Model: 6051T95G01

Aircraft Gas Turbine Rear Frame

Special Features:

Mainframe compressor section

Properties:

Inside Diameter
Between 15.495 inches and 15.535 inches
Overall Length
Between 4.517 inches and 4.531 inches
Outside Diameter
Between 16.995 inches and 17.005 inches
End Application
Acft.Eng. J85
Criticality Code Justification
Abhp and abkv and aarx and czlb
Part Name Assigned By Controlling Agency
Original name frame assembly, turbine
Number Of Variable Guide Vanes
6
Material
Nickel alloy
Reference Data And Literature
T.O. 2j-j85-54, fig 13, ind 1
NSN
2840-01-263-9333
Part Number
6051T95G01
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 6051T95G01 NSN 2840-01-263-9333

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:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
20.5 X 20.5 X 6.5
Paclk Weight:
16.5000lbs
Item Weight:
15.0000lbs
Item Dim:
017001700045
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
F000005D63
SPI Rev.:
SPC Mkg:
17
LVL_A:
LVL_B:

Freight Classification

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