2840PL0788966 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

2840PL0788966: SEAL,AIR,AIRCRAFT GAS TURBINE EN.

SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 25.004 INCHES MINIMUM AND 25.008 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 0.258 INCHES MINIMUM AND 0.268 INCHES MAXIMUM IN, end_item_identification: F100-PW-229 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMBUSTION CHAMBER. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-448-7035, 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

2840PL0788966

NSN: 2840-01-448-7035
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 9009H — JEDNOLITY INDEKS MATERIALOWY - UNIFORM MATERIAL INDEX (POL)

SPECIFICATIONS

diameter	25.004 INCHES MINIMUM AND 25.008 INCHES MAXIMUM IN
material	NICKEL ALLOY OVERALL
design_type	AXIAL COMPRESSOR
stage_number	1
overall_length	0.258 INCHES MINIMUM AND 0.268 INCHES MAXIMUM IN
end_item_identification	F100-PW-229 AIRCRAFT GAS TURBINE ENGINE
engine_section_location	COMBUSTION CHAMBER
criticality_code_justification	CZBJ AND ABHP AND ABMZ AND FEAT
material_document_and_classification	AMS5599 ASSN STD 1ST MATERIAL RESPONSE OR AMS5666 ASSN STD 2ND MATERIAL RESPONSE OVERALL
part_name_assigned_by_controlling_agency	ORIGINAL NAME SEAL BRUSH,COMBUSTION CHAMBER,OUTER ASSEMBLY
NSN	2840-01-448-7035

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: CZBJ AND ABHP AND ABMZ AND FEAT

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5599 ASSN STD 1ST MATERIAL RESPONSE OR AMS5666 ASSN STD 2ND MATERIAL RESPONSE OVERALL

•

DIAMETER: 25.004 INCHES MINIMUM AND 25.008 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: COMBUSTION CHAMBER

TECHNICAL CHARACTERISTICS

STAGE NUMBER	1
DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	CZBJ AND ABHP AND ABMZ AND FEAT
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5599 ASSN STD 1ST MATERIAL RESPONSE OR AMS5666 ASSN STD 2ND MATERIAL RESPONSE OVERALL
DIAMETER	25.004 INCHES MINIMUM AND 25.008 INCHES MAXIMUM IN
OVERALL LENGTH	0.258 INCHES MINIMUM AND 0.268 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMBUSTION CHAMBER
SPECIAL FEATURES	T.O. 2J-F100-54, FIG 86, IND 19F; USE ONLY ON P/NS 4083194, 4083560, AND 4083565; CONTAINS WIRE BRUSH, 2250-2650 WIRES PER CIRCUMFERENTIAL INCH; LOCATED NEAR THE REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY; TURBINE STATOR SUPPORT AND COMBUSTION CHAMBER
PART NAME ASSIGNED BY CONTROLLING AGENCY	ORIGINAL NAME SEAL BRUSH,COMBUSTION CHAMBER,OUTER ASSEMBLY
END ITEM IDENTIFICATION	F100-PW-229 AIRCRAFT GAS TURBINE ENGINE

SUBSTITUTES & CROSS-REFERENCES 2

4083197Reference document

Same NSN cross-reference

Reference document — Drawing number reference only

4083197-01Same 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 2840PL0788966?

2840PL0788966 is a SEAL,AIR,AIRCRAFT GAS TURBINE EN.

What parts can replace 2840PL0788966?

There are 2 known substitutes for 2840PL0788966: 4083197, 4083197-01. Substitute compatibility should be verified for your specific system.

What is the NSN for 2840PL0788966?

2840PL0788966 is cataloged in the U.S. Government catalog under NSN 2840-01-448-7035. This indicates validated use in U.S. government and defense supply chains.

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2840PL0788966 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

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