Power Distribution Panels - Page 14 of 161
4021 part numbers
16E1046-803
NSN 6110-01-051-2899
Cross Reference:
16E1046-3, 16E1046-801
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pylon on f-16a/b aircraft end application
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feat criticality code justification
16E1132-813
NSN 6110-01-051-3051
Cross Reference:
16E1132-803, 16E1132-807
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console mounting method
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partially enclosed inclosure feature
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4 panel quantity
16E1080-801
NSN 6110-01-051-3053
Cross Reference:
16E1080-3, 16E1080-5
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console mounting method
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29 accessory component quantity
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fully enclosed inclosure feature
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1 panel quantity
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radar set an/apn-59v end application
16E1047-813
NSN 6110-01-051-6306
Cross Reference:
16E1047-803, 16E1047-807, 16E1047-811
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any acceptable mounting method
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f-16 acft end application
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any acceptable inclosure feature
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feat criticality code justification
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used on wing stores no. 3 functional description
16E1363-803
NSN 6110-01-051-6398
Cross Reference:
16E1148-803, 16E1363-5
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f-16 aircraft end application
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fuel quantity system; used on 16e1364 functional description
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aircraft accessory equipment fsc application data
16E1090-3
NSN 6110-01-052-0924
Cross Reference:
16E1090-1
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console mounting method
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20 accessory component quantity
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switch 3, receptacle 1 furnished items
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partially enclosed inclosure feature
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3 panel quantity
16E1165-5
NSN 6110-01-052-0925
Cross Reference:
16E1165-1, 16E1165-3
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console mounting method
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6 accessory component quantity
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partially enclosed inclosure feature
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2 panel quantity
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6.750 inches overall length
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1.970 inches overall height
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6.500 inches overall width
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f-16 end application
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console mounting method
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27 accessory component quantity
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fully enclosed inclosure feature
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1 panel quantity
826899-1
NSN 6110-01-052-4863
Cross Reference:
FA9340
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any acceptable inclosure feature
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1 panel quantity
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1 electrical input quantity
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1 electrical output quantity
16E1157-9
NSN 6110-01-052-6070
Cross Reference:
16E1157-15
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f-16 aircraft end application
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console mounting method
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f-16 aircraft end application
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fully enclosed inclosure feature
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1 panel quantity
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miscellaneous systems testing functional description
16E1143-811
NSN 6110-01-054-1234
Cross Reference:
16E1143-819, 16E1143-827, 16E1143-843
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6.750 inches overall length
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1.970 inches overall height
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6.500 inches overall width
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f-16 end application
16E1156-15
NSN 6110-01-055-1964
Cross Reference:
16E1156-11
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f-16 end application
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forward avionics mux bus no.1 and 2 functional description
16E1046-804
NSN 6110-01-055-3330
Cross Reference:
16E1046-4, 16E1046-802
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panel mounting method
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68 accessory component quantity
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support assembly furnished items
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f-16a/b aircraft end application
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general dynamics accessory controlling agency
16E1047-812
NSN 6110-01-055-3331
Cross Reference:
16E1047-804
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any acceptable mounting method
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f-16 acft end application
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any acceptable inclosure feature
16E1081-801
NSN 6110-01-055-3507
Cross Reference:
16E10681-805, 16E1081, 16E1081-3, 16E1081-805
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panel mounting method
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partially enclosed inclosure feature
16E1363-801
NSN 6110-01-055-6442
Cross Reference:
16E1148-801, 16E1363-3
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f-16 aircraft end application
-
fuel quantity system; used on 16e1364 functional description
-
aircraft accessory equipment fsc application data
16E1156-17
NSN 6110-01-057-0806
Cross Reference:
16E1156-13
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f-16 end application
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forward avionics mux bus no.1 and 2 functional description
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350.0 wattage rating in watts
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chassis mounting method
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aluminum alloy panel material
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three input phase
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400 hertz output frequency rating
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cabinet and rack assembly, test station end application
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aircraft model f16a/b end application
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1.031 cubic inches cubic measure
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cpu didital end application
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15.0 pounds unpackaged unit weight