Model: 3040M77P02

Combustion Chamber Compo Support

Properties:

Inside Diameter
Between 22.980 inches and 23.000 inches
Overall Length
Between 1.120 inches and 1.140 inches
Outside Diameter
23.910 inches
Mounting Hole Diameter
0.083 inches
Mounting Hole Quantity
444
End Application
Aircraft eng tf 39
Criticality Code Justification
Agav
Material
Steel
NSN
2840-01-109-7709
Part Number
3040M77P02
Description
Support,combustion Chamber Compo
CAGE

A support designed for a chamber,combustion,aircraft gas turbine engine or one of its components. Excludes support,seal,aircraft gas turbine engine.

Part 3040M77P02 NSN 2840-01-109-7709

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52567
FIIG:
A521B0
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:
NY
CRITL:
Y

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
120800
UFC:
61410
LTL:
RATING VARIABLE
LCL:
--
WCC:
590
TCC:
Z
SHC:
9
ACC:
Trailers/Vehicles

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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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