1499M31P09 — DISK AND HUB,FAN,AIRCRAFT GAS TU

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1499M31P09: DISK AND HUB,FAN,AIRCRAFT GAS TU.

DISK AND HUB,FAN,AIRCRAFT GAS TU. Key specifications include material: TITANIUM ALLOY DISK, design_type: AXIAL COMPRESSOR, overall_width: 10.000 INCHES NOMINAL IN, overall_length: 16.600 INCHES NOMINAL IN, special_features: T.0. 2J-F110-14, FIG 23, IND 15, end_item_identification: ACFT ENG F110.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-442-1886, 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

1499M31P09

NSN: 2840-01-442-1886
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	TITANIUM ALLOY DISK
design_type	AXIAL COMPRESSOR
stage_number	1
overall_width	10.000 INCHES NOMINAL IN
overall_length	16.600 INCHES NOMINAL IN
special_features	T.0. 2J-F110-14, FIG 23, IND 15
end_item_identification	ACFT ENG F110
engine_section_location	FAN
reference_data_and_literature	2J-F110-14 FIG 23 IND 15
part_name_assigned_by_controlling_agency	ORIGINAL NAME DISK,FAN,AIRCRAFT GAS TURBINE ENGINE
NSN	2840-01-442-1886

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

DESIGN TYPE: AXIAL COMPRESSOR

•

REFERENCE DATA AND LITERATURE: 2J-F110-14 FIG 23 IND 15

•

ENGINE SECTION LOCATION: FAN

TYPICAL APPLICATIONS

Server thermal management and cooling
Hot-swap fan replacement in production environments
Redundant cooling for high-availability systems

TECHNICAL CHARACTERISTICS

STAGE NUMBER	1
DESIGN TYPE	AXIAL COMPRESSOR
REFERENCE DATA AND LITERATURE	2J-F110-14 FIG 23 IND 15
OVERALL LENGTH	16.600 INCHES NOMINAL IN
OVERALL WIDTH	10.000 INCHES NOMINAL IN
ENGINE SECTION LOCATION	FAN
SPECIAL FEATURES	T.0. 2J-F110-14, FIG 23, IND 15
PART NAME ASSIGNED BY CONTROLLING AGENCY	ORIGINAL NAME DISK,FAN,AIRCRAFT GAS TURBINE ENGINE
END ITEM IDENTIFICATION	ACFT ENG F110
MATERIAL	TITANIUM ALLOY DISK

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 2

1499M31P08Reference document

Disk and Hub,fan,aircraft Gas Tu

Reference document — Secondary reference

1499M31P07Reference document

Disk and Hub,fan,aircraft Gas Tu

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 1499M31P09?

1499M31P09 is a DISK AND HUB,FAN,AIRCRAFT GAS TU.

What parts can replace 1499M31P09?

There are 2 known substitutes for 1499M31P09: 1499M31P08, 1499M31P07. Substitute compatibility should be verified for your specific system.

What is the NSN for 1499M31P09?

1499M31P09 is cataloged in the U.S. Government catalog under NSN 2840-01-442-1886. This indicates validated use in U.S. government and defense supply chains.

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1499M31P09 — DISK AND HUB,FAN,AIRCRAFT GAS TU

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