Model: 6003T87G01

Aircraft Gas Turbine En Oil Sump

Special Features:

T.O. 2j-j85-94, fig 7, ind 28; 2nd end dia. 5.560

Properties:

Overall Length
Between 2.868 inches and 2.872 inches
Diameter
6.300 inches
Material Thickness
Between 0.070 inches and 0.090 inches
End Application
J85-ge-21/21a/21b aircraft gas turbine engine
Criticality Code Justification
Abhp and abpx and abmz and feat
Part Name Assigned By Controlling Agency
Original name sump, front frame
Engine Section Location
Compressor
Material
Aluminum
Material Specification
Ams4117 assn standard 1st material response or ams4065 assn standard 2nd material response
NSN
2840-00-855-5799
Part Number
6003T87G01
Description
Sump,oil,aircraft Gas Turbine En
CAGE

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 6003T87G01 NSN 2840-00-855-5799

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:
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:
M
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
WCC:
594
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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