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305-390-901-0 — NOZZLE SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

305-390-901-0: NOZZLE SEGMENT,TURBINE,AIRCRAFT.

NOZZLE SEGMENT,TURBINE,AIRCRAFT. Key specifications include material: NICKEL ALLOY OVERALL, overall_width: 49.1 MILLIMETERS NOMINAL MM, overall_length: 169.7 MILLIMETERS NOMINAL MM, special_features: WAS VANE,TURBINE NOZZLE,TURBINE ENGINE; MATL RENE 77, end_item_identification: ACFT ENG F108, engine_section_location: LOW PRESSURE TURBINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-187-3198, 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
305-390-901-0
NSN: 2840-01-187-3198
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
overall_width49.1 MILLIMETERS NOMINAL MM
overall_length169.7 MILLIMETERS NOMINAL MM
special_featuresWAS VANE,TURBINE NOZZLE,TURBINE ENGINE; MATL RENE 77
end_item_identificationACFT ENG F108
engine_section_locationLOW PRESSURE TURBINE
reference_data_and_literatureT.O. 2J-F108-14 FIG 72-54-00 IND 7-140D
criticality_code_justificationAGAV
part_name_assigned_by_controlling_agencyNOZZLE SEGMENT ASSEMBLY-LPT STG 4
NSN2840-01-187-3198
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available NOZZLE SEGMENT,TURBINE,AIRCRAFT TITLE COMPONENT PN 305-390-901-0 MFR NOZZLE SEGMENT,TURBINE
KEY FEATURES
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
REFERENCE DATA AND LITERATURE: T.O. 2J-F108-14 FIG 72-54-00 IND 7-140D
•
ENGINE SECTION LOCATION: LOW PRESSURE TURBINE
TECHNICAL CHARACTERISTICS
CRITICALITY CODE JUSTIFICATIONAGAV
REFERENCE DATA AND LITERATURET.O. 2J-F108-14 FIG 72-54-00 IND 7-140D
OVERALL LENGTH169.7 MILLIMETERS NOMINAL MM
OVERALL WIDTH49.1 MILLIMETERS NOMINAL MM
ENGINE SECTION LOCATIONLOW PRESSURE TURBINE
SPECIAL FEATURESWAS VANE,TURBINE NOZZLE,TURBINE ENGINE; MATL RENE 77
PART NAME ASSIGNED BY CONTROLLING AGENCYNOZZLE SEGMENT ASSEMBLY-LPT STG 4
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 3
301-557-708-0Reference document
Same NSN cross-reference
Reference document — Secondary reference
305-390-902-0Reference document
Same NSN cross-reference
Reference document — Secondary reference
305-390-904-0Reference 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 305-390-901-0?
305-390-901-0 is a NOZZLE SEGMENT,TURBINE,AIRCRAFT.
What parts can replace 305-390-901-0?
There are 3 known substitutes for 305-390-901-0: 301-557-708-0, 305-390-902-0, 305-390-904-0. Substitute compatibility should be verified for your specific system.
What is the NSN for 305-390-901-0?
305-390-901-0 is cataloged in the U.S. Government catalog under NSN 2840-01-187-3198. This indicates validated use in U.S. government and defense supply chains.
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