Model: 4013T87P02

Turbine Engine Cooling Plate

Properties:

End Application
Turbo prop engines (t58)
Criticality Code Justification
Agav
Part Name Assigned By Controlling Agency
Plate, stage 1 rear cooling air
NSN
2840-01-496-7472
Part Number
4013T87P02
Description
Plate,cooling,turbine Engine
CAGE
99207

An item of various cross sections used to exhaust heat from the gas generator turbine rotor of a turbine engine.

Part 4013T87P02 NSN 2840-01-496-7472

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
42000
FIIG:
A23900
Concept No.:
App. Key:
A
Cond. Code:
2
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:
CRITL:
F

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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