Model: 777886CL2

Aircraf Turbine Nozzle Lock Ring

Special Features:

Matl specification ams 5731

Properties:

Outside Diameter
Between 34.878 inches and 34.908 inches
Overall Thickness
Between 0.123 inches and 0.127 inches
End Application
Aircraft eng tf33
Criticality Code Justification
Agav
Stage Number
3
Material
Steel
Reference Data And Literature
2j-tf33-34, figure 28, index 21
NSN
2840-01-124-0722
Part Number
777886CL2
Description
Lock Ring,turbine Nozzle,aircraf
CAGE
77445

A round metallic item designed to retain a nozzle, nozzle assembly, or nozzle segment, turbine, aircraft gas turbine engine in a case and nozzle assembly, turbine, aircraft gas turbine engine. It may be a complete 360 degrees circle or a section thereof.

Part 777886CL2 NSN 2840-01-124-0722

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52365
FIIG:
A522R0
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:
RV
CRITL:
Y

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
WCC:
593
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

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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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