Model: 214-040-845-103

Engine Oil Pump Assembly

Special Features:

5.870 in.O/a l; speed 6925 rpm; flow 16.25-18-10 gpm at 180 degrees f and 150 psig; discharge pressure 160 plus or minus 10 psid at 180 degrees fahrenheit; oil plus mil-l-7808 or mil-l-23699

Properties:

End Application
Ah-1w acft
Reference Number Differentiating Characteristics
As differentiated by the source control dwg no.
NSN
2995-01-256-7641
Part Number
214-040-845-103
Description
Oil Pump Assembly,engine
CAGE
97499

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 214-040-845-103 NSN 2995-01-256-7641

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:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
8.0 X 7.0 X 7.0
Paclk Weight:
3.1000lbs
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:
128000
UFC:
64870
LTL:
85.0
LCL:
85.0
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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