4084517-705C — ROTOR,COMPRESSOR,AIRCRAFT GAS TU

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4084517-705C: ROTOR,COMPRESSOR,AIRCRAFT GAS TU.

ROTOR,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include design_type: AXIAL COMPRESSOR, end_item_identification: F100-PW-229 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMPRESSOR, criticality_code_justification: FEAT AND CZBJ, part_name_assigned_by_controlling_agency: ORIGINAL NAME ROTOR AND STATOR ASSY, TURBINE REAR COMPRESSOR DRIVE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-448-6985, 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

4084517-705C

NSN: 2840-01-448-6985
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)

SPECIFICATIONS

design_type	AXIAL COMPRESSOR
stage_number	1
special_features	T.O. 2J-F100-54, FIG 86, IND 1; LOCATION NEAR THE REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY, TURBINE STATOR SUPPORT; USE ONLY ON P/N 4084522-800, -801, -802 AND 4082657-808
end_item_identification	F100-PW-229 AIRCRAFT GAS TURBINE ENGINE
engine_section_location	COMPRESSOR
criticality_code_justification	FEAT AND CZBJ
part_name_assigned_by_controlling_agency	ORIGINAL NAME ROTOR AND STATOR ASSY, TURBINE REAR COMPRESSOR DRIVE
NSN	2840-01-448-6985

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: FEAT AND CZBJ

•

ENGINE SECTION LOCATION: COMPRESSOR

TECHNICAL CHARACTERISTICS

STAGE NUMBER	1
DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	FEAT AND CZBJ
ENGINE SECTION LOCATION	COMPRESSOR
SPECIAL FEATURES	T.O. 2J-F100-54, FIG 86, IND 1; LOCATION NEAR THE REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY, TURBINE STATOR SUPPORT; USE ONLY ON P/N 4084522-800, -801, -802 AND 4082657-808
PART NAME ASSIGNED BY CONTROLLING AGENCY	ORIGINAL NAME ROTOR AND STATOR ASSY, TURBINE REAR COMPRESSOR DRIVE
END ITEM IDENTIFICATION	F100-PW-229 AIRCRAFT GAS TURBINE ENGINE

SUBSTITUTES & CROSS-REFERENCES 6

4084517-700Reference document

Same NSN cross-reference

Reference document — Secondary reference

2840PL2059384Reference document

Same NSN cross-reference

Reference document — Informative reference only

4083015-701Reference document

Same NSN cross-reference

Reference document — Secondary reference

2840PL1952213Reference document

Same NSN cross-reference

Reference document — Informative reference only

4084517Reference document

Same NSN cross-reference

Reference document — Drawing number reference only

4084517-705Reference document

Same NSN cross-reference

Reference document — Secondary reference

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 4084517-705C?

4084517-705C is a ROTOR,COMPRESSOR,AIRCRAFT GAS TU.

What parts can replace 4084517-705C?

There are 6 known substitutes for 4084517-705C: 4084517-700, 2840PL2059384, 4083015-701 and 3 more. Substitute compatibility should be verified for your specific system.

What is the NSN for 4084517-705C?

4084517-705C is cataloged in the U.S. Government catalog under NSN 2840-01-448-6985. This indicates validated use in U.S. government and defense supply chains.

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4084517-705C — ROTOR,COMPRESSOR,AIRCRAFT GAS TU

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