1319M57G01 — CASE,COMPRESSOR,AIRCRAFT GAS TUR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1319M57G01: CASE,COMPRESSOR,AIRCRAFT GAS TUR.

CASE,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include diameter: 30.000 INCHES NOMINAL IN, material: TITANIUM OVERALL, design_type: AXIAL COMPRESSOR, overall_width: 27.500 INCHES NOMINAL IN, overall_length: 21.500 INCHES NOMINAL IN, special_features: ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-255-4405, 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

1319M57G01

NSN: 2840-01-255-4405
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 58828 — CFM INTERNATIONAL INC DBA CFM INTERNATIONAL (USA)

SPECIFICATIONS

diameter	30.000 INCHES NOMINAL IN
material	TITANIUM OVERALL
design_type	AXIAL COMPRESSOR
overall_width	27.500 INCHES NOMINAL IN
overall_length	21.500 INCHES NOMINAL IN
special_features	ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE
end_item_identification	ACFT.ENG. F108
engine_section_location	TURBINE
reference_data_and_literature	T.O. 2J-F108-14 FIG.72-32-00 IAL M152 STEEL, CONSISTS OF CASE ONLY WITHOUT VANES
criticality_code_justification	AGAV
NSN	2840-01-255-4405

COMPONENT DIAGRAM

KEY FEATURES

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

REFERENCE DATA AND LITERATURE: T.O. 2J-F108-14 FIG.72-32-00 IAL M152 STEEL, CONSISTS OF CASE ONLY WITHOUT VANES

•

DIAMETER: 30.000 INCHES NOMINAL IN

•

ENGINE SECTION LOCATION: TURBINE

TECHNICAL CHARACTERISTICS

DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	AGAV
REFERENCE DATA AND LITERATURE	T.O. 2J-F108-14 FIG.72-32-00 IAL M152 STEEL, CONSISTS OF CASE ONLY WITHOUT VANES
DIAMETER	30.000 INCHES NOMINAL IN
OVERALL LENGTH	21.500 INCHES NOMINAL IN
OVERALL WIDTH	27.500 INCHES NOMINAL IN
ENGINE SECTION LOCATION	TURBINE
SPECIAL FEATURES	ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE
END ITEM IDENTIFICATION	ACFT.ENG. F108
MATERIAL	TITANIUM 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 1

1319M57G03Reference document

Same NSN cross-reference

Reference document — Secondary reference

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 1319M57G01?

1319M57G01 is a CASE,COMPRESSOR,AIRCRAFT GAS TUR.

What parts can replace 1319M57G01?

There is 1 known substitute for 1319M57G01: 1319M57G03. Substitute compatibility should be verified for your specific system.

What is the NSN for 1319M57G01?

1319M57G01 is cataloged in the U.S. Government catalog under NSN 2840-01-255-4405. This indicates validated use in U.S. government and defense supply chains.

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1319M57G01 — CASE,COMPRESSOR,AIRCRAFT GAS TUR

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