565854CL6 — NOZZLE,TURBINE,AIRCRAFT GAS TURB

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

565854CL6: NOZZLE,TURBINE,AIRCRAFT GAS TURB.

NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include material: NICKEL ALLOY VANE, overall_width: 2.390 INCHES NOMINAL IN, overall_length: 8.740 INCHES NOMINAL IN, special_features: T.O. 2J-TF33-14, FIG 30, IND 19; 4.853-4.884 SQ IN, material_thickness: 1.245 INCHES NOMINAL IN, end_item_identification: TF33 AIRCRAFT ENGINE.

This part is cataloged in the U.S. Government catalog under NSN 2840-00-962-1263, 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

565854CL6

NSN: 2840-00-962-1263
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)

SPECIFICATIONS

material	NICKEL ALLOY VANE
stage_number	4
overall_width	2.390 INCHES NOMINAL IN
overall_length	8.740 INCHES NOMINAL IN
special_features	T.O. 2J-TF33-14, FIG 30, IND 19; 4.853-4.884 SQ IN
material_thickness	1.245 INCHES NOMINAL IN
end_item_identification	TF33 AIRCRAFT ENGINE
engine_section_location	TURBINE
criticality_code_justification	FEATG
material_document_and_classification	AMS5388 ASSN STD SINGLE MATERIAL RESPONSE VANE
part_name_assigned_by_controlling_agency	WAS VANE,TURBINE NOZZLE,TURBINE ENGINE
NSN	2840-00-962-1263

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 4

•

CRITICALITY CODE JUSTIFICATION: FEATG

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5388 ASSN STD SINGLE MATERIAL RESPONSE VANE

•

ENGINE SECTION LOCATION: TURBINE

•

MATERIAL THICKNESS: 1.245 INCHES NOMINAL IN

TECHNICAL CHARACTERISTICS

STAGE NUMBER	4
CRITICALITY CODE JUSTIFICATION	FEATG
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5388 ASSN STD SINGLE MATERIAL RESPONSE VANE
OVERALL LENGTH	8.740 INCHES NOMINAL IN
OVERALL WIDTH	2.390 INCHES NOMINAL IN
ENGINE SECTION LOCATION	TURBINE
MATERIAL THICKNESS	1.245 INCHES NOMINAL IN
SPECIAL FEATURES	T.O. 2J-TF33-14, FIG 30, IND 19; 4.853-4.884 SQ IN
PART NAME ASSIGNED BY CONTROLLING AGENCY	WAS VANE,TURBINE NOZZLE,TURBINE ENGINE
END ITEM IDENTIFICATION	TF33 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.

2840-00-004-4242 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 1

495254CL6Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 565854CL6?

565854CL6 is a NOZZLE,TURBINE,AIRCRAFT GAS TURB.

What parts can replace 565854CL6?

There is 1 known substitute for 565854CL6: 495254CL6. Substitute compatibility should be verified for your specific system.

What is the NSN for 565854CL6?

565854CL6 is cataloged in the U.S. Government catalog under NSN 2840-00-962-1263. This indicates validated use in U.S. government and defense supply chains.

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565854CL6 — NOZZLE,TURBINE,AIRCRAFT GAS TURB

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