1317M74P02 — LOCK,FAN BLADE,AIRCRAFT GAS TURB

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1317M74P02: LOCK,FAN BLADE,AIRCRAFT GAS TURB.

LOCK,FAN BLADE,AIRCRAFT GAS TURB. Key specifications include material: STEEL, overall_width: 0.210 INCHES MINIMUM AND 0.226 INCHES MAXIMUM IN, overall_length: 10.832 INCHES NOMINAL IN, special_features: WIDTH OF RESTRAINED 0.214-0.218; T.O. 2J-F110-14,FAN STATOR ASSY, material_thickness: 0.007 INCHES MINIMUM AND 0.009 INCHES MAXIMUM IN, end_item_identification: F110GE129 AIRCRAFT ENGINE.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-215-3610, 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

1317M74P02

NSN: 2840-01-215-3610
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	STEEL
stage_number	1
overall_width	0.210 INCHES MINIMUM AND 0.226 INCHES MAXIMUM IN
overall_length	10.832 INCHES NOMINAL IN
special_features	WIDTH OF RESTRAINED 0.214-0.218; T.O. 2J-F110-14,FAN STATOR ASSY
material_thickness	0.007 INCHES MINIMUM AND 0.009 INCHES MAXIMUM IN
end_item_identification	F110GE129 AIRCRAFT ENGINE
criticality_code_justification	AGAV
material_document_and_classification	AMS5537 ASSN STD SINGLE MATERIAL RESPONSE
NSN	2840-01-215-3610

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5537 ASSN STD SINGLE MATERIAL RESPONSE

•

MATERIAL THICKNESS: 0.007 INCHES MINIMUM AND 0.009 INCHES MAXIMUM IN

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
CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5537 ASSN STD SINGLE MATERIAL RESPONSE
OVERALL LENGTH	10.832 INCHES NOMINAL IN
OVERALL WIDTH	0.210 INCHES MINIMUM AND 0.226 INCHES MAXIMUM IN
MATERIAL THICKNESS	0.007 INCHES MINIMUM AND 0.009 INCHES MAXIMUM IN
SPECIAL FEATURES	WIDTH OF RESTRAINED 0.214-0.218; T.O. 2J-F110-14,FAN STATOR ASSY
END ITEM IDENTIFICATION	F110GE129 AIRCRAFT ENGINE
MATERIAL	STEEL

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

No substitute or cross-reference records for this part.

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 1317M74P02?

1317M74P02 is a LOCK,FAN BLADE,AIRCRAFT GAS TURB.

What is the NSN for 1317M74P02?

1317M74P02 is cataloged in the U.S. Government catalog under NSN 2840-01-215-3610. This indicates validated use in U.S. government and defense supply chains.

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1317M74P02 — LOCK,FAN BLADE,AIRCRAFT GAS TURB

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