Model: 220571Y2

Aircraft G Compressor Blade Lock

Special Features:

Goes on center main bearing support; compressor stator; front exit stage blade

Properties:

Overall Length
Between 0.548 inches and 0.552 inches
Overall Width
Between 0.112 inches and 0.116 inches
Material Thickness
0.010 inches
End Application
J-65 aircraft engine
Hardness Rating
Between 19.0 rockwell c and 26.0 rockwell c
Criticality Code Justification
Agav
Stage Number
1
Material
Steel
Material Specification
Ams5613 assn standard single material response
Reference Data And Literature
2j-j65-4
NSN
2840-00-326-1011
Part Number
220571Y2
Description
Lock,compressor Blade,aircraft G
CAGE
0AHP5

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 220571Y2 NSN 2840-00-326-1011

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:
SX
CRITL:
Y

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
194160
UFC:
55210
LTL:
50.0
LCL:
50.0
WCC:
713
TCC:
Z
SHC:
Z
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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