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9993M75G14 — NOZZLE SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

9993M75G14: NOZZLE SEGMENT,TURBINE,AIRCRAFT.

NOZZLE SEGMENT,TURBINE,AIRCRAFT. Key specifications include material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 4.000 INCHES NOMINAL IN, special_features: TWO BLADE ASSEMBLY, end_item_identification: ACFT.ENG. F108, engine_section_location: TURBINE.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-253-1391, 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
9993M75G14
NSN: 2840-01-253-1391
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 58828 — CFM INTERNATIONAL INC DBA CFM INTERNATIONAL (USA)
SPECIFICATIONS
materialNICKEL ALLOY OVERALL
design_typeAXIAL COMPRESSOR
overall_length4.000 INCHES NOMINAL IN
special_featuresTWO BLADE ASSEMBLY
end_item_identificationACFT.ENG. F108
engine_section_locationTURBINE
reference_data_and_literatureTO. 2J-F108-14
criticality_code_justificationCZBJ AND FEAT
part_name_assigned_by_controlling_agencyNOZZLE SEGMENT-HPT STATOR
NSN2840-01-253-1391
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available NOZZLE SEGMENT,TURBINE,AIRCRAFT TITLE COMPONENT PN 9993M75G14 MFR NOZZLE SEGMENT,TURBINE
KEY FEATURES
•
DESIGN TYPE: AXIAL COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: CZBJ AND FEAT
•
REFERENCE DATA AND LITERATURE: TO. 2J-F108-14
•
ENGINE SECTION LOCATION: TURBINE
TECHNICAL CHARACTERISTICS
DESIGN TYPEAXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATIONCZBJ AND FEAT
REFERENCE DATA AND LITERATURETO. 2J-F108-14
OVERALL LENGTH4.000 INCHES NOMINAL IN
ENGINE SECTION LOCATIONTURBINE
SPECIAL FEATURESTWO BLADE ASSEMBLY
PART NAME ASSIGNED BY CONTROLLING AGENCYNOZZLE SEGMENT-HPT STATOR
END ITEM IDENTIFICATIONACFT.ENG. F108
MATERIALNICKEL 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 8
1285M96G03Reference document
Same NSN cross-reference
Reference document — Secondary reference
1285M96G09Reference document
Same NSN cross-reference
Reference document — Secondary reference
1285M96G06Reference document
Same NSN cross-reference
Reference document — Secondary reference
1319M96G06Reference document
Same NSN cross-reference
Reference document — Secondary reference
1319M96G03Reference document
Same NSN cross-reference
Reference document — Secondary reference
1319M96G04Reference document
Same NSN cross-reference
Reference document — Secondary reference
LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — mutilation + specific procedure
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FREQUENTLY ASKED QUESTIONS
What is 9993M75G14?
9993M75G14 is a NOZZLE SEGMENT,TURBINE,AIRCRAFT.
What parts can replace 9993M75G14?
There are 8 known substitutes for 9993M75G14: 1285M96G03, 1285M96G09, 1285M96G06 and 5 more. Substitute compatibility should be verified for your specific system.
What is the NSN for 9993M75G14?
9993M75G14 is cataloged in the U.S. Government catalog under NSN 2840-01-253-1391. This indicates validated use in U.S. government and defense supply chains.
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✓ PartsTable — the parts reference. Every fact cited to its source.
PartsTable Design LLC · partstable.com
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-18.
PartsTable commercial catalog: edition Unified commercial catalog snapshot through 2026-09-28, edition date not on file, retrieved 2026-09-28.