
MIL-C-85049/38A
REQUIREMENTS:
Design and construction:
Dimensions and configuration: See figure .1.
Interface dimensions shall conform to MIL-C-38999 series III and IV.
The coupiing nut shall be captivated to the adapter body and free to rotate.
Figure 1 dimension F1 is applicable when the end of screw is flush with -BB-.
Material:
Adapter body, coupling nut, and saddle bars - ~luminum alloy in accordance with”
MIL-C-85049.
Clamp screws and l,ockwashers - Corrosion resisting steel, passivate.
Ffnish: In accordance with MIL-C-85049.
A- Black anodize
Part number: , See example below:
M85049/
I
I
Military designator I
Specification sheet iii
.-.” I1’
Shell size Ii
. . I
Finish I
QUALIFICATION: See MIL-C-85049, category 46.
- @QPLe valuatingactivity: Naval Avionics Center, Code il/714, 6000””East 21st
Street, Indianapolis, Indiana 46218.
Custodians:
Army - CR
Navy - AS
Air Force -’ 85
Review activities:
Army - AR, MI
Navy - EC
Air Force - 11, 15, 17, 19, 99
OLA - ES
Preparing activity:
Air Force - 85
(Project 5935-3294-5)
User activity:
Army - AV
Agent:
DLA - ES
3
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