705455 — SUPPORT,TURBINE NOZZLE,AIRCRAFT

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

705455: SUPPORT,TURBINE NOZZLE,AIRCRAFT.

SUPPORT,TURBINE NOZZLE,AIRCRAFT. Key specifications include material: NICKEL ALLOY, overall_length: 0.967 INCHES NOMINAL IN, inside_diameter: 23.110 INCHES MINIMUM AND 23.130 INCHES MAXIMUM IN, outside_diameter: 26.344 INCHES MINIMUM AND 26.348 INCHES MAXIMUM IN, mounting_hole_diameter: 0.214 INCHES MINIMUM AND 0.224 INCHES MAXIMUM IN, mounting_hole_quantity: 40. This part is cataloged in the U.S.

Government catalog under NSN 2840-00-413-0827, 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

705455

NSN: 2840-00-413-0827
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 77445 — RTX CORPORATION DBA PRATT & WHITNEY DIV PRATT &WHITNEY (USA)

SPECIFICATIONS

material	NICKEL ALLOY
overall_length	0.967 INCHES NOMINAL IN
inside_diameter	23.110 INCHES MINIMUM AND 23.130 INCHES MAXIMUM IN
outside_diameter	26.344 INCHES MINIMUM AND 26.348 INCHES MAXIMUM IN
mounting_hole_diameter	0.214 INCHES MINIMUM AND 0.224 INCHES MAXIMUM IN
mounting_hole_quantity	40
end_item_identification	TF-30 AIRCRAFT ENGINE
criticality_code_justification	AGAV
NSN	2840-00-413-0827

COMPONENT DIAGRAM

KEY FEATURES

•

MOUNTING HOLE QUANTITY: 40

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MOUNTING HOLE DIAMETER: 0.214 INCHES MINIMUM AND 0.224 INCHES MAXIMUM IN

•

OUTSIDE DIAMETER: 26.344 INCHES MINIMUM AND 26.348 INCHES MAXIMUM IN

•

INSIDE DIAMETER: 23.110 INCHES MINIMUM AND 23.130 INCHES MAXIMUM IN

•

MATERIAL: NICKEL ALLOY

TECHNICAL CHARACTERISTICS

MOUNTING HOLE QUANTITY	40
CRITICALITY CODE JUSTIFICATION	AGAV
MOUNTING HOLE DIAMETER	0.214 INCHES MINIMUM AND 0.224 INCHES MAXIMUM IN
OVERALL LENGTH	0.967 INCHES NOMINAL IN
OUTSIDE DIAMETER	26.344 INCHES MINIMUM AND 26.348 INCHES MAXIMUM IN
INSIDE DIAMETER	23.110 INCHES MINIMUM AND 23.130 INCHES MAXIMUM IN
END ITEM IDENTIFICATION	TF-30 AIRCRAFT ENGINE
MATERIAL	NICKEL ALLOY

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: Normally procured from the manufacturer (OEM)Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 705455?

705455 is a SUPPORT,TURBINE NOZZLE,AIRCRAFT.

What is the NSN for 705455?

705455 is cataloged in the U.S. Government catalog under NSN 2840-00-413-0827. This indicates validated use in U.S. government and defense supply chains.

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705455 — SUPPORT,TURBINE NOZZLE,AIRCRAFT

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