Miscellaneous Aircraft Accessories and Components: 16F0434-9, 16F1340-9, 16F1415-815
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
16F0434-9 16F04349 | 1680-01-083-7429 | Mount Support, Wrist | III End Item Identification: F-16 acft General Characteristics Item Description: Aluminum alloy, AMS4218-T6;2.900 inch HIGH;3.100 inch WIDE;2 0.191 inch diameter minimum, 0.196 inch diameter maximum holes in LINE;2 0.126 inch diameter holes in LINE;2 0.199 inch diameter holes in line;prime and paint all areas except omit prime and paint from insert and pin holes;install pins per FPS-3001, element 206;METAL removal PERFPS-3017;REMOVE cast dash number from cast part number and mark finished part dash no per FPS-3008 cl 2A III Fsc Application Data: Aircraft accessory equipment | Lockheed Martin Corporation (81755) | |
16F0438-7 16F04387 | 1680-01-084-2060 | Knob-Thumb Adjusting, Lock, Pilots | End Item Identification: F-16 acft pilots wrist support P/N 16F0435 General Characteristics Item Description: 0.985 inch outside DIAMETER;0.020INCH inside DIAMETER;20 grooves 0.032 inch deep equally spaced on 0.810 inchdiameter;mark parts per FPS-3008, CL2D;FILLET radii 0.03 maximum;finish spec per FPS-3001;MARKING spec per FPS-3008;TUBING bead std per MS33660 | Gencon Plastics Inc. (1W607) Lockheed Martin Corporation (81755) | |
16F1101-1 16F11011 | 1680-01-114-0255 | Panel Assembly, Instrument | III End Item Identification: F-16 aircraft General Characteristics Item Description: C/O15 INSERTS;4 nuts;rivets as REQUIRED;1 SPACER;2 panels;verify heat treatment per NDTS1500;USE of next longer or shorter grip nut in lieu of MS33737-11 is permissable;the material shall meet class a ultrasonic inspection of MIL-1-8950, NDTS5101;DIMENSIONS are 27.520 inches long by 10.250 inches wide;electrical bond per FPS-3024;METEL removal per FPS-3017;INSTALL bushings and inserts with FPS-3001 element 206;PRIME all areas.paint area noted except .5000/.5005 holes III Fsc Application Data: Aircraft accessory equipment | Lockheed Martin Corporation (81755) | |
16F1101-5 16F11015 | 1680-01-114-0255 | Panel Assembly, Instrument | III End Item Identification: F-16 aircraft General Characteristics Item Description: C/O15 INSERTS;4 nuts;rivets as REQUIRED;1 SPACER;2 panels;verify heat treatment per NDTS1500;USE of next longer or shorter grip nut in lieu of MS33737-11 is permissable;the material shall meet class a ultrasonic inspection of MIL-1-8950, NDTS5101;DIMENSIONS are 27.520 inches long by 10.250 inches wide;electrical bond per FPS-3024;METEL removal per FPS-3017;INSTALL bushings and inserts with FPS-3001 element 206;PRIME all areas.paint area noted except .5000/.5005 holes III Fsc Application Data: Aircraft accessory equipment | Lockheed Martin Corporation (81755) | |
16F1101-6 16F11016 | 1680-01-114-0255 | Panel Assembly, Instrument | III End Item Identification: F-16 aircraft General Characteristics Item Description: C/O15 INSERTS;4 nuts;rivets as REQUIRED;1 SPACER;2 panels;verify heat treatment per NDTS1500;USE of next longer or shorter grip nut in lieu of MS33737-11 is permissable;the material shall meet class a ultrasonic inspection of MIL-1-8950, NDTS5101;DIMENSIONS are 27.520 inches long by 10.250 inches wide;electrical bond per FPS-3024;METEL removal per FPS-3017;INSTALL bushings and inserts with FPS-3001 element 206;PRIME all areas.paint area noted except .5000/.5005 holes III Fsc Application Data: Aircraft accessory equipment | Lockheed Martin Corporation (81755) | |
16F1101-803 16F1101803 | 1680-01-114-0255 | Panel Assembly, Instrument | III End Item Identification: F-16 aircraft General Characteristics Item Description: C/O15 INSERTS;4 nuts;rivets as REQUIRED;1 SPACER;2 panels;verify heat treatment per NDTS1500;USE of next longer or shorter grip nut in lieu of MS33737-11 is permissable;the material shall meet class a ultrasonic inspection of MIL-1-8950, NDTS5101;DIMENSIONS are 27.520 inches long by 10.250 inches wide;electrical bond per FPS-3024;METEL removal per FPS-3017;INSTALL bushings and inserts with FPS-3001 element 206;PRIME all areas.paint area noted except .5000/.5005 holes III Fsc Application Data: Aircraft accessory equipment | Lockheed Martin Corporation (81755) | |
16F1101-805 16F1101805 | 1680-01-157-3900 | Panel Assembly, Instrument | III End Item Identification: F-16 aircraft General Characteristics Item Description: Consists of -17 panel;verify heattreatment per NDTS1500;USE of next longer or shorter grip nut in lieu of MS33737-11 is permissible;the material shall meet class a ultrasonic inspectionof MIL-1-8950, NDTS5101 III Fsc Application Data: Aircraft accessory equipment | Lockheed Martin Corporation (81755) | |
16F1226-1 16F12261 | 1680-01-116-2359 | Curtain Seat Assembly | III End Item Identification: F-16 aircraft III Fsc Application Data: Seat aircraft | Lockheed Martin Corporation (81755) | |
