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- NSN 2840-01-440-1697
NSN 2840-01-440-1697
Aircraft Tu Turbine Blade Damper
FSC: 2840 NIIN: 014401697DODParts.com distributes prime moving; and components aircraft gas turbines and jet engines, aircraft parts and consumables, electrical parts, fittings and other components for the aerospace and defense industries. Submit the short price quote form for NSN 2840-01-440-1697 to receive an up to date pricing and availability quote by email.
Product Characteristics
NSN:
2840014401697
Demilitarization:
DEMIL/MLI
INC:
50557
Shelf Life:
N/A
Overall Length:
Between 0.565 inches and 0.571 inches
Diameter:
16.788 inches
End Application:
F100-pw-229 aircraft gas turbine engine
Design Type:
Axial compressor
Hardness Rating:
34.0 rockwell c and 44.0 rockwell c
Criticality Code Justification:
Feat and czbj
Engine Section Location:
Compressor
Special Features:
T.O. 2j-f100-54, fig 99, ind 21; repl p/n 4074864 once tcto has been accomplished; retaining plate damper is symmetrical in shape and has 6 retention tabs forward and aft to preclude possible reverse installation and resulting cut-off of cooling air to the 2nd stage blades
Material:
Nickel alloy
Material Specification:
Ams5544 assn standard single material response
Part Numbers
-
4082885
UNITED TECHNOLOGIES CORPORATION
Shipping & Handling
HMIRS:No MSDS. No hazardous material.
ESD:No known electrostatic discharge.
Schedule B:8411997050 - Parts of gas turbine aircraft engines, other than for use in civil aircraft.
Professional Distribution
- ITAR Registered
- DDTC Registered
- HAZMAT Certified
- AS9120 Quality Standards
- 100% Quality Inspections
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Cage Codes
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