9686M18P11 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9686M18P11: SEAL,AIR,AIRCRAFT GAS TURBINE EN.

SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include material: NICKEL ALLOY DISK, overall_width: 0.100 INCHES MINIMUM AND 0.110 INCHES MAXIMUM IN, overall_length: 1.920 INCHES MINIMUM AND 1.940 INCHES MAXIMUM IN, special_features: T.O. 2J-TF39-4;TURBINE NOZZLE, material_thickness: 0.004 INCHES MINIMUM AND 0.007 INCHES MAXIMUM IN, end_item_identification: ACFT ENG TF-39.

This part is cataloged in the U.S. Government catalog under NSN 2840-00-112-2164, 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

9686M18P11

NSN: 2840-00-112-2164
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	NICKEL ALLOY DISK
stage_number	2
overall_width	0.100 INCHES MINIMUM AND 0.110 INCHES MAXIMUM IN
overall_length	1.920 INCHES MINIMUM AND 1.940 INCHES MAXIMUM IN
special_features	T.O. 2J-TF39-4;TURBINE NOZZLE
material_thickness	0.004 INCHES MINIMUM AND 0.007 INCHES MAXIMUM IN
end_item_identification	ACFT ENG TF-39
engine_section_location	HIGH PRESSURE TURBINE
material_document_and_classification	AMS 5536 ASSN STD SINGLE MATERIAL RESPONSE DISK
NSN	2840-00-112-2164

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 2

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS 5536 ASSN STD SINGLE MATERIAL RESPONSE DISK

•

ENGINE SECTION LOCATION: HIGH PRESSURE TURBINE

•

MATERIAL THICKNESS: 0.004 INCHES MINIMUM AND 0.007 INCHES MAXIMUM IN

TECHNICAL CHARACTERISTICS

STAGE NUMBER	2
MATERIAL DOCUMENT AND CLASSIFICATION	AMS 5536 ASSN STD SINGLE MATERIAL RESPONSE DISK
OVERALL LENGTH	1.920 INCHES MINIMUM AND 1.940 INCHES MAXIMUM IN
OVERALL WIDTH	0.100 INCHES MINIMUM AND 0.110 INCHES MAXIMUM IN
ENGINE SECTION LOCATION	HIGH PRESSURE TURBINE
MATERIAL THICKNESS	0.004 INCHES MINIMUM AND 0.007 INCHES MAXIMUM IN
SPECIAL FEATURES	T.O. 2J-TF39-4;TURBINE NOZZLE
END ITEM IDENTIFICATION	ACFT ENG TF-39
MATERIAL	NICKEL ALLOY DISK

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

9686M18P15Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

2840PL0786415Reference document

Same NSN cross-reference

Reference document — Informative reference only

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Normally procured from the manufacturer (OEM)No demilitarization required

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FREQUENTLY ASKED QUESTIONS

What is 9686M18P11?

9686M18P11 is a SEAL,AIR,AIRCRAFT GAS TURBINE EN.

What parts can replace 9686M18P11?

There are 2 known substitutes for 9686M18P11: 9686M18P15, 2840PL0786415. Substitute compatibility should be verified for your specific system.

What is the NSN for 9686M18P11?

9686M18P11 is cataloged in the U.S. Government catalog under NSN 2840-00-112-2164. This indicates validated use in U.S. government and defense supply chains.

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9686M18P11 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

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