Model: 6812955

Igniter Assembly

Properties:

Width
2.188 inches
Length
3.065 inches
Polarization Feature
Not included
Mounting Facility Size
Two 0.312 in. Diameter holes 1.500 in. C to c
Mounting Method
Flange
Plug Design
Elbow
Height
1.341 inches
NSN
2925-00-802-1418
Part Number
6812955
Description
Igniter Assembly
CAGE
24617

An item having one or more electrodes arranged to form an air gap across which an electric spark is introduced and discharged to ignite fuel and air mixture in an internal combustion engine for the purpose of initial starting only. In engines designed for the single electrode type, two plugs are required within the combustion chamber in proper placement to effect the air gap. An igniter plug differs from a spark plug by always having cooling facilities in the form of holes or slots in the plug casing to allow entry of air currents around the electrode(s). Excludes spark plug; glow plug and electrode.

Part 6812955 NSN 2925-00-802-1418

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
19767
FIIG:
T130-M
Concept No.:
App. Key:
MA
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:
--
Paclk Weight:
100.0000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
LVL_B:

End Items End applications NSN 2925-00-802-1418 is a component of

  • Turbo Prop Engines/(t56)

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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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