MIL-DTL-55302/154C
REQUIREMENTS
Dimensions and configurations: See figure 1.
Hardware intermateability: See table I.
Materials and finishes: Copper alloy in accordance with ASTM B16, plated in accordance with
SAE-AMS-QQ-N-290, grade G, for subpart number 2; stainless steel for subpart number 1.
Application: Each Part or Identifying Number (PIN) with subpart number 1 shall be interchangeable in
MIL-DTL-55302/140 through /153. Each PIN with subpart number 2 shall be interchangeable in
MIL-DTL-55302/144 through /153.
PIN example: M55302/154-1A.
A denotes different hardware styles.
1 denotes application in type of connector.
Changes from previous issue. Marginal notations are not used in this revision to identify changes with
respect to the previous issue due to the extent of the changes.
Referenced documents. In addition to MIL-DTL-55302, this document references the following:
MIL-DTL-55302/140
MIL-DTL-55302/144
MIL-DTL-55302/148
MIL-DTL-55302/153
MIL-DTL-55302/141
MIL-DTL-55302/145
MIL-DTL-55302/149
MIL-DTL-55302/155
MIL-DTL-55302/142
MIL-DTL-55302/146
MIL-DTL-55302/150
ASTM B16
MIL-DTL-55302/143
MIL-DTL-55302/147
MIL-DTL-55302/151
SAE-AMS-QQ-N-290
MIL-DTL-55302/152
CONCLUDING MATERIAL
Review activities:
Preparing activity:
Army CR
DLA - CC
Navy EC
Air Force 11
(Project 5935-4499-000)
DLA - CC
Review activities:
Army AR, AT, AV, CR4
Navy AS, MC, OS, SH
Air Force 19, 99
NOTE: The activities listed above were interested in this document as of the date of this document.
Since organizations and responsibilities can change, you should verify the currency of the information
above using the ASSIST Online database at https://assist.daps.dla.mil.
7
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