Model: 4009T25G08

Aircraft Gas Turbine Rear Frame

Properties:

Inside Diameter
15.515 inches
Overall Length
4.524 inches
Outside Diameter
17.000 inches
End Application
Aircraft eng j-85
Criticality Code Justification
Abhp and abkv and aarx
Part Name Assigned By Controlling Agency
Original name frame assembly, main
Number Of Variable Guide Vanes
6
Material
Nickel alloy
Reference Data And Literature
T.O. 2j-j85-74, fig 3, ind 53
NSN
2840-01-118-3521
Part Number
4009T25G08
Description
Frame,rear,aircraft Gas Turbine
CAGE
99207

A frame used for and part of the rear section of an aircraft gas turbine engine. May include struts.

Part 4009T25G08 NSN 2840-01-118-3521

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52347
FIIG:
A522Q0
Concept No.:
1
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:
OK
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
31.0 X 28.0 X 15.0
Paclk Weight:
38.0000lbs
Item Weight:
18.0000lbs
Item Dim:
017001700047
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
F000006XF1
SPI Rev.:
SPC Mkg:
17
LVL_A:
LVL_B:

Freight Classification

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