Model: 9940M55P08-108

Aircraft Gas Tur Compressor Disk

Special Features:

Original name disk, turbine, turbine engine

Properties:

Overall Width
Between 1.180 inches and 1.190 inches
Diameter
17.000 inches
Material Thickness
1.5000 inches
End Application
Aircraft eng f108
Design Type
Axial compressor
Part Name Assigned By Controlling Agency
Disk, compressor rotor - stage 3
Engine Section Location
Compressor
Stage Number
3
Material
Titanium
Reference Data And Literature
2j-f108-14 fig 72-31-00-1 ind 120d
NSN
2840-01-187-3182
Part Number
9940M55P08-108
Description
Disk,compressor,aircraft Gas Tur
CAGE
07482

An item having provisions on the outer periphery for attaching a designated number of blade, compressor, aircraft gas turbine engine. it also has provisions for attachment to a hub, compressor, aircraft gas turbine engine and/or a shaft, turbine, aircraft gas turbine engine.

Part 9940M55P08-108 NSN 2840-01-187-3182

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50567
FIIG:
A10700
Concept No.:
App. Key:
G
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:
PN
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
23.1 X 23.1 X 2.6
Paclk Weight:
15.0000lbs
Item Weight:
10.0000lbs
Item Dim:
017301730013
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F012276613
SPI Rev.:
D
SPC Mkg:
ZZ
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
WCC:
593
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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