305-390-411-0 — NOZZLE SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

305-390-411-0: NOZZLE SEGMENT,TURBINE,AIRCRAFT.

NOZZLE SEGMENT,TURBINE,AIRCRAFT. Key specifications include material: NICKEL ALLOY OVERALL, overall_length: 9.000 INCHES NOMINAL IN, end_item_identification: ACFT ENG F108, engine_section_location: LOW PRESSURE TURBINE, reference_data_and_literature: T.O.2J-F108-14 FIG 72-54-00-09A, IND 280E A, criticality_code_justification: AGAV. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-340-9213, 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

305-390-411-0

NSN: 2840-01-340-9213
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	NICKEL ALLOY OVERALL
overall_length	9.000 INCHES NOMINAL IN
end_item_identification	ACFT ENG F108
engine_section_location	LOW PRESSURE TURBINE
reference_data_and_literature	T.O.2J-F108-14 FIG 72-54-00-09A, IND 280E A
criticality_code_justification	AGAV
part_name_assigned_by_controlling_agency	NOZZLE SEG ASSY-LPT STG2
NSN	2840-01-340-9213

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

REFERENCE DATA AND LITERATURE: T.O.2J-F108-14 FIG 72-54-00-09A, IND 280E A

•

ENGINE SECTION LOCATION: LOW PRESSURE TURBINE

•

MATERIAL: NICKEL ALLOY OVERALL

TECHNICAL CHARACTERISTICS

CRITICALITY CODE JUSTIFICATION	AGAV
REFERENCE DATA AND LITERATURE	T.O.2J-F108-14 FIG 72-54-00-09A, IND 280E A
OVERALL LENGTH	9.000 INCHES NOMINAL IN
ENGINE SECTION LOCATION	LOW PRESSURE TURBINE
PART NAME ASSIGNED BY CONTROLLING AGENCY	NOZZLE SEG ASSY-LPT STG2
END ITEM IDENTIFICATION	ACFT ENG F108
MATERIAL	NICKEL 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.

2840-00-000-0048 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 1

305-390-408-0Reference 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 305-390-411-0?

305-390-411-0 is a NOZZLE SEGMENT,TURBINE,AIRCRAFT.

What parts can replace 305-390-411-0?

There is 1 known substitute for 305-390-411-0: 305-390-408-0. Substitute compatibility should be verified for your specific system.

What is the NSN for 305-390-411-0?

305-390-411-0 is cataloged in the U.S. Government catalog under NSN 2840-01-340-9213. This indicates validated use in U.S. government and defense supply chains.

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305-390-411-0 — NOZZLE SEGMENT,TURBINE,AIRCRAFT

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