Model: GD252-3

Engine Oil Pump Assembly

Special Features:

Rotation clockwise, involute spline drive, 13 teeth, 32/64 diametral pitch, 30 deg. Pressure angle; flow vs speed inlet pressure 25-30 ins hg abs discharge, pressure: 35 psi. Oil: mil-l-780, temp: 180 degrees f, no entrained air.Flow vs inlet pressure speed; 4694rpm; discharge pressure 35 psi; oil mil-l-7808; temp 180 deg. F, no entrained air

Properties:

End Application
J69-t-25a engine
Reference Number Differentiating Characteristics
Asdifferentiated by drawing
NSN
2995-01-430-5539
Part Number
GD252-3
Description
Oil Pump Assembly,engine
CAGE
86329

A device designed to maintain oil pressure within the moving parts of an internal combustion engine. May contain parts such as shaft, gears, pin, bushing, screen, adjusting screw and the like.

Part GD252-3 NSN 2995-01-430-5539

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
36330
FIIG:
A526G0
Concept No.:
App. Key:
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:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
8.2 X 8.2 X 12.5
Paclk Weight:
3.8000lbs
Item Weight:
2.0000lbs
Item Dim:
007500750115
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
F000002XA2
SPI Rev.:
SPC Mkg:
17
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
127600
UFC:
64730
LTL:
85.0
LCL:
--
WCC:
594
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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