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9383M91P01 — DISK,FAN,AIRCRAFT GAS TURBINE EN

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

9383M91P01: DISK,FAN,AIRCRAFT GAS TURBINE EN.

DISK,FAN,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 25.183 INCHES MINIMUM AND 25.191 INCHES MAXIMUM IN, design_type: AXIAL COMPRESSOR, overall_length: 4.360 INCHES NOMINAL IN, special_features: ORIGINAL NAME DISK,AXIAL COMPRESSOR,TURBINE ENGINE, end_item_identification: ACFT ENG TF-39, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.

Government catalog under NSN 2840-00-103-0824, 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
9383M91P01
NSN: 2840-00-103-0824
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
diameter25.183 INCHES MINIMUM AND 25.191 INCHES MAXIMUM IN
design_typeAXIAL COMPRESSOR
overall_length4.360 INCHES NOMINAL IN
special_featuresORIGINAL NAME DISK,AXIAL COMPRESSOR,TURBINE ENGINE
end_item_identificationACFT ENG TF-39
engine_section_locationCOMPRESSOR
criticality_code_justificationAGAV
NSN2840-00-103-0824
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available DISK,FAN,AIRCRAFT GAS TURBINE EN TITLE COMPONENT PN 9383M91P01 MFR DISK,FAN,AIRCRAFT GAS
KEY FEATURES
•
DESIGN TYPE: AXIAL COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
DIAMETER: 25.183 INCHES MINIMUM AND 25.191 INCHES MAXIMUM IN
•
ENGINE SECTION LOCATION: COMPRESSOR
TYPICAL APPLICATIONS
  • Server thermal management and cooling
  • Hot-swap fan replacement in production environments
  • Redundant cooling for high-availability systems
TECHNICAL CHARACTERISTICS
DESIGN TYPEAXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATIONAGAV
DIAMETER25.183 INCHES MINIMUM AND 25.191 INCHES MAXIMUM IN
OVERALL LENGTH4.360 INCHES NOMINAL IN
ENGINE SECTION LOCATIONCOMPRESSOR
SPECIAL FEATURESORIGINAL NAME DISK,AXIAL COMPRESSOR,TURBINE ENGINE
END ITEM IDENTIFICATIONACFT ENG TF-39
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
9653M10P05Same NSN cross-reference
Same NSN cross-reference
Also cataloged under this NSN
LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — mutilation + specific procedure
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FREQUENTLY ASKED QUESTIONS
What is 9383M91P01?
9383M91P01 is a DISK,FAN,AIRCRAFT GAS TURBINE EN.
What parts can replace 9383M91P01?
There is 1 known substitute for 9383M91P01: 9653M10P05. Substitute compatibility should be verified for your specific system.
What is the NSN for 9383M91P01?
9383M91P01 is cataloged in the U.S. Government catalog under NSN 2840-00-103-0824. This indicates validated use in U.S. government and defense supply chains.
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