37D401302P101 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

37D401302P101: 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 2840-00-797-0380, 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

37D401302P101

NSN: 2840-00-797-0380
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 99207 — GENERAL ELECTRIC COMPANY DBA GE AEROSPACE (USA)

SPECIFICATIONS

diameter	10.440 INCHES MINIMUM AND 10.450 INCHES MAXIMUM IN
material	STEEL OVERALL
design_type	COMPRESSOR
stage_number	2
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
end_item_identification	ACFT ENG J85
engine_section_location	COMPRESSOR
part_name_assigned_by_controlling_agency	SEAL,AIR,GAS TURBINE ENGINE
NSN	2840-00-797-0380

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 2

•

DESIGN TYPE: COMPRESSOR

•

HARDNESS RATING: 37.0 ROCKWELL C MINIMUM AND 44.0 ROCKWELL C MAXIMUM OVERALL

•

DIAMETER: 10.440 INCHES MINIMUM AND 10.450 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: COMPRESSOR

TECHNICAL CHARACTERISTICS

STAGE NUMBER	2
DESIGN TYPE	COMPRESSOR
HARDNESS RATING	37.0 ROCKWELL C MINIMUM AND 44.0 ROCKWELL C MAXIMUM OVERALL
DIAMETER	10.440 INCHES MINIMUM AND 10.450 INCHES MAXIMUM IN
OVERALL LENGTH	1.450 INCHES MINIMUM AND 1.453 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMPRESSOR
SPECIAL FEATURES	T.O. 2J-J85-54; LIFE LIMITED
PART NAME ASSIGNED BY CONTROLLING AGENCY	SEAL,AIR,GAS TURBINE ENGINE
END ITEM IDENTIFICATION	ACFT ENG J85
MATERIAL	STEEL 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.

2840-00-004-4242 2840-00-021-4702 2840-00-043-0981 2840-00-043-0982 2840-00-048-5261 2840-00-407-9165 2840-01-171-0875

SUBSTITUTES & CROSS-REFERENCES

No substitute or cross-reference records for this part.

LIFECYCLE

NSN statusActive· U.S. Government catalog

No demilitarization required

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FREQUENTLY ASKED QUESTIONS

What is 37D401302P101?

37D401302P101 is a SEAL,AIR,AIRCRAFT GAS TURBINE EN.

What is the NSN for 37D401302P101?

37D401302P101 is cataloged in the U.S. Government catalog under NSN 2840-00-797-0380. This indicates validated use in U.S. government and defense supply chains.

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37D401302P101 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

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