Model: 9992M60G07-108

Aircraft Gas Tur Compressor Disk

Properties:

Overall Length
6.287 inches
Diameter
17.200 inches
End Application
Aircraft eng f108
Design Type
Axial-centrifugal
Criticality Code Justification
Abhp and abmz and apgf and czbj
Part Name Assigned By Controlling Agency
Spool compressor rotor stages 1&2
Engine Section Location
Compressor
Stage Number
1
Material
Titanium
Reference Data And Literature
T.O. 2j-f108-4 fig 72-31-00-01 ind 140b
NSN
2840-01-313-4567
Part Number
9992M60G07-108
Description
Disk,compressor,aircraft Gas Tur
CAGE
98748

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 9992M60G07-108 NSN 2840-01-313-4567

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:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
21.0 X 21.0 X 8.0
Paclk Weight:
45.0000lbs
Item Weight:
35.0000lbs
Item Dim:
015501550068
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F012326379
SPI Rev.:
B
SPC Mkg:
ZZ
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114215
UFC:
63220
LTL:
RATING VARIABLE
LCL:
77.5
WCC:
671
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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