4038410 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

4038410: SEAL,AIR,AIRCRAFT GAS TURBINE EN.

SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include material: NICKEL ALLOY OVERALL, overall_height: 0.430 INCHES MINIMUM AND 0.450 INCHES MAXIMUM IN, overall_length: 1.104 INCHES MINIMUM AND 1.106 INCHES MAXIMUM IN, special_features: T.O. 2J-F100-4; GOES ON THE AUGMENTOR CONVERGENT NOZZLE SEGMENT; METALLIC HARDNESS DPH 353 MIN OR EQUIVALENT, material_thickness: 0.005 INCHES MINIMUM AND 0.007 INCHES MAXIMUM IN, end_item_identification: ENGINE,ACFT,TURBO-FAN,MODEL F100PW100.

This part is cataloged in the U.S. Government catalog under NSN 2840-00-348-6236, 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

4038410

NSN: 2840-00-348-6236
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
overall_height	0.430 INCHES MINIMUM AND 0.450 INCHES MAXIMUM IN
overall_length	1.104 INCHES MINIMUM AND 1.106 INCHES MAXIMUM IN
special_features	T.O. 2J-F100-4; GOES ON THE AUGMENTOR CONVERGENT NOZZLE SEGMENT; METALLIC HARDNESS DPH 353 MIN OR EQUIVALENT
material_thickness	0.005 INCHES MINIMUM AND 0.007 INCHES MAXIMUM IN
end_item_identification	ENGINE,ACFT,TURBO-FAN,MODEL F100PW100
engine_section_location	TURBINE
criticality_code_justification	AGAV
material_document_and_classification	AMS5596 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-00-348-6236

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5596 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

ENGINE SECTION LOCATION: TURBINE

•

MATERIAL THICKNESS: 0.005 INCHES MINIMUM AND 0.007 INCHES MAXIMUM IN

TECHNICAL CHARACTERISTICS

OVERALL HEIGHT	0.430 INCHES MINIMUM AND 0.450 INCHES MAXIMUM IN
CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5596 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
OVERALL LENGTH	1.104 INCHES MINIMUM AND 1.106 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	TURBINE
MATERIAL THICKNESS	0.005 INCHES MINIMUM AND 0.007 INCHES MAXIMUM IN
SPECIAL FEATURES	T.O. 2J-F100-4; GOES ON THE AUGMENTOR CONVERGENT NOZZLE SEGMENT; METALLIC HARDNESS DPH 353 MIN OR EQUIVALENT
END ITEM IDENTIFICATION	ENGINE,ACFT,TURBO-FAN,MODEL F100PW100
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 4038410?

4038410 is a SEAL,AIR,AIRCRAFT GAS TURBINE EN.

What is the NSN for 4038410?

4038410 is cataloged in the U.S. Government catalog under NSN 2840-00-348-6236. This indicates validated use in U.S. government and defense supply chains.

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4038410 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

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