301-330-114-0 — BLADE,TURBINE ROTOR,AIRCRAFT GAS

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

301-330-114-0: BLADE,TURBINE ROTOR,AIRCRAFT GAS.

BLADE,TURBINE ROTOR,AIRCRAFT GAS. Key specifications include material: NICKEL ALLOY OVERALL, overall_length: 3.650 INCHES NOMINAL IN, end_item_identification: F108CF100 AND F108CF200, engine_section_location: LOW PRESSURE TURBINE, reference_data_and_literature: T.O. 2J-F108-14 FIG 9A IND 522C A, criticality_code_justification: AGAV.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-466-7430, 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

301-330-114-0

NSN: 2840-01-466-7430
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 58828 — CFM INTERNATIONAL INC DBA CFM INTERNATIONAL (USA)

SPECIFICATIONS

material	NICKEL ALLOY OVERALL
stage_number	1
overall_length	3.650 INCHES NOMINAL IN
end_item_identification	F108CF100 AND F108CF200
engine_section_location	LOW PRESSURE TURBINE
reference_data_and_literature	T.O. 2J-F108-14 FIG 9A IND 522C A
criticality_code_justification	AGAV
part_name_assigned_by_controlling_agency	BLADE-LPT ROTOR STG 1
NSN	2840-01-466-7430

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

REFERENCE DATA AND LITERATURE: T.O. 2J-F108-14 FIG 9A IND 522C A

•

ENGINE SECTION LOCATION: LOW PRESSURE TURBINE

•

MATERIAL: NICKEL ALLOY OVERALL

TECHNICAL CHARACTERISTICS

STAGE NUMBER	1
CRITICALITY CODE JUSTIFICATION	AGAV
REFERENCE DATA AND LITERATURE	T.O. 2J-F108-14 FIG 9A IND 522C A
OVERALL LENGTH	3.650 INCHES NOMINAL IN
ENGINE SECTION LOCATION	LOW PRESSURE TURBINE
PART NAME ASSIGNED BY CONTROLLING AGENCY	BLADE-LPT ROTOR STG 1
END ITEM IDENTIFICATION	F108CF100 AND F108CF200
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

301-330-113-0Reference 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 301-330-114-0?

301-330-114-0 is a BLADE,TURBINE ROTOR,AIRCRAFT GAS.

What parts can replace 301-330-114-0?

There is 1 known substitute for 301-330-114-0: 301-330-113-0. Substitute compatibility should be verified for your specific system.

What is the NSN for 301-330-114-0?

301-330-114-0 is cataloged in the U.S. Government catalog under NSN 2840-01-466-7430. This indicates validated use in U.S. government and defense supply chains.

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301-330-114-0 — BLADE,TURBINE ROTOR,AIRCRAFT GAS

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