9992M60G06-108 — DISK,COMPRESSOR,AIRCRAFT GAS TUR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9992M60G06-108: DISK,COMPRESSOR,AIRCRAFT GAS TUR.

DISK,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include diameter: 17.197 INCHES MINIMUM AND 17.201 INCHES MAXIMUM IN, material: TITANIUM OVERALL, design_type: AXIAL-CENTRIFUGAL, overall_length: 6.287 INCHES NOMINAL IN, end_item_identification: ACFT ENG F101-GE-100,F108-CF-100,F110-GE-100, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-147-0535, 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

9992M60G06-108

NSN: 2840-01-147-0535
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

diameter	17.197 INCHES MINIMUM AND 17.201 INCHES MAXIMUM IN
material	TITANIUM OVERALL
design_type	AXIAL-CENTRIFUGAL
stage_number	1
overall_length	6.287 INCHES NOMINAL IN
end_item_identification	ACFT ENG F101-GE-100,F108-CF-100,F110-GE-100
engine_section_location	COMPRESSOR
reference_data_and_literature	T.O. 2J-F108-4 FIG 72-31-00-01 IND 140B
part_name_assigned_by_controlling_agency	SPOOL-STAGES 1&2
NSN	2840-01-147-0535

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

DESIGN TYPE: AXIAL-CENTRIFUGAL

•

REFERENCE DATA AND LITERATURE: T.O. 2J-F108-4 FIG 72-31-00-01 IND 140B

•

DIAMETER: 17.197 INCHES MINIMUM AND 17.201 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: COMPRESSOR

TECHNICAL CHARACTERISTICS

STAGE NUMBER	1
DESIGN TYPE	AXIAL-CENTRIFUGAL
REFERENCE DATA AND LITERATURE	T.O. 2J-F108-4 FIG 72-31-00-01 IND 140B
DIAMETER	17.197 INCHES MINIMUM AND 17.201 INCHES MAXIMUM IN
OVERALL LENGTH	6.287 INCHES NOMINAL IN
ENGINE SECTION LOCATION	COMPRESSOR
PART NAME ASSIGNED BY CONTROLLING AGENCY	SPOOL-STAGES 1&2
END ITEM IDENTIFICATION	ACFT ENG F101-GE-100,F108-CF-100,F110-GE-100
MATERIAL	TITANIUM 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 1

9992M60G07Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Terminal item — no further procurement; issued until stock is exhaustedDemilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 9992M60G06-108?

9992M60G06-108 is a DISK,COMPRESSOR,AIRCRAFT GAS TUR.

What parts can replace 9992M60G06-108?

There is 1 known substitute for 9992M60G06-108: 9992M60G07. Substitute compatibility should be verified for your specific system.

What is the NSN for 9992M60G06-108?

9992M60G06-108 is cataloged in the U.S. Government catalog under NSN 2840-01-147-0535. This indicates validated use in U.S. government and defense supply chains.

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9992M60G06-108 — DISK,COMPRESSOR,AIRCRAFT GAS TUR

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