PartsTable
Technical Data Sheet
Download PDF

2840PL0696901 — SHROUD SEGMENT,TURBINE,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

2840PL0696901: SHROUD SEGMENT,TURBINE,AIRCRAFT.

SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include diameter: 19.207 INCHES MINIMUM AND 19.213 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 0.846 INCHES NOMINAL IN, special_features: T.O. 2J-F100-54, material_thickness: 0.486 INCHES NOMINAL IN.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-321-4453, 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
2840PL0696901
NSN: 2840-01-321-4453
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 9009H — JEDNOLITY INDEKS MATERIALOWY - UNIFORM MATERIAL INDEX (POL)
SPECIFICATIONS
diameter19.207 INCHES MINIMUM AND 19.213 INCHES MAXIMUM IN
materialNICKEL ALLOY OVERALL
design_typeAXIAL COMPRESSOR
stage_number4
overall_length0.846 INCHES NOMINAL IN
special_featuresT.O. 2J-F100-54
material_thickness0.486 INCHES NOMINAL IN
end_item_identificationF100PW0229 AIRCRAFT ENGINE
engine_section_locationCOMPRESSOR
criticality_code_justificationAGAV
NSN2840-01-321-4453
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available SHROUD SEGMENT,TURBINE,AIRCRAFT TITLE COMPONENT PN 2840PL0696901 MFR SHROUD SEGMENT,TURBINE
KEY FEATURES
•
STAGE NUMBER: 4
•
DESIGN TYPE: AXIAL COMPRESSOR
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
DIAMETER: 19.207 INCHES MINIMUM AND 19.213 INCHES MAXIMUM IN
•
ENGINE SECTION LOCATION: COMPRESSOR
•
MATERIAL THICKNESS: 0.486 INCHES NOMINAL IN
TECHNICAL CHARACTERISTICS
STAGE NUMBER4
DESIGN TYPEAXIAL COMPRESSOR
CRITICALITY CODE JUSTIFICATIONAGAV
DIAMETER19.207 INCHES MINIMUM AND 19.213 INCHES MAXIMUM IN
OVERALL LENGTH0.846 INCHES NOMINAL IN
ENGINE SECTION LOCATIONCOMPRESSOR
MATERIAL THICKNESS0.486 INCHES NOMINAL IN
SPECIAL FEATUREST.O. 2J-F100-54
END ITEM IDENTIFICATIONF100PW0229 AIRCRAFT ENGINE
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

No substitute or cross-reference records for this part.

LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — mutilation + specific procedure
Ready to buy 2840PL0696901?
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 2840PL0696901?
2840PL0696901 is a SHROUD SEGMENT,TURBINE,AIRCRAFT.
What is the NSN for 2840PL0696901?
2840PL0696901 is cataloged in the U.S. Government catalog under NSN 2840-01-321-4453. 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 — 2840PL0696901

✓ PartsTable — the parts reference. Every fact cited to its source.
PartsTable Design LLC · partstable.com
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-18.
PartsTable commercial catalog: edition Unified commercial catalog snapshot through 2026-09-28, edition date not on file, retrieved 2026-09-28.