3502957-6 — DUCT,EXHAUST,NONAIRCRAFT GAS TUR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

3502957-6: DUCT,EXHAUST,NONAIRCRAFT GAS TUR.

DUCT,EXHAUST,NONAIRCRAFT GAS TUR. Key specifications include material: NICKEL ALLOY OVERALL, overall_width: 10.540 INCHES MINIMUM AND 10.620 INCHES MAXIMUM IN, overall_length: 6.970 INCHES MINIMUM AND 7.030 INCHES MAXIMUM IN, end_item_identification: PACER SPECIAL; NEXT HIGHER ASSY 3505569; U/O 3505568, engine_section_location: EXHAUST, criticality_code_justification: AGAV. This part is cataloged in the U.S.

Government catalog under NSN 2835-01-386-6571, 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

3502957-6

NSN: 2835-01-386-6571
FSC: 2835 — Gas Turbines and Jet Engines; Non-aircraft Prime Mover, Aircraft Non-prime Mover, and Components
CAGE: 59364 — HONEYWELL INTERNATIONAL INC. DBA HONEYWELL INTERNATIONAL DIV AEROSPACE - TEMPE (WEST WARNER ROAD) (USA)

SPECIFICATIONS

material	NICKEL ALLOY OVERALL
overall_width	10.540 INCHES MINIMUM AND 10.620 INCHES MAXIMUM IN
overall_length	6.970 INCHES MINIMUM AND 7.030 INCHES MAXIMUM IN
special_features	CONTAINS HARDNESS CRITICAL ITEMS OR HARDNESS CRITICAL PROCESSES--ALL CHANGES TO OR PROPOSED SUBSTITUTIONS OF HCI/HCP ITEMS MUST BE EVALUATED FOR HARDNESS IMPACTS
end_item_identification	PACER SPECIAL; NEXT HIGHER ASSY 3505569; U/O 3505568
engine_section_location	EXHAUST
criticality_code_justification	AGAV
nuclear_hardness_critical_feature	HARDENED
NSN	2835-01-386-6571

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

ENGINE SECTION LOCATION: EXHAUST

•

MATERIAL: NICKEL ALLOY OVERALL

•

NUCLEAR HARDNESS CRITICAL FEATURE: HARDENED

TECHNICAL CHARACTERISTICS

CRITICALITY CODE JUSTIFICATION	AGAV
OVERALL LENGTH	6.970 INCHES MINIMUM AND 7.030 INCHES MAXIMUM IN
OVERALL WIDTH	10.540 INCHES MINIMUM AND 10.620 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	EXHAUST
SPECIAL FEATURES	CONTAINS HARDNESS CRITICAL ITEMS OR HARDNESS CRITICAL PROCESSES--ALL CHANGES TO OR PROPOSED SUBSTITUTIONS OF HCI/HCP ITEMS MUST BE EVALUATED FOR HARDNESS IMPACTS
END ITEM IDENTIFICATION	PACER SPECIAL; NEXT HIGHER ASSY 3505569; U/O 3505568
MATERIAL	NICKEL ALLOY OVERALL
NUCLEAR HARDNESS CRITICAL FEATURE	HARDENED

OTHER ITEMS IN FSC 2835 — Gas Turbines and Jet Engines; Non-aircraft Prime Mover, Aircraft Non-prime Mover, and Components

Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.

2835-00-055-1954 2835-00-076-6471 2835-00-082-1005 2835-00-318-9258 2835-00-340-7539 2835-00-340-7670 2835-00-356-2739 2835-00-716-4668

SUBSTITUTES & CROSS-REFERENCES 1

3502957-5Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

No demilitarization required

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FREQUENTLY ASKED QUESTIONS

What is 3502957-6?

3502957-6 is a DUCT,EXHAUST,NONAIRCRAFT GAS TUR.

What parts can replace 3502957-6?

There is 1 known substitute for 3502957-6: 3502957-5. Substitute compatibility should be verified for your specific system.

What is the NSN for 3502957-6?

3502957-6 is cataloged in the U.S. Government catalog under NSN 2835-01-386-6571. This indicates validated use in U.S. government and defense supply chains.

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3502957-6 — DUCT,EXHAUST,NONAIRCRAFT GAS TUR

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