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1499M30G02 — CASE,COMPRESSOR,AIRCRAFT GAS TUR

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

1499M30G02: CASE,COMPRESSOR,AIRCRAFT GAS TUR.

CASE,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include diameter: 30.000 INCHES NOMINAL IN, material: TITANIUM OVERALL, overall_width: 27.500 INCHES NOMINAL IN, overall_length: 21.500 INCHES NOMINAL IN, special_features: COMPRESSOR CASE ONLY, WITHOUT VANES, end_item_identification: F108 ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-312-2268, 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
1499M30G02
NSN: 2840-01-312-2268
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 58828 — CFM INTERNATIONAL INC DBA CFM INTERNATIONAL (USA)
SPECIFICATIONS
diameter30.000 INCHES NOMINAL IN
materialTITANIUM OVERALL
overall_width27.500 INCHES NOMINAL IN
overall_length21.500 INCHES NOMINAL IN
special_featuresCOMPRESSOR CASE ONLY, WITHOUT VANES
end_item_identificationF108 ENGINE
engine_section_locationHIGH PRESSURE COMPRESSOR
reference_data_and_literatureT.O. 2J-F108-14 FIG. 72-32-00-5B, IND. 130A A
criticality_code_justificationAGAV
part_name_assigned_by_controlling_agencyCASE ASSEMBLY-COMPRESSOR STATOR
NSN2840-01-312-2268
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available CASE,COMPRESSOR,AIRCRAFT GAS TUR TITLE COMPONENT PN 1499M30G02 MFR CASE,COMPRESSOR,AIRCRA
KEY FEATURES
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
REFERENCE DATA AND LITERATURE: T.O. 2J-F108-14 FIG. 72-32-00-5B, IND. 130A A
•
DIAMETER: 30.000 INCHES NOMINAL IN
•
ENGINE SECTION LOCATION: HIGH PRESSURE COMPRESSOR
TECHNICAL CHARACTERISTICS
CRITICALITY CODE JUSTIFICATIONAGAV
REFERENCE DATA AND LITERATURET.O. 2J-F108-14 FIG. 72-32-00-5B, IND. 130A A
DIAMETER30.000 INCHES NOMINAL IN
OVERALL LENGTH21.500 INCHES NOMINAL IN
OVERALL WIDTH27.500 INCHES NOMINAL IN
ENGINE SECTION LOCATIONHIGH PRESSURE COMPRESSOR
SPECIAL FEATURESCOMPRESSOR CASE ONLY, WITHOUT VANES
PART NAME ASSIGNED BY CONTROLLING AGENCYCASE ASSEMBLY-COMPRESSOR STATOR
END ITEM IDENTIFICATIONF108 ENGINE
MATERIALTITANIUM 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
1499M30G03Reference 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 1499M30G02?
1499M30G02 is a CASE,COMPRESSOR,AIRCRAFT GAS TUR.
What parts can replace 1499M30G02?
There is 1 known substitute for 1499M30G02: 1499M30G03. Substitute compatibility should be verified for your specific system.
What is the NSN for 1499M30G02?
1499M30G02 is cataloged in the U.S. Government catalog under NSN 2840-01-312-2268. This indicates validated use in U.S. government and defense supply chains.
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