1881M11P01 — BLADE,TURBINE ROTOR,AIRCRAFT GAS

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1881M11P01: BLADE,TURBINE ROTOR,AIRCRAFT GAS.

BLADE,TURBINE ROTOR,AIRCRAFT GAS. Key specifications include material: NICKEL ALLOY BLADE, design_type: AXIAL COMPRESSOR, overall_length: 4.784 INCHES MINIMUM AND 4.794 INCHES MAXIMUM IN, blade_attachment_method: FIR TREE, end_item_identification: ACFT ENG F110GE129, engine_section_location: LOW PRESSURE TURBINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-447-2506, 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

1881M11P01

NSN: 2840-01-447-2506
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	NICKEL ALLOY BLADE
design_type	AXIAL COMPRESSOR
stage_number	1
overall_length	4.784 INCHES MINIMUM AND 4.794 INCHES MAXIMUM IN
blade_attachment_method	FIR TREE
end_item_identification	ACFT ENG F110GE129
engine_section_location	LOW PRESSURE TURBINE
reference_data_and_literature	2J-F110-14 FIG 90 IND 1
criticality_code_justification	AGAV
part_name_assigned_by_controlling_agency	BLADE,LOW PRESSURE TURBINE ROTOR-STAGE 1, MACH
NSN	2840-01-447-2506

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

REFERENCE DATA AND LITERATURE: 2J-F110-14 FIG 90 IND 1

•

BLADE ATTACHMENT METHOD: FIR TREE

•

ENGINE SECTION LOCATION: LOW PRESSURE TURBINE

TECHNICAL CHARACTERISTICS

STAGE NUMBER	1
DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	AGAV
REFERENCE DATA AND LITERATURE	2J-F110-14 FIG 90 IND 1
BLADE ATTACHMENT METHOD	FIR TREE
OVERALL LENGTH	4.784 INCHES MINIMUM AND 4.794 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	LOW PRESSURE TURBINE
PART NAME ASSIGNED BY CONTROLLING AGENCY	BLADE,LOW PRESSURE TURBINE ROTOR-STAGE 1, MACH
END ITEM IDENTIFICATION	ACFT ENG F110GE129
MATERIAL	NICKEL ALLOY BLADE

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

KDS 2840-4003Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Insurance item — stocked against contingency demandDemilitarization required — mutilation + specific procedure

Ready to buy 1881M11P01?

Compare prices from verified sellers on eBay

Buy on eBay →

As an eBay Partner, PartsTable may earn a commission. Your price is not affected.

FREQUENTLY ASKED QUESTIONS

What is 1881M11P01?

1881M11P01 is a BLADE,TURBINE ROTOR,AIRCRAFT GAS.

What parts can replace 1881M11P01?

There is 1 known substitute for 1881M11P01: KDS 2840-4003. Substitute compatibility should be verified for your specific system.

What is the NSN for 1881M11P01?

1881M11P01 is cataloged in the U.S. Government catalog under NSN 2840-01-447-2506. This indicates validated use in U.S. government and defense supply chains.

Community Feedback

1881M11P01 — BLADE,TURBINE ROTOR,AIRCRAFT GAS

Request a Quote — 1881M11P01