Airframe Structural Components: 16B4460-6, 16B4460-802, 16B4505-159
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 16B4460-6 16B44606 | 1560-01-045-6844 | Beam, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: C/O:BEAM(16B4460-22), QQ-A-250/4, 19.000IN lg, 9.000IN wd, 0.040IN thk, DOUBLER(16B4460-23) & assorted hdwre; superseded P/N 16B4460-802 ni per ecn 93818;NHA 16B410-77;EFF:61-0014-0261 | Lockheed Martin Corporation (81755) | |
| 16B4460-802 16B4460802 | 1560-01-107-5340 | Beam Assembly, Avonics bay | III End Item Identification: Acft model F-16A/B usaf General Characteristics Item Description: C/O stiffener 1 ea P/N 16B4460-14, bracket 2 ea P/N 12B4460-16, stiffener 1 ea P/N 16B4460-18, beam 1 ea P/N 16B4460-30, plate 1 ea P/N 16B4460-31, plate 1 ea P/N 16B4460-33, cap 1 ea P/N 16B4460-36, rh, located from fs 217 to 236; superseded P/N 16B4460-802 ow per ecn 5B379; eff on 61-0262-9999; nha 16B410-99 | Lockheed Martin Corporation (81755) | |
| 16B4460-803 16B4460803 | 1560-01-107-8207 | Beam Assembly, Avionics bay | III End Item Identification: Acft model F-16A/B usaf General Characteristics Item Description: C/O stiffener 1 ea P/N 16B4430-13, bracket 2 ea P/N 16B4460-15, stiffener 1 ea P/N 16B4460-17, plate 1 ea P/N 16B4460-23 and -33, cap 1 ea P/N 16B4460-35, beam 1 ea P/N 16B4460-37, located from fs 217 to fs 236; superseded P/N 16B4460-5 ni per ecn 93264; nha 16B410-99 | Lockheed Martin Corporation (81755) | |
| 16B4460-806 16B4460806 | 1560-01-107-5340 | Beam Assembly, Avonics bay | III End Item Identification: Acft model F-16A/B usaf General Characteristics Item Description: C/O stiffener 1 ea P/N 16B4460-14, bracket 2 ea P/N 12B4460-16, stiffener 1 ea P/N 16B4460-18, beam 1 ea P/N 16B4460-30, plate 1 ea P/N 16B4460-31, plate 1 ea P/N 16B4460-33, cap 1 ea P/N 16B4460-36, rh, located from fs 217 to 236; superseded P/N 16B4460-802 ow per ecn 5B379; eff on 61-0262-9999; nha 16B410-99 | Lockheed Martin Corporation (81755) | |
| 16B4501-11 16B450111 | 1560-01-123-3891 | Cover Assembly | III End Item Identification: Acft model F-16A/B usaf General Characteristics Item Description: Location-avionics bay-fs 217.00 to fs 243.00, left hand; components-stifeener 1, cover 1, grommet 46, as required rivet; eff on 61-0004-9999; nha 16B4501-805 | Lockheed Martin Corporation (81755) | |
| 16B4501-15 16B450115 | 1560-01-161-5582 | Cover, Access | Material: Aluminum alloy 2024 END Item Identification: Acft model F16 Special Features: Access-avionics;fuselage sta 217 to 243 | Hellenic Aerospace Industry SA EAV (5U422) Israel Aircraft Industries LTD (1BG25) Lockheed Martin Corporation (81755) | |
| 16B4501-21 16B450121 | 1560-01-397-0156 | Cover, Access, Aircraft | Special Features: Lh avionics bay FS217 to FS243 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4-T62 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 16B4501-805 16B4501805 | 1560-01-045-0409 | Plate, Structural, Aircraft | III End Item Identification: Acft model F-16A/B usaf Special Features: Nha 16B410-67; eff on 0004-ON | Lockheed Martin Corporation (81755) | |
| 16B4502-1 16B45021 | 1560-01-117-8422 | Cover, Access, Aircraft | End Item Identification: Acft model F-16 Special Features: Alum alloy per QQ-A-250-T81, 12.00 in lg, 5.000 in wd, 0.063 in thk | Lockheed Martin Corporation (81755) | |
| 16B4502-11 16B450211 | 1560-01-117-8422 | Cover, Access, Aircraft | End Item Identification: Acft model F-16 Special Features: Alum alloy per QQ-A-250-T81, 12.00 in lg, 5.000 in wd, 0.063 in thk | Lockheed Martin Corporation (81755) | |
| 16B4502-9 16B45029 | 1560-01-047-2323 | Cover, Access | Material: Aluminum alloy 2024 END Item Identification: Acft model F-16A/B usaf Special Features: Eff on 0004-ON; nha 16B415-3 | Lockheed Martin Corporation (81755) | |
| 16B4503-9 16B45039 | 1560-01-057-3404 | Cover, Trunnion Pin | End Item Identification: Acft model F-16A/B usaf General Characteristics Item Description: Alum.alloy, per QQ-A-250/4-T81, stock size 0.050 in.thick, 3.00 in.wide, 4.00 in.length, located at fuselage station 194.00; eff on 0004-ON; nha 16B410-67 | Lockheed Martin Corporation (81755) | |
| 16B4504-11 16B450411 | 1560-01-282-8724 | Cover, Access | Material: Aluminum alloy END Item Identification: F-16A/B aircraft Securing Device Type: Threaded fastener | Lockheed Martin Corporation (81755) | |
| 16B4504-13 16B450413 | 1560-01-282-8723 | Cover, Access | Material: Aluminum alloy END Item Identification: F-16A/B aircraft Securing Device Type: Threaded fastener | Lockheed Martin Corporation (81755) | |
| 16B4505-135 16B4505135 | 1560-01-182-2897 | Skin, Aircraft | III End Item Identification: F-16 Special Features: Retrofit;replaces 16B4505-69;TCTO 16W37-7-501;ECP 0610 | Lockheed Martin Corporation (81755) | |
| 16B4505-137 16B4505137 | 1560-01-182-2898 | Door Assy, Avion | Lockheed Martin Corporation (81755) | ||
| 16B4505-139 16B4505139 | 1560-01-182-2899 | Door, Access, Aircraft | Material: Aluminum alloy End Item Identification: Avionics bay, F-16 aircraft Securing Device Type: Hinge | Lockheed Martin Corporation (81755) | |
| 16B4505-149 16B4505149 | 1560-01-182-2900 | Panel, Structural, Aircraft | III End Item Identification: F-16 Special Features: Retrofit;tcto 16W37-7-501;ECP 0610;REPLACES 16B4505-73 | Lockheed Martin Corporation (81755) | |
| 16B4505-151 16B4505151 | 1560-01-169-5201 | Door, Access, Aircraft | Special Features: Avionics bay, fs 217.00 to 243.00, rh Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 16B4505-159 16B4505159 | 1560-01-467-5577 | Door, Access, Aircraft | Material: Aluminum alloy End Item Identification: R.H. door, avionics bay, F-16 aircraft Securing Device Type: Hinge | Lockheed Martin Corporation (81755) |