1476M11P02 — BLADE,FAN,AIRCRAFT GAS TURBINE E

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1476M11P02: BLADE,FAN,AIRCRAFT GAS TURBINE E.

BLADE,FAN,AIRCRAFT GAS TURBINE E. Key specifications include diameter: 18.924 INCHES MAXIMUM IN, material: TITANIUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_width: 3.098 INCHES MINIMUM AND 3.102 INCHES MAXIMUM IN, overall_length: 11.348 INCHES MINIMUM AND 11.358 INCHES MAXIMUM IN, special_features: MATL TITANIUM; STAGE 1; SLOT BLADE ATTACHMENT METHOD. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-371-9462, 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

1476M11P02

NSN: 2840-01-371-9462
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

diameter	18.924 INCHES MAXIMUM IN
material	TITANIUM ALLOY OVERALL
design_type	AXIAL COMPRESSOR
stage_number	1
overall_width	3.098 INCHES MINIMUM AND 3.102 INCHES MAXIMUM IN
overall_length	11.348 INCHES MINIMUM AND 11.358 INCHES MAXIMUM IN
special_features	MATL TITANIUM; STAGE 1; SLOT BLADE ATTACHMENT METHOD
blade_attachment_method	SLOT
end_item_identification	F110-GE-129 AIRCRAFT ENGINE
engine_section_location	FAN
reference_data_and_literature	2J-F110-14
NSN	2840-01-371-9462

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

DESIGN TYPE: AXIAL COMPRESSOR

•

REFERENCE DATA AND LITERATURE: 2J-F110-14

•

BLADE ATTACHMENT METHOD: SLOT

•

DIAMETER: 18.924 INCHES MAXIMUM IN

•

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
BLADE ATTACHMENT METHOD	SLOT
DIAMETER	18.924 INCHES MAXIMUM IN
OVERALL LENGTH	11.348 INCHES MINIMUM AND 11.358 INCHES MAXIMUM IN
OVERALL WIDTH	3.098 INCHES MINIMUM AND 3.102 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	FAN
SPECIAL FEATURES	MATL TITANIUM; STAGE 1; SLOT BLADE ATTACHMENT METHOD
END ITEM IDENTIFICATION	F110-GE-129 AIRCRAFT 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.

2840-00-004-4242 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

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

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FREQUENTLY ASKED QUESTIONS

What is 1476M11P02?

1476M11P02 is a BLADE,FAN,AIRCRAFT GAS TURBINE E.

What is the NSN for 1476M11P02?

1476M11P02 is cataloged in the U.S. Government catalog under NSN 2840-01-371-9462. This indicates validated use in U.S. government and defense supply chains.

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1476M11P02 — BLADE,FAN,AIRCRAFT GAS TURBINE E

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