3008T23P01 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

3008T23P01: SEAL,AIR,AIRCRAFT GAS TURBINE EN.

SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 13.709 INCHES MINIMUM AND 13.713 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, overall_width: 0.250 INCHES MINIMUM AND 0.270 INCHES MAXIMUM IN, overall_length: 0.025 INCHES NOMINAL IN, special_features: T.O. 2J-T64-14, FIG 12, IND 13; SAME NAVAIR 02B-105AJB-4, end_item_identification: ACFT ENG J79, J85, T58, T64.

This part is cataloged in the U.S. Government catalog under NSN 2840-00-885-0743, 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

3008T23P01

NSN: 2840-00-885-0743
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 99207 — GENERAL ELECTRIC COMPANY DBA GE AEROSPACE (USA)

SPECIFICATIONS

diameter	13.709 INCHES MINIMUM AND 13.713 INCHES MAXIMUM IN
material	NICKEL ALLOY OVERALL
overall_width	0.250 INCHES MINIMUM AND 0.270 INCHES MAXIMUM IN
overall_length	0.025 INCHES NOMINAL IN
special_features	T.O. 2J-T64-14, FIG 12, IND 13; SAME NAVAIR 02B-105AJB-4
end_item_identification	ACFT ENG J79, J85, T58, T64
engine_section_location	COMBUSTION CHAMBER
criticality_code_justification	CZBJ AND ABHP AND ABMZ AND ABMK
part_name_assigned_by_controlling_agency	ORIGINAL NAME PLATE,SEALING
NSN	2840-00-885-0743

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: CZBJ AND ABHP AND ABMZ AND ABMK

•

DIAMETER: 13.709 INCHES MINIMUM AND 13.713 INCHES MAXIMUM IN

•

ENGINE SECTION LOCATION: COMBUSTION CHAMBER

TECHNICAL CHARACTERISTICS

CRITICALITY CODE JUSTIFICATION	CZBJ AND ABHP AND ABMZ AND ABMK
DIAMETER	13.709 INCHES MINIMUM AND 13.713 INCHES MAXIMUM IN
OVERALL LENGTH	0.025 INCHES NOMINAL IN
OVERALL WIDTH	0.250 INCHES MINIMUM AND 0.270 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	COMBUSTION CHAMBER
SPECIAL FEATURES	T.O. 2J-T64-14, FIG 12, IND 13; SAME NAVAIR 02B-105AJB-4
PART NAME ASSIGNED BY CONTROLLING AGENCY	ORIGINAL NAME PLATE,SEALING
END ITEM IDENTIFICATION	ACFT ENG J79, J85, T58, T64
MATERIAL	NICKEL 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

Acquisition advice: Insurance item — stocked against contingency demandDemilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 3008T23P01?

3008T23P01 is a SEAL,AIR,AIRCRAFT GAS TURBINE EN.

What is the NSN for 3008T23P01?

3008T23P01 is cataloged in the U.S. Government catalog under NSN 2840-00-885-0743. This indicates validated use in U.S. government and defense supply chains.

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3008T23P01 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

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