305-390-504-0 — NOZZLE SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

305-390-504-0: NOZZLE SEGMENT,TURBINE,AIRCRAFT.

NOZZLE SEGMENT,TURBINE,AIRCRAFT. Key specifications include diameter: 425.0 MILLIMETERS NOMINAL MM, material: NICKEL ALLOY OVERALL, overall_length: 8.500 INCHES NOMINAL IN, special_features: MATERIALRENE 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 2840-01-187-3196, 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

305-390-504-0

NSN: 2840-01-187-3196
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 58828 — CFM INTERNATIONAL INC DBA CFM INTERNATIONAL (USA)

SPECIFICATIONS

diameter	425.0 MILLIMETERS NOMINAL MM
material	NICKEL ALLOY OVERALL
stage_number	2
overall_length	8.500 INCHES NOMINAL IN
special_features	MATERIALRENE 77
end_item_identification	ACFT ENG F108
engine_section_location	LOW PRESSURE TURBINE
reference_data_and_literature	T.O. 2J-F108-14, FIG 72-54-00-9, IND 240D
criticality_code_justification	AGAV
part_name_assigned_by_controlling_agency	NOZZLESEG. ASSY-LPT STG 2
NSN	2840-01-187-3196

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 2

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

REFERENCE DATA AND LITERATURE: T.O. 2J-F108-14, FIG 72-54-00-9, IND 240D

•

DIAMETER: 425.0 MILLIMETERS NOMINAL MM

•

ENGINE SECTION LOCATION: LOW PRESSURE TURBINE

TECHNICAL CHARACTERISTICS

STAGE NUMBER	2
CRITICALITY CODE JUSTIFICATION	AGAV
REFERENCE DATA AND LITERATURE	T.O. 2J-F108-14, FIG 72-54-00-9, IND 240D
DIAMETER	425.0 MILLIMETERS NOMINAL MM
OVERALL LENGTH	8.500 INCHES NOMINAL IN
ENGINE SECTION LOCATION	LOW PRESSURE TURBINE
SPECIAL FEATURES	MATERIALRENE 77
PART NAME ASSIGNED BY CONTROLLING AGENCY	NOZZLESEG. ASSY-LPT STG 2
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.

2840-00-004-4242 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 4

305-390-507-0Reference document

Same NSN cross-reference

Reference document — Secondary reference

305-390-506-0Reference document

Same NSN cross-reference

Reference document — Secondary reference

305-390-503-0Reference document

Same NSN cross-reference

Reference document — Secondary reference

305-390-510-0Reference 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 305-390-504-0?

305-390-504-0 is a NOZZLE SEGMENT,TURBINE,AIRCRAFT.

What parts can replace 305-390-504-0?

There are 4 known substitutes for 305-390-504-0: 305-390-507-0, 305-390-506-0, 305-390-503-0 and 1 more. Substitute compatibility should be verified for your specific system.

What is the NSN for 305-390-504-0?

305-390-504-0 is cataloged in the U.S. Government catalog under NSN 2840-01-187-3196. This indicates validated use in U.S. government and defense supply chains.

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305-390-504-0 — NOZZLE SEGMENT,TURBINE,AIRCRAFT

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