Model: 4079610

Aircraft G Compressor Blade Lock

Special Features:

44 units per assembly; 1 per 2 statorvanes

Properties:

Overall Length
1.411 inches
Overall Width
Between 0.701 inches and 0.708 inches
Material Thickness
Between 0.071 inches and 0.078 inches
End Application
F100pw229 aircraft eng core
Hardness Rating
36.0 rockwell c
Criticality Code Justification
Agav
Stage Number
6
Material
Nickel alloy
Material Specification
Ams5596 assn standard single material response
Reference Data And Literature
2j-f100-54, fig 96, ind 51
NSN
2840-01-374-4833
Part Number
4079610
Description
Lock,compressor Blade,aircraft G
CAGE
77445

An item used to maintain the position of a blade, compressor, aircraft gas turbine engine in the proper place on a disk, compressor, aircraft gas turbine engine. this item eliminates axial movement of the blade.

Part 4079610 NSN 2840-01-374-4833

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50454
FIIG:
A503Q0
Concept No.:
App. Key:
Cond. Code:
1
Status:
A

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
A
ESD:
ESD:
MMAC:
NZ
CRITL:
Y

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
120800
UFC:
61410
LTL:
RATING VARIABLE
LCL:
--
WCC:
590
TCC:
Z
SHC:
9
ACC:
Trailers/Vehicles

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Schedule B and Export
  • Schedule B: 8411997050
  • SITC: 71499
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

Freight Class: Parts of gas turbine aircraft engines, other than for use in civil aircraft

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