Miscellaneous Aircraft Accessories and Components: 16E2545-59, 16E2545-61, 16E3149-1
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
16E2545-59 16E254559 | 1680-01-119-5310 | Matrix Assembly | III End Item Identification: F-16 aircraft General Characteristics Item Description: C/otape as REQUIRED;7 SCREWS;6 relays;verify heat treat per NDTS1500 III Fsc Application Data: Aircraft accessory equipment | Lockheed Martin Corporation (81755) | |
16E2545-61 16E254561 | 1680-01-119-5309 | Matrix Assembly | III End Item Identification: F-16 aircraft General Characteristics Item Description: C/otape as REQUIRED;17 SCREWS;14 RELAYS;17 NUTS;2 CLAMPS;1 WASHER;12 GUARDS;1 harness;adhesive as REQUIRED;1 tray assembly;verify heat treat per NDTS1500 III Fsc Application Data: Aircraft accessory equipment | Lockheed Martin Corporation (81755) | |
16E2545-69 16E254569 | 1680-01-119-5310 | Matrix Assembly | III End Item Identification: F-16 aircraft General Characteristics Item Description: C/otape as REQUIRED;7 SCREWS;6 relays;verify heat treat per NDTS1500 III Fsc Application Data: Aircraft accessory equipment | Lockheed Martin Corporation (81755) | |
16E2545-71 16E254571 | 1680-01-119-5309 | Matrix Assembly | III End Item Identification: F-16 aircraft General Characteristics Item Description: C/otape as REQUIRED;17 SCREWS;14 RELAYS;17 NUTS;2 CLAMPS;1 WASHER;12 GUARDS;1 harness;adhesive as REQUIRED;1 tray assembly;verify heat treat per NDTS1500 III Fsc Application Data: Aircraft accessory equipment | Lockheed Martin Corporation (81755) | |
16E2545-73 16E254573 | 1680-01-119-5310 | Matrix Assembly | III End Item Identification: F-16 aircraft General Characteristics Item Description: C/otape as REQUIRED;7 SCREWS;6 relays;verify heat treat per NDTS1500 III Fsc Application Data: Aircraft accessory equipment | Lockheed Martin Corporation (81755) | |
16E2545-75 16E254575 | 1680-01-139-2201 | Matrix Assembly | III End Item Identification: F-16 aircraft General Characteristics Item Description: C/oscrew NAS1101-3-9, NAS1101-04-6;RELAY P/N M83726/24-3002, M83726/24-1002, C4942-1, M6106/24-003, M6106/22-003, M6106/21-003;NUT P/N MS21042L3, C8836-3, C8836-1;CLAMP P/N C2874D6, C2874D4;WASHER P/N AN960D10;HARNESS P/N H16DW1160-07;ADHESIVE P/N H16DW1160-53;TRAY assembly P/N H16DW1160-49 III Fsc Application Data: Aircraft accessory equipment | Lockheed Martin Corporation (81755) | |
16E2545-77 16E254577 | 1680-01-139-2808 | Matrix Assembly | III End Item Identification: F-16B aircraft General Characteristics Item Description: Matrix installation, engine, increases low oil pressure switch warning light time delay III Fsc Application Data: Aircraft accessory equipment | Lockheed Martin Corporation (81755) | |
16E2545-79 16E254579 | 1680-01-173-0453 | Panel, Control, Electrical-Electro | III End Item Identification: F-16 aircraft III Fsc Application Data: Aircraft accessory equipment III Type/Model Designation: F-16C/D air combat fighter, tail effectivity 5C 0001 9999 | Lockheed Martin Corporation (81755) | |
16E2545-85 16E254585 | 1680-01-173-0453 | Panel, Control, Electrical-Electro | III End Item Identification: F-16 aircraft III Fsc Application Data: Aircraft accessory equipment III Type/Model Designation: F-16C/D air combat fighter, tail effectivity 5C 0001 9999 | Lockheed Martin Corporation (81755) | |
16E2545-99 16E254599 | 1680-01-173-0453 | Panel, Control, Electrical-Electro | III End Item Identification: F-16 aircraft III Fsc Application Data: Aircraft accessory equipment III Type/Model Designation: F-16C/D air combat fighter, tail effectivity 5C 0001 9999 | Lockheed Martin Corporation (81755) | |
16E2547-859 16E2547859 | 1680-01-235-6016 | Relay Assembly | END Item Identification: F-16C/D aircraft Functional Description: Landing gear no 2, flap drive bay, used on 16E2508-5 Type/Model Designation: Egypt peculiar; tail effectivity 4G 0015 9999 | Lockheed Martin Corporation (81755) | |
16E2547-871 16E2547871 | 1680-01-235-6016 | Relay Assembly | END Item Identification: F-16C/D aircraft Functional Description: Landing gear no 2, flap drive bay, used on 16E2508-5 Type/Model Designation: Egypt peculiar; tail effectivity 4G 0015 9999 | Lockheed Martin Corporation (81755) | |
16E2547-875 16E2547875 | 1680-01-295-5521 | Matrix Assembly | Lockheed Martin Corporation (81755) | ||
16E2552-1 16E25521 | 1680-01-108-5705 | Panel, Power Distribution | END Item Identification: F-16 Overall Width: 6.750 inches nominal Overall Height: 2.290 inches nominal | Lockheed Martin Corporation (81755) | |
16E2552-233 16E2552233 | 1680-01-208-4057 | Matrix Assy, Elec Po | Lockheed Martin Corporation (81755) | ||
16E2552-3 16E25523 | 1680-01-108-5705 | Panel, Power Distribution | END Item Identification: F-16 Overall Width: 6.750 inches nominal Overall Height: 2.290 inches nominal | Lockheed Martin Corporation (81755) | |
16E2552-805 16E2552805 | 1680-01-108-5705 | Panel, Power Distribution | END Item Identification: F-16 Overall Width: 6.750 inches nominal Overall Height: 2.290 inches nominal | Lockheed Martin Corporation (81755) | |
16E2552-849 16E2552849 | 1680-01-173-5610 | Panel, Power Distribution | END Item Identification: F-16 aircraft FSC Application Data: Aircraft accessory equipment Functional Description: Landing gear and engine | Lockheed Martin Corporation (81755) | |
16E2552-875 16E2552875 | 1680-01-173-5610 | Panel, Power Distribution | END Item Identification: F-16 aircraft FSC Application Data: Aircraft accessory equipment Functional Description: Landing gear and engine | Lockheed Martin Corporation (81755) | |
16E3149-1 16E31491 | 1680-01-161-5585 | Matrix Assembly | III End Item Identification: F-16C/D aircraft General Characteristics Item Description: C/O relay P/NC4370-1;HARNESS P/N H16DW1209-200;PANEL P/N H16DW1209-9;ENCLOSURE assembly P/N H16DW1209-7;TAPE P/N P5393-1, P5374-1;SCREW P/N NAS1101-06-4;VERIFY heat treat per NDTS1500 III Fsc Application Data: Aircraft accessory equipment | Lockheed Martin Corporation (81755) |