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6866634 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

6866634: SEAL,AIR,AIRCRAFT GAS TURBINE EN.

SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 10.046 INCHES NOMINAL IN, material: ALUMINUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 1.280 INCHES NOMINAL IN, end_item_identification: TF-41 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: TURBINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-00-236-5002, 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
6866634
NSN: 2840-00-236-5002
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 63005 — ROLLS-ROYCE CORPORATION (USA)
SPECIFICATIONS
diameter10.046 INCHES NOMINAL IN
materialALUMINUM ALLOY OVERALL
design_typeAXIAL COMPRESSOR
overall_length1.280 INCHES NOMINAL IN
end_item_identificationTF-41 AIRCRAFT GAS TURBINE ENGINE
engine_section_locationTURBINE
criticality_code_justificationAPGF AND CZBJ AND ABHP AND ABMZ
material_document_and_classificationAMS4217 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
part_name_assigned_by_controlling_agencyORIGINAL NAME SEAL,STATIC REAR
NSN2840-00-236-5002
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available SEAL,AIR,AIRCRAFT GAS TURBINE EN TITLE COMPONENT PN 6866634 MFR SEAL,AIR,AIRCRAFT GAS
KEY FEATURES
•
DESIGN TYPE: AXIAL COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: APGF AND CZBJ AND ABHP AND ABMZ
•
MATERIAL DOCUMENT AND CLASSIFICATION: AMS4217 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
•
DIAMETER: 10.046 INCHES NOMINAL IN
•
ENGINE SECTION LOCATION: TURBINE
TECHNICAL CHARACTERISTICS
DESIGN TYPEAXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATIONAPGF AND CZBJ AND ABHP AND ABMZ
MATERIAL DOCUMENT AND CLASSIFICATIONAMS4217 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DIAMETER10.046 INCHES NOMINAL IN
OVERALL LENGTH1.280 INCHES NOMINAL IN
ENGINE SECTION LOCATIONTURBINE
PART NAME ASSIGNED BY CONTROLLING AGENCYORIGINAL NAME SEAL,STATIC REAR
END ITEM IDENTIFICATIONTF-41 AIRCRAFT GAS TURBINE ENGINE
MATERIALALUMINUM 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
6860782Reference document
Same NSN cross-reference
Reference document — Secondary reference
LIFECYCLE
NSN statusActive· U.S. Government catalog
Acquisition advice: Terminal item — stock exhausted; no further procurementNo demilitarization required
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FREQUENTLY ASKED QUESTIONS
What is 6866634?
6866634 is a SEAL,AIR,AIRCRAFT GAS TURBINE EN.
What parts can replace 6866634?
There is 1 known substitute for 6866634: 6860782. Substitute compatibility should be verified for your specific system.
What is the NSN for 6866634?
6866634 is cataloged in the U.S. Government catalog under NSN 2840-00-236-5002. This indicates validated use in U.S. government and defense supply chains.
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