4083877-02 — VANE ASSEMBLY,COMPRESSOR,AIRCRAF

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4083877-02: VANE ASSEMBLY,COMPRESSOR,AIRCRAF.

VANE ASSEMBLY,COMPRESSOR,AIRCRAF. Key specifications include diameter: 24.401 INCHES MINIMUM AND 24.405 INCHES MAXIMUM IN, material: NICKEL ALLOY VANE, design_type: AXIAL COMPRESSOR, overall_length: 3.327 INCHES MINIMUM AND 3.341 INCHES MAXIMUM IN, special_features: NE NAME TO BE VANE SEGMENT,COMPRESSOR,TURBINE ENGINE; NO. OF VANES IN SEGMENT IS APPROX 10, end_item_identification: F100PW0229 AIRCRAFT ENGINE.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-368-6493, 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

4083877-02

NSN: 2840-01-368-6493
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)

SPECIFICATIONS

diameter	24.401 INCHES MINIMUM AND 24.405 INCHES MAXIMUM IN
material	NICKEL ALLOY VANE
design_type	AXIAL COMPRESSOR
stage_number	7
overall_length	3.327 INCHES MINIMUM AND 3.341 INCHES MAXIMUM IN
special_features	NE NAME TO BE VANE SEGMENT,COMPRESSOR,TURBINE ENGINE; NO. OF VANES IN SEGMENT IS APPROX 10
end_item_identification	F100PW0229 AIRCRAFT ENGINE
engine_section_location	COMPRESSOR
reference_data_and_literature	T.O.2J-F100-54 F96 I81
criticality_code_justification	AGAV
NSN	2840-01-368-6493

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 7

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

REFERENCE DATA AND LITERATURE: T.O.2J-F100-54 F96 I81

•

DIAMETER: 24.401 INCHES MINIMUM AND 24.405 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: COMPRESSOR

TECHNICAL CHARACTERISTICS

STAGE NUMBER	7
DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	AGAV
REFERENCE DATA AND LITERATURE	T.O.2J-F100-54 F96 I81
DIAMETER	24.401 INCHES MINIMUM AND 24.405 INCHES MAXIMUM IN
OVERALL LENGTH	3.327 INCHES MINIMUM AND 3.341 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMPRESSOR
SPECIAL FEATURES	NE NAME TO BE VANE SEGMENT,COMPRESSOR,TURBINE ENGINE; NO. OF VANES IN SEGMENT IS APPROX 10
END ITEM IDENTIFICATION	F100PW0229 AIRCRAFT ENGINE
MATERIAL	NICKEL ALLOY VANE

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 2

4077877-02Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

2840PL0818199Reference document

Same NSN cross-reference

Reference document — Informative reference only

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Terminal item — no further procurement; issued until stock is exhaustedDemilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 4083877-02?

4083877-02 is a VANE ASSEMBLY,COMPRESSOR,AIRCRAF.

What parts can replace 4083877-02?

There are 2 known substitutes for 4083877-02: 4077877-02, 2840PL0818199. Substitute compatibility should be verified for your specific system.

What is the NSN for 4083877-02?

4083877-02 is cataloged in the U.S. Government catalog under NSN 2840-01-368-6493. This indicates validated use in U.S. government and defense supply chains.

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4083877-02 — VANE ASSEMBLY,COMPRESSOR,AIRCRAF

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