PartsTable
Technical Data Sheet
Download PDF

2840PL0786409 — SEAL,AIR,AIRCRAFT GAS TURBINE EN

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

2840PL0786409: 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
2840PL0786409
NSN: 2840-00-112-2163
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 9009H — JEDNOLITY INDEKS MATERIALOWY - UNIFORM MATERIAL INDEX (POL)
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 2840PL0786409 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 2
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
Ready to buy 2840PL0786409?
Compare prices from verified sellers on eBay
Buy on eBay →
As an eBay Partner, PartsTable may earn a commission. Your price is not affected.
FREQUENTLY ASKED QUESTIONS
What is 2840PL0786409?
2840PL0786409 is a SEAL,AIR,AIRCRAFT GAS TURBINE EN.
What parts can replace 2840PL0786409?
There are 2 known substitutes for 2840PL0786409: 9686M18P16, 9686M18P12. Substitute compatibility should be verified for your specific system.
What is the NSN for 2840PL0786409?
2840PL0786409 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.
Community Feedback
Leave a Comment
Comments are reviewed before appearing. You will receive an email to verify before your comment appears.

Request a Quote — 2840PL0786409