9686M18P24 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9686M18P24: SEAL,AIR,AIRCRAFT GAS TURBINE EN.

SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include material: NICKEL ALLOY OVERALL, overall_width: 0.185 INCHES MINIMUM AND 0.195 INCHES MAXIMUM IN, overall_length: 1.730 INCHES MINIMUM AND 1.750 INCHES MAXIMUM IN, special_features: T.O. 2J-TF39-4; TURBINE NOZZLE, material_thickness: 0.011 INCHES NOMINAL IN, end_item_identification: ACFT ENG TF-39.

This part is cataloged in the U.S. Government catalog under NSN 2840-00-111-1017, 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

9686M18P24

NSN: 2840-00-111-1017
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	NICKEL ALLOY OVERALL
stage_number	2
overall_width	0.185 INCHES MINIMUM AND 0.195 INCHES MAXIMUM IN
overall_length	1.730 INCHES MINIMUM AND 1.750 INCHES MAXIMUM IN
special_features	T.O. 2J-TF39-4; TURBINE NOZZLE
material_thickness	0.011 INCHES NOMINAL IN
end_item_identification	ACFT ENG TF-39
engine_section_location	HIGH PRESSURE TURBINE
criticality_code_justification	AGAV
material_document_and_classification	AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-00-111-1017

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 2

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

ENGINE SECTION LOCATION: HIGH PRESSURE TURBINE

•

MATERIAL THICKNESS: 0.011 INCHES NOMINAL IN

TECHNICAL CHARACTERISTICS

STAGE NUMBER	2
CRITICALITY CODE JUSTIFICATION	AGAV
MATERIAL DOCUMENT AND CLASSIFICATION	AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
OVERALL LENGTH	1.730 INCHES MINIMUM AND 1.750 INCHES MAXIMUM IN
OVERALL WIDTH	0.185 INCHES MINIMUM AND 0.195 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	HIGH PRESSURE TURBINE
MATERIAL THICKNESS	0.011 INCHES NOMINAL IN
SPECIAL FEATURES	T.O. 2J-TF39-4; TURBINE NOZZLE
END ITEM IDENTIFICATION	ACFT ENG TF-39
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 2

2840PL0786323Reference document

Same NSN cross-reference

Reference document — Informative reference only

9686M18P08Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Insurance item — stocked against contingency demandNo demilitarization required

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FREQUENTLY ASKED QUESTIONS

What is 9686M18P24?

9686M18P24 is a SEAL,AIR,AIRCRAFT GAS TURBINE EN.

What parts can replace 9686M18P24?

There are 2 known substitutes for 9686M18P24: 2840PL0786323, 9686M18P08. Substitute compatibility should be verified for your specific system.

What is the NSN for 9686M18P24?

9686M18P24 is cataloged in the U.S. Government catalog under NSN 2840-00-111-1017. This indicates validated use in U.S. government and defense supply chains.

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9686M18P24 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

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