1292M19G02 — FRAME,TURBINE,AIRCRAFT GAS TURBI

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1292M19G02: FRAME,TURBINE,AIRCRAFT GAS TURBI.

FRAME,TURBINE,AIRCRAFT GAS TURBI. Key specifications include material: STEEL, overall_length: 10.310 INCHES MINIMUM AND 10.340 INCHES MAXIMUM IN, inside_diameter: 15.200 INCHES MINIMUM AND 15.203 INCHES MAXIMUM IN, outside_diameter: 50.200 INCHES MINIMUM AND 50.240 INCHES MAXIMUM IN, end_item_identification: TF39 ENGINE, reference_data_and_literature: 2J-TF39-4 FIGURE 69 INDEX 17. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-468-3016, 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

1292M19G02

NSN: 2840-01-468-3016
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	STEEL
overall_length	10.310 INCHES MINIMUM AND 10.340 INCHES MAXIMUM IN
inside_diameter	15.200 INCHES MINIMUM AND 15.203 INCHES MAXIMUM IN
outside_diameter	50.200 INCHES MINIMUM AND 50.240 INCHES MAXIMUM IN
end_item_identification	TF39 ENGINE
reference_data_and_literature	2J-TF39-4 FIGURE 69 INDEX 17
criticality_code_justification	AGAV
number_of_variable_guide_vanes	8
NSN	2840-01-468-3016

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

REFERENCE DATA AND LITERATURE: 2J-TF39-4 FIGURE 69 INDEX 17

•

OUTSIDE DIAMETER: 50.200 INCHES MINIMUM AND 50.240 INCHES MAXIMUM IN

•

NUMBER OF VARIABLE GUIDE VANES: 8

•

INSIDE DIAMETER: 15.200 INCHES MINIMUM AND 15.203 INCHES MAXIMUM IN

•

MATERIAL: STEEL

TECHNICAL CHARACTERISTICS

CRITICALITY CODE JUSTIFICATION	AGAV
REFERENCE DATA AND LITERATURE	2J-TF39-4 FIGURE 69 INDEX 17
OVERALL LENGTH	10.310 INCHES MINIMUM AND 10.340 INCHES MAXIMUM IN
OUTSIDE DIAMETER	50.200 INCHES MINIMUM AND 50.240 INCHES MAXIMUM IN
NUMBER OF VARIABLE GUIDE VANES	8
INSIDE DIAMETER	15.200 INCHES MINIMUM AND 15.203 INCHES MAXIMUM IN
END ITEM IDENTIFICATION	TF39 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 — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 1292M19G02?

1292M19G02 is a FRAME,TURBINE,AIRCRAFT GAS TURBI.

What is the NSN for 1292M19G02?

1292M19G02 is cataloged in the U.S. Government catalog under NSN 2840-01-468-3016. This indicates validated use in U.S. government and defense supply chains.

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1292M19G02 — FRAME,TURBINE,AIRCRAFT GAS TURBI

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