9666M43P05 — DISK,FAN,AIRCRAFT GAS TURBINE EN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9666M43P05: DISK,FAN,AIRCRAFT GAS TURBINE EN.

DISK,FAN,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 33.189 INCHES MINIMUM AND 33.209 INCHES MAXIMUM IN, material: TITANIUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 6.693 INCHES NOMINAL IN, special_features: ORIGINAL NAME DISK,AXIAL COMPRESSOR,TURBINE ENGINE, end_item_identification: ACFT ENG TF-39. This part is cataloged in the U.S.

Government catalog under NSN 2840-00-103-0825, 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

9666M43P05

NSN: 2840-00-103-0825
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

diameter	33.189 INCHES MINIMUM AND 33.209 INCHES MAXIMUM IN
material	TITANIUM ALLOY OVERALL
design_type	AXIAL COMPRESSOR
stage_number	2
overall_length	6.693 INCHES NOMINAL IN
special_features	ORIGINAL NAME DISK,AXIAL COMPRESSOR,TURBINE ENGINE
end_item_identification	ACFT ENG TF-39
engine_section_location	COMPRESSOR
criticality_code_justification	AGAV
NSN	2840-00-103-0825

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 2

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

DIAMETER: 33.189 INCHES MINIMUM AND 33.209 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: COMPRESSOR

TYPICAL APPLICATIONS

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

TECHNICAL CHARACTERISTICS

STAGE NUMBER	2
DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	AGAV
DIAMETER	33.189 INCHES MINIMUM AND 33.209 INCHES MAXIMUM IN
OVERALL LENGTH	6.693 INCHES NOMINAL IN
ENGINE SECTION LOCATION	COMPRESSOR
SPECIAL FEATURES	ORIGINAL NAME DISK,AXIAL COMPRESSOR,TURBINE ENGINE
END ITEM IDENTIFICATION	ACFT ENG TF-39
MATERIAL	TITANIUM ALLOY 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 2

9666M43P04Reference document

Same NSN cross-reference

Reference document — Secondary reference

9666M43P03Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 9666M43P05?

9666M43P05 is a DISK,FAN,AIRCRAFT GAS TURBINE EN.

What parts can replace 9666M43P05?

There are 2 known substitutes for 9666M43P05: 9666M43P04, 9666M43P03. Substitute compatibility should be verified for your specific system.

What is the NSN for 9666M43P05?

9666M43P05 is cataloged in the U.S. Government catalog under NSN 2840-00-103-0825. This indicates validated use in U.S. government and defense supply chains.

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9666M43P05 — DISK,FAN,AIRCRAFT GAS TURBINE EN

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