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555665 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

555665: SEAL,AIR,AIRCRAFT GAS TURBINE EN.

SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 24.900 INCHES NOMINAL IN, material: STEEL OVERALL, design_type: AXIAL COMPRESSOR, stage_number: 10, overall_length: 1.134 INCHES MINIMUM AND 1.154 INCHES MAXIMUM IN, hardness_rating: 30.0 ROCKWELL C NOMINAL OVERALL. This part is cataloged in the U.S.

Government catalog under NSN 2840-00-227-8889, 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
555665
NSN: 2840-00-227-8889
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)
SPECIFICATIONS
diameter24.900 INCHES NOMINAL IN
materialSTEEL OVERALL
design_typeAXIAL COMPRESSOR
stage_number10
overall_length1.134 INCHES MINIMUM AND 1.154 INCHES MAXIMUM IN
hardness_rating30.0 ROCKWELL C NOMINAL OVERALL
special_featuresT.O. 2J-J75-4, FIG 13, IND 12; CASE-REAR COMPRESSOR FRONT
surface_treatmentNICKEL AND CADMIUM OVERALL
end_item_identificationJ-75 AIRCRAFT ENGINE
engine_section_locationCOMPRESSOR
criticality_code_justificationCZBJ AND SFTT AND ABMZ AND ABHP AND FEAT
part_name_assigned_by_controlling_agencyORIGINAL NAME RING,COMPRESSOR ROTOR,AIRCRAFT GAS TURBINE ENGINE
NSN2840-00-227-8889
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available SEAL,AIR,AIRCRAFT GAS TURBINE EN TITLE COMPONENT PN 555665 MFR SEAL,AIR,AIRCRAFT GAS
KEY FEATURES
•
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION: AMS2416 ASSN STD SINGLE TREATMENT RESPONSE OVERALL
•
STAGE NUMBER: 10
•
DESIGN TYPE: AXIAL COMPRESSOR
•
HARDNESS RATING: 30.0 ROCKWELL C NOMINAL OVERALL
•
CRITICALITY CODE JUSTIFICATION: CZBJ AND SFTT AND ABMZ AND ABHP AND FEAT
•
DIAMETER: 24.900 INCHES NOMINAL IN
•
ENGINE SECTION LOCATION: COMPRESSOR
TECHNICAL CHARACTERISTICS
SURFACE TREATMENT DOCUMENT AND CLASSIFICATIONAMS2416 ASSN STD SINGLE TREATMENT RESPONSE OVERALL
STAGE NUMBER10
DESIGN TYPEAXIAL COMPRESSOR
HARDNESS RATING30.0 ROCKWELL C NOMINAL OVERALL
CRITICALITY CODE JUSTIFICATIONCZBJ AND SFTT AND ABMZ AND ABHP AND FEAT
DIAMETER24.900 INCHES NOMINAL IN
OVERALL LENGTH1.134 INCHES MINIMUM AND 1.154 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONCOMPRESSOR
SPECIAL FEATUREST.O. 2J-J75-4, FIG 13, IND 12; CASE-REAR COMPRESSOR FRONT
SURFACE TREATMENTNICKEL AND CADMIUM OVERALL
SUBSTITUTES & CROSS-REFERENCES 1
309770Reference document
Same NSN cross-reference
Reference document — Secondary reference
LIFECYCLE
NSN statusActive· U.S. Government catalog
Acquisition advice: Terminal item — stock exhausted; no further procurementDemilitarization required — mutilation
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FREQUENTLY ASKED QUESTIONS
What is 555665?
555665 is a SEAL,AIR,AIRCRAFT GAS TURBINE EN.
What parts can replace 555665?
There is 1 known substitute for 555665: 309770. Substitute compatibility should be verified for your specific system.
What is the NSN for 555665?
555665 is cataloged in the U.S. Government catalog under NSN 2840-00-227-8889. This indicates validated use in U.S. government and defense supply chains.
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