Model: 6900T74G02

Aircraf Combustion Chamber Liner

Special Features:

T.O. 2j-j85-74, fig 17, ind 9; includes cowl and dome

Properties:

End Application
Acft.Eng. J85 17/17a
Criticality Code Justification
Agav
Part Name Assigned By Controlling Agency
Original name liner assembly, cowl anddome
Engine Section Location
Diffuser
Material
Nickel alloy
Material Specification
Ams5540 assn standard 1st material response and ams5552 assn standard 2nd material response
NSN
2840-01-229-0990
Part Number
6900T74G02
Description
Liner,combustion Chamber,aircraf
CAGE
T0545

A cylindrical shaped item positioned inside the chamber, combustion, aircraft gas turbine engine. It is designed to direct the flow of hot gasses to the turbine assembly, aircraft gas turbine engine.

Part 6900T74G02 NSN 2840-01-229-0990

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50349
FIIG:
A530F0
Concept No.:
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:
--
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
Q
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
012190
UFC:
04870
LTL:
100.0
LCL:
--
WCC:
593
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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