1863M32P02-101 — SHAFT,TURBINE,AIRCRAFT GAS TURBI

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1863M32P02-101: SHAFT,TURBINE,AIRCRAFT GAS TURBI.

SHAFT,TURBINE,AIRCRAFT GAS TURBI. Key specifications include overall_length: 10.371 INCHES MINIMUM AND 10.381 INCHES MAXIMUM IN, end_item_identification: F101 ENGINE, engine_section_location: HIGH PRESSURE TURBINE, reference_data_and_literature: 2J-F101-4 FIG 56 IND 3, criticality_code_justification: AGAV, part_name_assigned_by_controlling_agency: SHAFT,FWD HPT ROTOR. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-511-0612, 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

1863M32P02-101

NSN: 2840-01-511-0612
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

overall_length	10.371 INCHES MINIMUM AND 10.381 INCHES MAXIMUM IN
end_item_identification	F101 ENGINE
engine_section_location	HIGH PRESSURE TURBINE
reference_data_and_literature	2J-F101-4 FIG 56 IND 3
criticality_code_justification	AGAV
part_name_assigned_by_controlling_agency	SHAFT,FWD HPT ROTOR
NSN	2840-01-511-0612

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

REFERENCE DATA AND LITERATURE: 2J-F101-4 FIG 56 IND 3

•

ENGINE SECTION LOCATION: HIGH PRESSURE TURBINE

TECHNICAL CHARACTERISTICS

CRITICALITY CODE JUSTIFICATION	AGAV
REFERENCE DATA AND LITERATURE	2J-F101-4 FIG 56 IND 3
OVERALL LENGTH	10.371 INCHES MINIMUM AND 10.381 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	HIGH PRESSURE TURBINE
PART NAME ASSIGNED BY CONTROLLING AGENCY	SHAFT,FWD HPT ROTOR
END ITEM IDENTIFICATION	F101 ENGINE

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

1863M32P01-101Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 1863M32P02-101?

1863M32P02-101 is a SHAFT,TURBINE,AIRCRAFT GAS TURBI.

What parts can replace 1863M32P02-101?

There is 1 known substitute for 1863M32P02-101: 1863M32P01-101. Substitute compatibility should be verified for your specific system.

What is the NSN for 1863M32P02-101?

1863M32P02-101 is cataloged in the U.S. Government catalog under NSN 2840-01-511-0612. This indicates validated use in U.S. government and defense supply chains.

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1863M32P02-101 — SHAFT,TURBINE,AIRCRAFT GAS TURBI

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