9063M47P01 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9063M47P01: SEAL,AIR,AIRCRAFT GAS TURBINE EN.

SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include material: STEEL OVERALL, overall_length: 1.370 INCHES MINIMUM AND 1.430 INCHES MAXIMUM IN, special_features: T.O. 2J-TF39-4; SEAL IS SQUARE; 1HOLE 0.568-0.572 IN.

DIA.; MID FRAME LINER SUPPORT AND BEAM REPAIR IN, material_thickness: 0.023 INCHES MINIMUM AND 0.027 INCHES MAXIMUM IN, end_item_identification: ENGINE,ACFT,MODEL TF39-G1A, engine_section_location: LOW PRESSURE TURBINE. This part is cataloged in the U.S. Government catalog under NSN 2840-00-352-2212, 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

9063M47P01

NSN: 2840-00-352-2212
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	STEEL OVERALL
stage_number	1
overall_length	1.370 INCHES MINIMUM AND 1.430 INCHES MAXIMUM IN
special_features	T.O. 2J-TF39-4; SEAL IS SQUARE; 1HOLE 0.568-0.572 IN. DIA.; MID FRAME LINER SUPPORT AND BEAM REPAIR IN
material_thickness	0.023 INCHES MINIMUM AND 0.027 INCHES MAXIMUM IN
end_item_identification	ENGINE,ACFT,MODEL TF39-G1A
engine_section_location	LOW PRESSURE TURBINE
criticality_code_justification	AGAV
material_document_and_classification	AMS5537 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-00-352-2212

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 1

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5537 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

ENGINE SECTION LOCATION: LOW PRESSURE TURBINE

•

MATERIAL THICKNESS: 0.023 INCHES MINIMUM AND 0.027 INCHES MAXIMUM IN

TECHNICAL CHARACTERISTICS

STAGE NUMBER	1
CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5537 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
OVERALL LENGTH	1.370 INCHES MINIMUM AND 1.430 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	LOW PRESSURE TURBINE
MATERIAL THICKNESS	0.023 INCHES MINIMUM AND 0.027 INCHES MAXIMUM IN
SPECIAL FEATURES	T.O. 2J-TF39-4; SEAL IS SQUARE; 1HOLE 0.568-0.572 IN. DIA.; MID FRAME LINER SUPPORT AND BEAM REPAIR IN
END ITEM IDENTIFICATION	ENGINE,ACFT,MODEL TF39-G1A
MATERIAL	STEEL 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

2840PL0802068Reference document

Same NSN cross-reference

Reference document — Informative reference only

LIFECYCLE

NSN statusActive· U.S. Government catalog

No demilitarization required

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FREQUENTLY ASKED QUESTIONS

What is 9063M47P01?

9063M47P01 is a SEAL,AIR,AIRCRAFT GAS TURBINE EN.

What parts can replace 9063M47P01?

There is 1 known substitute for 9063M47P01: 2840PL0802068. Substitute compatibility should be verified for your specific system.

What is the NSN for 9063M47P01?

9063M47P01 is cataloged in the U.S. Government catalog under NSN 2840-00-352-2212. This indicates validated use in U.S. government and defense supply chains.

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9063M47P01 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

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