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37D401302P103 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

37D401302P103: SEAL,AIR,AIRCRAFT GAS TURBINE EN.

SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 10.440 INCHES MINIMUM AND 10.450 INCHES MAXIMUM IN, material: STEEL OVERALL, design_type: COMPRESSOR, overall_length: 1.450 INCHES MINIMUM AND 1.453 INCHES MAXIMUM IN, hardness_rating: 37.0 ROCKWELL C MINIMUM AND 44.0 ROCKWELL C MAXIMUM OVERALL, special_features: T.O. 2J-J85-54; LIFE LIMITED.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-068-2048, 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
37D401302P103
NSN: 2840-01-068-2048
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 99207 — GENERAL ELECTRIC COMPANY DBA GE AEROSPACE (USA)
SPECIFICATIONS
diameter10.440 INCHES MINIMUM AND 10.450 INCHES MAXIMUM IN
materialSTEEL OVERALL
design_typeCOMPRESSOR
stage_number2
overall_length1.450 INCHES MINIMUM AND 1.453 INCHES MAXIMUM IN
hardness_rating37.0 ROCKWELL C MINIMUM AND 44.0 ROCKWELL C MAXIMUM OVERALL
special_featuresT.O. 2J-J85-54; LIFE LIMITED
end_item_identificationACFT ENG J85-GE-5,-13,-17
engine_section_locationCOMPRESSOR
criticality_code_justificationAGAV
NSN2840-01-068-2048
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available SEAL,AIR,AIRCRAFT GAS TURBINE EN TITLE COMPONENT PN 37D401302P103 MFR SEAL,AIR,AIRCRAFT GAS
KEY FEATURES
•
STAGE NUMBER: 2
•
DESIGN TYPE: COMPRESSOR
•
HARDNESS RATING: 37.0 ROCKWELL C MINIMUM AND 44.0 ROCKWELL C MAXIMUM OVERALL
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
DIAMETER: 10.440 INCHES MINIMUM AND 10.450 INCHES MAXIMUM IN
•
ENGINE SECTION LOCATION: COMPRESSOR
TECHNICAL CHARACTERISTICS
STAGE NUMBER2
DESIGN TYPECOMPRESSOR
HARDNESS RATING37.0 ROCKWELL C MINIMUM AND 44.0 ROCKWELL C MAXIMUM OVERALL
CRITICALITY CODE JUSTIFICATIONAGAV
DIAMETER10.440 INCHES MINIMUM AND 10.450 INCHES MAXIMUM IN
OVERALL LENGTH1.450 INCHES MINIMUM AND 1.453 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONCOMPRESSOR
SPECIAL FEATUREST.O. 2J-J85-54; LIFE LIMITED
END ITEM IDENTIFICATIONACFT ENG J85-GE-5,-13,-17
MATERIALSTEEL 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

No substitute or cross-reference records for this part.

LIFECYCLE
NSN statusActive· U.S. Government catalog
Acquisition advice: Insurance item — stocked against contingency demandDemilitarization required — critical (Q)
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FREQUENTLY ASKED QUESTIONS
What is 37D401302P103?
37D401302P103 is a SEAL,AIR,AIRCRAFT GAS TURBINE EN.
What is the NSN for 37D401302P103?
37D401302P103 is cataloged in the U.S. Government catalog under NSN 2840-01-068-2048. This indicates validated use in U.S. government and defense supply chains.
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✓ PartsTable — the parts reference. Every fact cited to its source.
PartsTable Design LLC · partstable.com
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-18.
PartsTable commercial catalog: edition Unified commercial catalog snapshot through 2026-09-28, edition date not on file, retrieved 2026-09-28.