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1317M36G05 — NOZZLE SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

1317M36G05: NOZZLE SEGMENT,TURBINE,AIRCRAFT.

NOZZLE SEGMENT,TURBINE,AIRCRAFT. Key specifications include design_type: AXIAL COMPRESSOR, special_features: TWO BLADE ASSEMBLY, end_item_identification: F108 AIRCRAFT ENGINE, engine_section_location: HIGH PRESSURE TURBINE, reference_data_and_literature: 2J-F108-14, criticality_code_justification: CZBJ AND FEAT. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-339-6142, 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
1317M36G05
NSN: 2840-01-339-6142
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 58828 — CFM INTERNATIONAL INC DBA CFM INTERNATIONAL (USA)
SPECIFICATIONS
design_typeAXIAL COMPRESSOR
special_featuresTWO BLADE ASSEMBLY
end_item_identificationF108 AIRCRAFT ENGINE
engine_section_locationHIGH PRESSURE TURBINE
reference_data_and_literature2J-F108-14
criticality_code_justificationCZBJ AND FEAT
part_name_assigned_by_controlling_agencyNOZZLE SEGMENT-HPT STATOR
NSN2840-01-339-6142
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available NOZZLE SEGMENT,TURBINE,AIRCRAFT TITLE COMPONENT PN 1317M36G05 MFR NOZZLE SEGMENT,TURBINE
KEY FEATURES
•
DESIGN TYPE: AXIAL COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: CZBJ AND FEAT
•
REFERENCE DATA AND LITERATURE: 2J-F108-14
•
ENGINE SECTION LOCATION: HIGH PRESSURE TURBINE
TECHNICAL CHARACTERISTICS
DESIGN TYPEAXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATIONCZBJ AND FEAT
REFERENCE DATA AND LITERATURE2J-F108-14
ENGINE SECTION LOCATIONHIGH PRESSURE TURBINE
SPECIAL FEATURESTWO BLADE ASSEMBLY
PART NAME ASSIGNED BY CONTROLLING AGENCYNOZZLE SEGMENT-HPT STATOR
END ITEM IDENTIFICATIONF108 AIRCRAFT ENGINE
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 6
9527M50G04Reference document
Same NSN cross-reference
Reference document — Secondary reference
1317M36G04Reference document
Same NSN cross-reference
Reference document — Secondary reference
9527M50G10Reference document
Same NSN cross-reference
Reference document — Secondary reference
9527M50G06Reference document
Same NSN cross-reference
Reference document — Secondary reference
9527M50G05Reference document
Same NSN cross-reference
Reference document — Secondary reference
1441M29G06Reference 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 1317M36G05?
1317M36G05 is a NOZZLE SEGMENT,TURBINE,AIRCRAFT.
What parts can replace 1317M36G05?
There are 6 known substitutes for 1317M36G05: 9527M50G04, 1317M36G04, 9527M50G10 and 3 more. Substitute compatibility should be verified for your specific system.
What is the NSN for 1317M36G05?
1317M36G05 is cataloged in the U.S. Government catalog under NSN 2840-01-339-6142. 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.