Model: 9084M77G02

Aircraft Gas Turbine En Oil Sump

Properties:

Diameter
Between 16.019 inches and 16.023 inches
End Application
Engine, acft, turbofan, model tf39-g1a
Criticality Code Justification
Agav
Material
Stainless steel
NSN
2840-00-352-2165
Part Number
9084M77G02
Description
Sump,oil,aircraft Gas Turbine En
CAGE
07482

A chamber surrounding the main bearings for a shaft, turbine, aircraft gas turbine engine. The chanber is used to collect lubricating fluid for recirculation.

Part 9084M77G02 NSN 2840-00-352-2165

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52549
FIIG:
A10700
Concept No.:
App. Key:
G
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:
U
ESD:
ESD:
MMAC:
NY
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
18.5 X 18.5 X 12.5
Paclk Weight:
34.0000lbs
Item Weight:
31.0000lbs
Item Dim:
016501600090
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
F000005E58
SPI Rev.:
SPC Mkg:
17
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114215
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
WCC:
671
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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