Airframe Structural Components: 16B4212-5, 16B4213-807, 16B4215-9
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 16B4212-5 16B42125 | 1560-01-110-8042 | Frame, Aircraft | Aircraft Mission Design Series: F-16 Special Features: Nacelle aft inlet section Material: Aluminum alloy 2024 | Lockheed Martin Corporation (81755) | |
| 16B4212-7 16B42127 | 1560-01-048-8471 | Frame, Nacelle | III End Item Identification: Acft model F-16 General Characteristics Item Description: Located at fuselage station 203.35 | Lockheed Martin Corporation (81755) | |
| 16B4212-803 16B4212803 | 1560-01-110-8042 | Frame, Aircraft | Aircraft Mission Design Series: F-16 Special Features: Nacelle aft inlet section Material: Aluminum alloy 2024 | Lockheed Martin Corporation (81755) | |
| 16B4212-805 16B4212805 | 1560-01-110-8042 | Frame, Aircraft | Aircraft Mission Design Series: F-16 Special Features: Nacelle aft inlet section Material: Aluminum alloy 2024 | Lockheed Martin Corporation (81755) | |
| 16B4212-809 16B4212809 | 1560-01-110-6477 | Frame Assembly | III End Item Identification: Acft model F-16A/B General Characteristics Item Description: C/O 1 plate, 2 frame, 1 stiffener, misc hardware; nha 16B410-99; eff 61 0262 9999; superseded P/N 16B4212-809 ni per ecn 92895 | Lockheed Martin Corporation (81755) | |
| 16B4212-810 16B4212810 | 1560-01-110-8042 | Frame, Aircraft | Aircraft Mission Design Series: F-16 Special Features: Nacelle aft inlet section Material: Aluminum alloy 2024 | Lockheed Martin Corporation (81755) | |
| 16B4212-811 16B4212811 | 1560-01-110-6477 | Frame Assembly | III End Item Identification: Acft model F-16A/B General Characteristics Item Description: C/O 1 plate, 2 frame, 1 stiffener, misc hardware; nha 16B410-99; eff 61 0262 9999; superseded P/N 16B4212-809 ni per ecn 92895 | Lockheed Martin Corporation (81755) | |
| 16B4212-813 16B4212813 | 1560-01-110-8042 | Frame, Aircraft | Aircraft Mission Design Series: F-16 Special Features: Nacelle aft inlet section Material: Aluminum alloy 2024 | Lockheed Martin Corporation (81755) | |
| 16B4213-3 16B42133 | 1560-01-044-8898 | Frame, Nacelle | III End Item Identification: Acft model F-16A/B General Characteristics Item Description: Located at fuselage station 210.25; nha 16B410-67; eff 0001 on | Lockheed Martin Corporation (81755) | |
| 16B4213-4 16B42134 | 1560-01-044-8897 | Frame, Nacelle | III End Item Identification: Acft model F-16A/B General Characteristics Item Description: Located at fuselage station 210.25; nha 16B410-67; eff 0007 on | Lockheed Martin Corporation (81755) | |
| 16B4213-5 16B42135 | 1560-01-044-8897 | Frame, Nacelle | III End Item Identification: Acft model F-16A/B General Characteristics Item Description: Located at fuselage station 210.25; nha 16B410-67; eff 0007 on | Lockheed Martin Corporation (81755) | |
| 16B4213-805 16B4213805 | 1560-01-111-1815 | Frame Assembly | III End Item Identification: Acft model F-16 General Characteristics Item Description: C/O plate P/N 16B4213-49, frame P/N 16B4213-47, plate P/N 16B4213-45, stiffener P/N 16B4213-23, plate P/N 16B4213-19, stiffener P/N 16B4213-11, stiffener P/N 16B4213 | Lockheed Martin Corporation (81755) | |
| 16B4213-806 16B4213806 | 1560-01-115-2711 | Frame Assembly | III End Item Identification: Acft model F-16 General Characteristics Item Description: C/O plate P/N 16B4213-49, frame P/N 16B4213-48, plate P/N 16B4213-46, plate P/N 16B4213-20, stiffener P/N 16B4213-23, 2 ea. plate P/N 16B4213-41, stiffener P/N 16B4213-11, stiffener P/N 16B4213-9 | Lockheed Martin Corporation (81755) | |
| 16B4213-807 16B4213807 | 1560-01-111-1815 | Frame Assembly | III End Item Identification: Acft model F-16 General Characteristics Item Description: C/O plate P/N 16B4213-49, frame P/N 16B4213-47, plate P/N 16B4213-45, stiffener P/N 16B4213-23, plate P/N 16B4213-19, stiffener P/N 16B4213-11, stiffener P/N 16B4213 | Lockheed Martin Corporation (81755) | |
| 16B4213-809 16B4213809 | 1560-01-115-2711 | Frame Assembly | III End Item Identification: Acft model F-16 General Characteristics Item Description: C/O plate P/N 16B4213-49, frame P/N 16B4213-48, plate P/N 16B4213-46, plate P/N 16B4213-20, stiffener P/N 16B4213-23, 2 ea. plate P/N 16B4213-41, stiffener P/N 16B4213-11, stiffener P/N 16B4213-9 | Lockheed Martin Corporation (81755) | |
| 16B4213-811 16B4213811 | 1560-01-120-1865 | Frame Assembly | III End Item Identification: F-16 aircraft General Characteristics Item Description: Location-nacelle fuselage station 210.25; C/O-frame 1, stiffener 3, plate 5, as required rivet | Lockheed Martin Corporation (81755) | |
| 16B4215-11 16B421511 | 1560-01-045-0354 | Frame, Nose Landing Gear Duct | III End Item Identification: Acft model F-16A/B General Characteristics Item Description: Material spec.fms 1109, 3.500 in. high, 3.800 in. wide, 23.000 in. long; nha 16B410-77; eff 0007 on; superseded P/N 16B4215-9 ow per ecn 49967 | Lockheed Martin Corporation (81755) | |
| 16B4215-13 16B421513 | 1560-01-114-0340 | Frame, Duct | III End Item Identification: Acft model F-16 General Characteristics Item Description: Material spec fms 1109, 3.500 in.thk, 3.800 in.W, 23.000 in.lg, located at fs 203.35, used on nlg | Lockheed Martin Corporation (81755) | |
| 16B4215-15 16B421515 | 1560-01-114-0340 | Frame, Duct | III End Item Identification: Acft model F-16 General Characteristics Item Description: Material spec fms 1109, 3.500 in.thk, 3.800 in.W, 23.000 in.lg, located at fs 203.35, used on nlg | Aerospace & Commerical Technologies (1XKR3) Lockheed Martin Corporation (81755) | |
| 16B4215-9 16B42159 | 1560-01-045-0354 | Frame, Nose Landing Gear Duct | III End Item Identification: Acft model F-16A/B General Characteristics Item Description: Material spec.fms 1109, 3.500 in. high, 3.800 in. wide, 23.000 in. long; nha 16B410-77; eff 0007 on; superseded P/N 16B4215-9 ow per ecn 49967 | Lockheed Martin Corporation (81755) |