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2920-00-540-8343

Spark Plug

2920005408343 005408343 WS506 J12 A11 48 M11

An item containing two or more electrodes across which an electric spark is discharged to ignite a fuel and air mixture, primarily in internal combustion engines. Excludes GLOW PLUG; and ELECTRODE. View more Spark Plug

2920-00-540-8343 SPARK PLUG 2920005408343 005408343

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
January 2023
NATO Update Count
12
NATO Data Quality
AAQL Style A11 for 2920-00-540-8343 1/2
NSN 2920-00-540-8343 (Identification) 1/2
AYGA Style B1 for 2920-00-540-8343 2/2
NSN 2920-00-540-8343 (Identification) 2/2

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2920-00-540-8343 Related Documents Related Documents 2920-00-540-8343 5+ Documents (More...)

9 | DAC: 5 1 Jan 1963 2920-00-540-7841 Spark Plug MT13RRNCC: 5 | RNVC: 9 | DAC: 5 1 Jan 1963 2920-00-540-8343
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TFS20 A11 J12 J14 DEFSTAN29-2 An item containing two or more electrodes across which an electric spark
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2920-00-540-8343 Demil Restrictions 2920-00-540-8343

DEMIL: A | DEMILI: | CRITICALITY: X | HMIC: N | PMIC: U | EDC: | ADPEC:

2920-00-540-8343 is a Spark Plug that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. The precious metals content of this item is unknown.

2920-00-540-8343 HTS and ScheduleB Import and Export 2920-00-540-8343

2920-00-540-8343 End Users End Users 2920-00-540-8343

NASA (G720)
Effective Date:
1 Apr 1991
NASA (G900)
Effective Date:
1 Apr 1991
Australia (ZA01)
Effective Date:
1 Oct 2016
Denmark (ZS01)
Effective Date:
1 Dec 1996

2920-00-540-8343 Manufacturers Approved Sources 2920-00-540-8343

2920-00-540-8343 Technical Data Datasheet 2920-00-540-8343

Characteristic
Specifications
FIIG
A10400
Electrode Style [AYGA]
Single Flat Shell Ground Electrode (See Also Style 4)
Body Style [AAQL]
Unshielded,Solid Or Threaded Post,Gasket Seat
Height Above Mounting Surface [AYGJ]
2.300 Inches Nominal
Mean Effective Pressure Rating [AYGF]
100.0 Pounds Per Square Inch Minimum And 115.0 Pounds Per Square Inch Maximum
Nondefinitive Spec/Std Data [ZZZT]
3 Type And B Class
Reach Length [AHPM]
0.375 Inches Nominal
Seat Major Diameter [AYGH]
0.812 Inches Maximum
Usage Design [ALBY]
Engine Other Than Aircraft
Width Across Flats [ASDB]
0.812 Inches Nominal
Test Data Document [TEST]
81348-Ws506 Specification (Includes Engineering Type Bulletins, Brochures,Etc., That Reflect Specification Type Data In Specification Format; Excludes Commercial Catalogs, Industry Directories, And Similar Trade Publications, Reflecting General Type Data On Certain Environmental And Performance Requirements And Test Conditions That Are Shown As "Typical", "Average", "Nominal", Etc.).
Thread Size And Series/Type Designator And Location [AYGB]
14-1.25Mm Base

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2920-00-540-8343 Freight Data Freight Information 2920-00-540-8343

2920-00-540-8343 has freight characteristics.. 2920-00-540-8343 has a variance between NMFC and UFC when transported by rail and the description should be consulted.