NOZZLE,TURBINE,AIRCRAFT GAS TURB.

NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include diameter: 28.450 INCHES MINIMUM AND 28.465 INCHES MAXIMUM IN, material: STEEL OVERALL, design_type: AXIAL COMPRESSOR, special_features: T.O. 2J-TF39-4, FIG 67 IND 38; MADE ALTERNATE JAN 94 FOR MAINTENANCE ECONOMY PER T.O.

2J-TF39-4S-2, end_item_identification: ACFT ENG TF39, engine_section_location: LOW PRESSURE TURBINE. This part is cataloged in the U.S. Government catalog under NSN 2840-01-163-6701, 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
9395M67P01
NSN: 2840-01-163-6701
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
diameter28.450 INCHES MINIMUM AND 28.465 INCHES MAXIMUM IN
materialSTEEL OVERALL
design_typeAXIAL COMPRESSOR
stage_number5
special_featuresT.O. 2J-TF39-4, FIG 67 IND 38; MADE ALTERNATE JAN 94 FOR MAINTENANCE ECONOMY PER T.O. 2J-TF39-4S-2
end_item_identificationACFT ENG TF39
engine_section_locationLOW PRESSURE TURBINE
criticality_code_justificationFEAT AND CZCJ AND CZBJ
NSN2840-01-163-6701
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available NOZZLE,TURBINE,AIRCRAFT GAS TURB TITLE COMPONENT PN 9395M67P01 MFR NOZZLE,TURBINE,AIRCRAF
KEY FEATURES
•
STAGE NUMBER: 5
•
DESIGN TYPE: AXIAL COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: FEAT AND CZCJ AND CZBJ
•
DIAMETER: 28.450 INCHES MINIMUM AND 28.465 INCHES MAXIMUM IN
•
ENGINE SECTION LOCATION: LOW PRESSURE TURBINE
•
MATERIAL: STEEL OVERALL
TECHNICAL CHARACTERISTICS
STAGE NUMBER5
DESIGN TYPEAXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATIONFEAT AND CZCJ AND CZBJ
DIAMETER28.450 INCHES MINIMUM AND 28.465 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONLOW PRESSURE TURBINE
SPECIAL FEATUREST.O. 2J-TF39-4, FIG 67 IND 38; MADE ALTERNATE JAN 94 FOR MAINTENANCE ECONOMY PER T.O. 2J-TF39-4S-2
END ITEM IDENTIFICATIONACFT ENG TF39
MATERIALSTEEL 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.
2840-00-000-0048 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

No substitute or cross-reference records for this part.

LIFECYCLE
NSN statusActive· U.S. Government catalog
Acquisition advice: Terminal item — no further procurement; issued until stock is exhaustedDemilitarization required — mutilation + specific procedure
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FREQUENTLY ASKED QUESTIONS
What is 9395M67P01?
9395M67P01 is a NOZZLE,TURBINE,AIRCRAFT GAS TURB.
What is the NSN for 9395M67P01?
9395M67P01 is cataloged in the U.S. Government catalog under NSN 2840-01-163-6701. This indicates validated use in U.S. government and defense supply chains.
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