Model: 6044T93P02

Turbine Engine Cooling Plate

Special Features:

Flight safety critical aircraft part

Properties:

General Description
5 holes, 0.272 in. Min, 0.276 in. Max diameter located on 3.520 in. Bolt circle dia, 38 grooves equally spaced
NSN
2840-01-140-6733
Part Number
6044T93P02
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 6044T93P02 NSN 2840-01-140-6733

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

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
8.0 X 8.0 X 3.0
Paclk Weight:
1.0000lbs
Item Weight:
0.8000lbs
Item Dim:
006000600009
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
136500
UFC:
68455
LTL:
RATING VARIABLE
LCL:
--
WCC:
576
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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