Electrical-electro Control Panels - Page 19 of 78
1928 part numbers
-
pacer special end application
-
control panel-overhead lighting special features
-
aircraft a-6e end application
-
mount constant speed drive usage design
-
constant speed drive panel assembly special features
-
f-16 aircraft end application
-
main fuel panel; front seat special features
-
c-17a aircraft end application
-
front panel assembly special features
-
c-130 cargo aircraft end application
-
mounting holes on all 4 corners mounting configuration
-
aluminum panel material
-
pilots lighting control panel special features
41646-1
NSN 1680-01-386-5060
Cross Reference:
10-0178-1
-
5.656 inches overall length
-
2.563 inches overall height
-
5.656 inches overall width
-
between 0.210 inches and 0.230 inches overall thickness
-
ch-53d and ch-53e helicopter. end application
-
mh-53 helo end application
-
f-14d aircraft end application
476270-01-01
NSN 1680-01-388-1892
Cross Reference:
ZC8-60-931-1-1
-
pacer dawn end application
-
pacer special end application
-
hardened nuclear hardness critical feature
-
0.063 inches overall thickness
-
c-130 hercules aircraft end application
-
aluminum alloy panel material
-
c-17 aircraft end application
-
feat criticality code justification
-
b-2 aircraft end application
-
a-6e end application
-
aluminum alloy panel material
-
panel controls ground refueling operation special features
-
c-130 aircraft end application
-
switches /control accessory components and quantity
-
aluminum alloy panel material
-
equipped with guarded switches special features
-
c-130h aircraft end application
-
4.750 inches overall length
-
c-130 aircraft end application
-
four mounting holes at corner edge of panel mounting configuration
-
aluminum alloy panel material
-
pilot; co-pilot overhead control panel special features
-
pacer special end application