Electrical-electro Control Panels - Page 35 of 78
1928 part numbers
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c-17a aircraft end application
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feat criticality code justification
16F8425-5
NSN 1680-01-457-7545
Cross Reference:
16F8425-1
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c-17a aircraft end application
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feat criticality code justification
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b-1b aircraft end application
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1 knob; 1 rotary switch; 1 toggleswitch accessory components and quantity
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hardened nuclear hardness critical feature
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t.o. 8a3-18-13-2 reference data and literature
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f-16 aircraft end application
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engine and jet start functional description
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aircraft c-17a end application
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b-2 aircraft end application
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b-2 aircraft end application
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f-16 aircraft end application
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f-16 aircraft end application
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h-53 helicopteer end application
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ch47 helicopter end application
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flight director mode select panel supplementary features
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f-16 aircraft end application
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c-130e aircraft end application
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c-17a acft end application
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f-15i aircraft end application
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target acquisition designation sight, pilot end application
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a-10 acft end application
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fill panel accessory components and quantity
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4 holes mounting configuration
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5.750 inches overall length
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2.625 inches overall width
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avionics auxiliary panel a-10 acft end application