Model: 9080M68P01

Aircraft G Compressor Blade Lock
Description:

1.722 inches overall length, 1.530 inches overall width, 0.078 inches material thickness, acft eng. Tf-39 end item identification.

Special Features:

0.082 in. Thick

Properties:

Overall Length
1.722 inches
Overall Width
1.530 inches
Material Thickness
Between 0.078 inches and 0.082 inches
End Application
Aircraft eng. Tf-39
Criticality Code Justification
Matt and abhp and abmk
Stage Number
2
Material
Nickel alloy
NSN
2840-00-008-6168
Part Number
9080M68P01
Description
Lock,compressor Blade,aircraft G
CAGE
07482

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 9080M68P01 NSN 2840-00-008-6168

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:
NY
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
0.1000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
194120
UFC:
95100
LTL:
85.0
LCL:
100.0
WCC:
671
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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