Model: 9992M69G40

Aircraft Gas Tur Compressor Case

Special Features:

Original name case and nozzle, turbine, turbine engine

Properties:

Overall Length
22.000 inches
End Application
Aircraft eng f108
Design Type
Axial compressor
Criticality Code Justification
Agav
Part Name Assigned By Controlling Agency
Case assembly-front & extension cprsr sttr
Engine Section Location
Turbine
Material
Titanium
Reference Data And Literature
T.O. 2j-f108-14 fig 72-32-00-05 ind 400l
NSN
2840-01-189-2633
Part Number
9992M69G40
Description
Case,compressor,aircraft Gas Tur
CAGE
58828

A case that is an integral part of an engine, gas turbine, aircraft, designed to surround and protect a rotor, compressor, aircraft gas turbine engine.

Part 9992M69G40 NSN 2840-01-189-2633

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50547
FIIG:
A10700
Concept No.:
3
App. Key:
D
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:
34.3 X 34.3 X 28.3
Paclk Weight:
202.0000lbs
Item Weight:
92.0000lbs
Item Dim:
028002800216
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F011892633
SPI Rev.:
D
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:
85.0
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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