16F1226-3 16F12263 | 1680-01-117-7514 | Closeout Curtain Seat, Assembly | III End Item Identification: F-16 aircraft General Characteristics Item Description: C/othread as REQUIRED;6 SHIMS;6 EYELETS;1 MARKING;11 CURTAINS;11 POUCHES;3 flap assemblies III Fsc Application Data: Seat, aircraft | Lockheed Martin Corporation (81755) | |
16F1226-5 16F12265 | 1680-01-116-2359 | Curtain Seat Assembly | III End Item Identification: F-16 aircraft III Fsc Application Data: Seat aircraft | Lockheed Martin Corporation (81755) | |
16F1226-801 16F1226801 | 1680-01-117-7514 | Closeout Curtain Seat, Assembly | III End Item Identification: F-16 aircraft General Characteristics Item Description: C/othread as REQUIRED;6 SHIMS;6 EYELETS;1 MARKING;11 CURTAINS;11 POUCHES;3 flap assemblies III Fsc Application Data: Seat, aircraft | Lockheed Martin Corporation (81755) | |
16F1226-803 16F1226803 | 1680-01-117-7514 | Closeout Curtain Seat, Assembly | III End Item Identification: F-16 aircraft General Characteristics Item Description: C/othread as REQUIRED;6 SHIMS;6 EYELETS;1 MARKING;11 CURTAINS;11 POUCHES;3 flap assemblies III Fsc Application Data: Seat, aircraft | Lockheed Martin Corporation (81755) | |
16F1340-9 16F13409 | 1680-01-160-7248 | Panel Assembly, Sensor Power | End Item Identification: F-16C/D aircraft General Characteristics Item Description: 2 holes 0.220 minimum, 0.250 maximum inch DIAMETER;2 holes 0.311 minimum, 0.318 maximum inch grommet HOLE;4 holes 0.515 counterbore 0.735 inch diameter, 0.125 inch deep minimum, 0.546 counterbore, 0.765 inch diameter, 0.156 maximum inch deep;all counterbore holes 0.016 outer radius permissible;break all edges 0.02R;ROUND all corners 0.06 Type/Model Designation: Tail effectivity 5C OOO1 9999 | Aeropanel Corporation (33583) Aerospace Optics Inc. (32245) Airco Industries Inc. (16329) CMP Display Systems Inc. (59057) Lockheed Martin Corporation (81755) | |
16F1415-3 16F14153 | 1680-01-116-2356 | Panel Assembly, Equipment, Right H | III End Item Identification: F-16 aircraft General Characteristics Item Description: C/O25 SWITCHS;4 RECEPTACLES;3 clouseout PANELS;3 INDICATORS;1 secure VOICE;2 vhf/am fm PANELS;2 COMPASS;2 INDICATORS;2 CLOCKS;2 ALTIMETERS;4 BLINKERS;2 epu fuel INDICATORS;6 caution PANELS;1 CONTROL;2 fc/nav PANELS;2 range mkg INSTL;3 oxy PANELS;2 switch PANELS;9 blank PANELS;4 nuc consent PANELS;4TAKE control PANELS;5 chaff/flare PANELS;4 ext LIGHTING;4 lighting PANELS;4 air cond PANELS;4 anti-ice PANELS;4 feul Qty SEL;1 CONTROL;1 buc gnd PL;1 zeroizer PL;2 range rkg INSTL;1 dtu CONNSPRT;1 avionics PANEL;1 sensor PANEL;1NUC/VHF PANEL;47 SCREWS;1 guard;government furnished aeronautical EQUIPMENT;16VE012-3 may be used as an alternate part for 16VE012-4 III Fsc Application Data: Panel, control, electrical control equipment, aircraft | Lockheed Martin Corporation (81755) | |
16F1415-801 16F1415801 | 1680-01-161-0434 | Panel, Control, Electrical-Electro | III End Item Identification: F-16 aircraft III Fsc Application Data: Aircraft accessory equipment Accessory Components and Quantity: Switches, guard, wiring harness, covers, panel, mounting plate, mountindevice, connector | Lockheed Martin Corporation (81755) | |
16F1415-803 16F1415803 | 1680-01-166-5384 | Panel, Control, Electrical-Electro | III End Item Identification: F-16 aircraft III Fsc Application Data: Control assembly, aircraft III Functional Description: Modification of panel assembly, equipment, right hand console P/N 16F1415-3 | Aerospace Engineering & Support Inc. (1DA92) Lockheed Martin Corporation (81755) | |
16F1415-809 16F1415809 | 1680-01-279-3982 | Panel, Control, Electrical-Electro | III End Item Identification: F-16C/D air combat fighter III Functional Description: Nuc & vhf; used on 16F8014-1 Accessory Components and Quantity: Switches, guard, wiring harness, covers, panel, mounting plate, mounting device, connector | Lockheed Martin Corporation (81755) | |
16F1415-811 16F1415811 | 1680-01-279-3982 | Panel, Control, Electrical-Electro | III End Item Identification: F-16C/D air combat fighter III Functional Description: Nuc & vhf; used on 16F8014-1 Accessory Components and Quantity: Switches, guard, wiring harness, covers, panel, mounting plate, mounting device, connector | Lockheed Martin Corporation (81755) | |
16F1415-813 16F1415813 | 1680-01-279-3982 | Panel, Control, Electrical-Electro | III End Item Identification: F-16C/D air combat fighter III Functional Description: Nuc & vhf; used on 16F8014-1 Accessory Components and Quantity: Switches, guard, wiring harness, covers, panel, mounting plate, mounting device, connector | Lockheed Martin Corporation (81755) | |
16F1415-815 16F1415815 | 1680-01-448-9562 | Panel, Control, Electrical-Electro | III End Item Identification: F-16C acft Special Features: Modification to incorporate nightvision illuminated panel P/N 69196-003 | Lockheed Martin Corporation (81755) |