Model: 6029T68G01

Aircraft Turbine Component Liner

Special Features:

T.O. 2j-j85-94, fig 22, ind 73; liner front is a fishmouth design; 2nd end dia. 17.768

Properties:

Overall Length
12.457 inches
Diameter
18.100 inches
End Application
Aircraft engine j85-ge-21a
Criticality Code Justification
Feat and abhp and abmz and czbj
Part Name Assigned By Controlling Agency
Original name liner, front afterburber
Engine Section Location
Afterburner
Material
Nickel alloy
Material Specification
Ams5536 assn standard single material response
NSN
2840-01-045-3880
Part Number
6029T68G01
Description
Liner,turbine Component,aircraft
CAGE

A liner designed for a turbine assembly, aircraft gas turbine engine or one of its components.

Part 6029T68G01 NSN 2840-01-045-3880

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52538
FIIG:
A530F0
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:
--
Paclk Weight:
12.0000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114730
UFC:
58790
LTL:
85.0
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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