P121P03 — BLADE,COMPRESSOR,AIRCRAFT GAS TU

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

P121P03: BLADE,COMPRESSOR,AIRCRAFT GAS TU.

BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: TITANIUM ALLOY BLADE, design_type: COMPRESSOR, overall_width: 1.778 INCHES MINIMUM AND 1.783 INCHES MAXIMUM IN, overall_length: 3.814 INCHES NOMINAL IN, special_features: ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE, end_item_identification: ACFT ENG F101-GE-100 AND F110-GE-100. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-146-9443, 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

P121P03

NSN: 2840-01-146-9443
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	TITANIUM ALLOY BLADE
design_type	COMPRESSOR
stage_number	1
overall_width	1.778 INCHES MINIMUM AND 1.783 INCHES MAXIMUM IN
overall_length	3.814 INCHES NOMINAL IN
special_features	ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE
end_item_identification	ACFT ENG F101-GE-100 AND F110-GE-100
engine_section_location	LOW PRESSURE COMPRESSOR
criticality_code_justification	AGAV
NSN	2840-01-146-9443

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

DESIGN TYPE: COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

ENGINE SECTION LOCATION: LOW PRESSURE COMPRESSOR

TECHNICAL CHARACTERISTICS

STAGE NUMBER	1
DESIGN TYPE	COMPRESSOR
CRITICALITY CODE JUSTIFICATION	AGAV
OVERALL LENGTH	3.814 INCHES NOMINAL IN
OVERALL WIDTH	1.778 INCHES MINIMUM AND 1.783 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	LOW PRESSURE COMPRESSOR
SPECIAL FEATURES	ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE
END ITEM IDENTIFICATION	ACFT ENG F101-GE-100 AND F110-GE-100
MATERIAL	TITANIUM 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

P121P01Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — mutilation

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FREQUENTLY ASKED QUESTIONS

What is P121P03?

P121P03 is a BLADE,COMPRESSOR,AIRCRAFT GAS TU.

What parts can replace P121P03?

There is 1 known substitute for P121P03: P121P01. Substitute compatibility should be verified for your specific system.

What is the NSN for P121P03?

P121P03 is cataloged in the U.S. Government catalog under NSN 2840-01-146-9443. This indicates validated use in U.S. government and defense supply chains.

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P121P03 — BLADE,COMPRESSOR,AIRCRAFT GAS TU

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