1796M20G02 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1796M20G02: SEAL,AIR,AIRCRAFT GAS TURBINE EN.

SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 28.730 INCHES MINIMUM AND 28.850 INCHES MAXIMUM IN, material: TITANIUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 2.370 INCHES MINIMUM AND 2.450 INCHES MAXIMUM IN, end_item_identification: TF-39 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: HIGH PRESSURE TURBINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-444-7692, 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

1796M20G02

NSN: 2840-01-444-7692
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

diameter	28.730 INCHES MINIMUM AND 28.850 INCHES MAXIMUM IN
material	TITANIUM ALLOY OVERALL
design_type	AXIAL COMPRESSOR
stage_number	2
overall_length	2.370 INCHES MINIMUM AND 2.450 INCHES MAXIMUM IN
end_item_identification	TF-39 AIRCRAFT GAS TURBINE ENGINE
engine_section_location	HIGH PRESSURE TURBINE
criticality_code_justification	FEAT AND ABHP AND ABMZ AND CZBJ
material_document_and_classification	B50TF25 CL-A MFR REF SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-01-444-7692

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 2

•

DESIGN TYPE: AXIAL COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: FEAT AND ABHP AND ABMZ AND CZBJ

•

MATERIAL DOCUMENT AND CLASSIFICATION: B50TF25 CL-A MFR REF SINGLE MATERIAL RESPONSE OVERALL

•

DIAMETER: 28.730 INCHES MINIMUM AND 28.850 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: HIGH PRESSURE TURBINE

TECHNICAL CHARACTERISTICS

STAGE NUMBER	2
DESIGN TYPE	AXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATION	FEAT AND ABHP AND ABMZ AND CZBJ
MATERIAL DOCUMENT AND CLASSIFICATION	B50TF25 CL-A MFR REF SINGLE MATERIAL RESPONSE OVERALL
DIAMETER	28.730 INCHES MINIMUM AND 28.850 INCHES MAXIMUM IN
OVERALL LENGTH	2.370 INCHES MINIMUM AND 2.450 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	HIGH PRESSURE TURBINE
SPECIAL FEATURES	T.O 2J-TF39-4, FIG 62, IND 35; ECP 369; DCN 97-37; HONEYCOMBED; REPLACES P/N 9083M60G06; DO NOT GRP PER ECP/DCN, WHOLE NEW CONFIGURATION; ONCE THE OLD CONFIG IS REPL BY THE TCTO KITS WITH THE NEW P/N, THE OLD CONFIG IS THROWN AWAY; INTERSTAGE SEAL; NOT I&S ABLE
END ITEM IDENTIFICATION	TF-39 AIRCRAFT GAS TURBINE ENGINE
MATERIAL	TITANIUM ALLOY 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

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 1796M20G02?

1796M20G02 is a SEAL,AIR,AIRCRAFT GAS TURBINE EN.

What is the NSN for 1796M20G02?

1796M20G02 is cataloged in the U.S. Government catalog under NSN 2840-01-444-7692. This indicates validated use in U.S. government and defense supply chains.

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1796M20G02 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

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