Model: 4007T78G08

Aircraft Gas Tu Compressor Frame

Properties:

Overall Length
Between 4.427 inches and 4.431 inches
Outside Diameter
Between 16.995 inches and 17.005 inches
End Application
J85-ge-21b aircraft gas turbine engine
Criticality Code Justification
Abhp and abkv
Part Name Assigned By Controlling Agency
Mainframe and bracket assembly
Reference Data And Literature
T.O. 2j-j85-94 fig 11 ind 1 or fig 3 ind 13
NSN
2840-01-268-2008
Part Number
4007T78G08
Description
Frame,compressor,aircraft Gas Tu
CAGE
99207

A frame used for and part of a compressor,aircraft gas turbine engine. May include struts with or without variable guide vanes.

Part 4007T78G08 NSN 2840-01-268-2008

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52339
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:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
22.3 X 22.3 X 12.5
Paclk Weight:
14.9000lbs
Item Weight:
9.8000lbs
Item Dim:
018001800070
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
F000005D66
SPI Rev.:
SPC Mkg:
17
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
191760
UFC:
93940
LTL:
70.0
LCL:
70.0
WCC:
586
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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