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9686M18P25 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

9686M18P25: SEAL,AIR,AIRCRAFT GAS TURBINE EN.

SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include material: NICKEL ALLOY OVERALL, overall_width: 0.100 INCHES MINIMUM AND 0.110 INCHES MAXIMUM IN, overall_length: 1.720 INCHES MINIMUM AND 1.740 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 AND GAS TURBINE ENG LM2500.

This part is cataloged in the U.S. Government catalog under NSN 2840-00-112-2163, 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
9686M18P25
NSN: 2840-00-112-2163
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
materialNICKEL ALLOY OVERALL
stage_number2
overall_width0.100 INCHES MINIMUM AND 0.110 INCHES MAXIMUM IN
overall_length1.720 INCHES MINIMUM AND 1.740 INCHES MAXIMUM IN
special_featuresT.O. 2J-TF39-4; TURBINE NOZZLE
material_thickness0.004 INCHES MINIMUM AND 0.007 INCHES MAXIMUM IN
end_item_identificationACFT ENG TF-39 AND GAS TURBINE ENG LM2500
engine_section_locationHIGH PRESSURE TURBINE
NSN2840-00-112-2163
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available SEAL,AIR,AIRCRAFT GAS TURBINE EN TITLE COMPONENT PN 9686M18P25 MFR SEAL,AIR,AIRCRAFT GAS
KEY FEATURES
•
STAGE NUMBER: 2
•
ENGINE SECTION LOCATION: HIGH PRESSURE TURBINE
•
MATERIAL THICKNESS: 0.004 INCHES MINIMUM AND 0.007 INCHES MAXIMUM IN
•
MATERIAL: NICKEL ALLOY OVERALL
TECHNICAL CHARACTERISTICS
STAGE NUMBER2
OVERALL LENGTH1.720 INCHES MINIMUM AND 1.740 INCHES MAXIMUM IN
OVERALL WIDTH0.100 INCHES MINIMUM AND 0.110 INCHES MAXIMUM IN
ENGINE SECTION LOCATIONHIGH PRESSURE TURBINE
MATERIAL THICKNESS0.004 INCHES MINIMUM AND 0.007 INCHES MAXIMUM IN
SPECIAL FEATUREST.O. 2J-TF39-4; TURBINE NOZZLE
END ITEM IDENTIFICATIONACFT ENG TF-39 AND GAS TURBINE ENG LM2500
MATERIALNICKEL 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 3
2840PL0786409Reference document
Same NSN cross-reference
Reference document — Informative reference only
9686M18P16Reference document
Same NSN cross-reference
Reference document — Secondary reference
9686M18P12Reference document
Same NSN cross-reference
Reference document — Secondary reference
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 9686M18P25?
9686M18P25 is a SEAL,AIR,AIRCRAFT GAS TURBINE EN.
What parts can replace 9686M18P25?
There are 3 known substitutes for 9686M18P25: 2840PL0786409, 9686M18P16, 9686M18P12. Substitute compatibility should be verified for your specific system.
What is the NSN for 9686M18P25?
9686M18P25 is cataloged in the U.S. Government catalog under NSN 2840-00-112-2163. This indicates validated use in U.S. government and defense supply chains.
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