Electrical-electro Control Panels - Page 28 of 78
1928 part numbers
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c-130 aircraft end application
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f-16 aircraft end application
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drawing name - panel assembly - fuel control special features
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f-16 aircraft end application
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1 acrylic panel, 1 knob, 8 switches, 1 cover accessory components and quantity
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plastic panel material
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feat criticality code justification
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preprovisioning support navicp is poe end application
AE91005
NSN 1680-01-432-0021
Cross Reference:
4490006-501
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between 5.688 inches and 5.718 inches overall length
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1.453 inches overall height
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helicopter, lamps mark iii, sh-60b end application
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plastic, mil-p-5425 panel material
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c-130 aircraft end application
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c-17 aircraft end application
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feat criticality code justification
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c-17 aircraft end application
3350079-5
NSN 1680-01-433-1958
Cross Reference:
3350079-3
697910-1
NSN 1680-01-433-4990
Cross Reference:
712940-1
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c130-j acft end application
697961-1
NSN 1680-01-433-4991
Cross Reference:
30106-01
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c130-j end application
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t.o.1c-130j-4-46-1 special features
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c130-j acft end application
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c130-j acft end application
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c130-j acft end application
697914-1
NSN 1680-01-433-6895
Cross Reference:
6376850G1
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3.730 inches overall height
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7.950 inches overall width
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c130-j acft end application
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aluminum alloy panel material
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b-2 aircraft end application
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hardened nuclear hardness critical feature
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b-2 aircraft end application
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drawing name- control panel - apumaintenance special features
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hardened nuclear hardness critical feature
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b-2 aircraft end application
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1 panel assembly, 1 switch, 1 wiring harness accessory components and quantity
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drawing name - control panel, aftaccess door special features
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hardened nuclear hardness critical feature
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f-16 aircraft end application
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drawing name - panel assembly - stickcontrol special features
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3.000 inches overall height
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3.000 inches overall width
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aircraft c-130 end application
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relay cover usage design
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relay assembly, undervoltage ac. special features