Airframe Structural Components: 16L363-11, 16M043-4, 16M043-6
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
16L363-11 16L36311 | 1560-01-045-0349 | Bumper, Shank Arresting Hook | III End Item Identification: Acft model F-16 | Lockheed Martin Corporation (81755) | |
16L363-13 16L36313 | 1560-01-087-8961 | Bumper, Shank Arresting Hook | End Item Identification: Acft model F-16A/B General Characteristics Item Description: 2.09 in. wd, 4.48 in. lg; eff 0024 on; nha 16L005-3; superseded P/N 16L363-11 ow per ecn 72929 | Lockheed Martin Corporation (81755) | |
16L363-7 16L3637 | 1560-01-045-0349 | Bumper, Shank Arresting Hook | III End Item Identification: Acft model F-16 | Lockheed Martin Corporation (81755) | |
16L363-7 16L3637 | 1560-01-087-8961 | Bumper, Shank Arresting Hook | End Item Identification: Acft model F-16A/B General Characteristics Item Description: 2.09 in. wd, 4.48 in. lg; eff 0024 on; nha 16L005-3; superseded P/N 16L363-11 ow per ecn 72929 | Lockheed Martin Corporation (81755) | |
16L363-9 16L3639 | 1560-01-045-0349 | Bumper, Shank Arresting Hook | III End Item Identification: Acft model F-16 | Lockheed Martin Corporation (81755) | |
16L364-1 16L3641 | 1560-01-081-5176 | Bumper Assembly, Arresting Hook | III End Item Identification: Acft model F-16A/B General Characteristics Item Description: Consist of 3 bumper, 1 plate; 8.030 in. oa lg, 4.800 in. oa wd; matl cres 321 per MIL-S-6721 annealed; eff 61 0007 9999; nha 16L005-17; supeperseded P/N 16L364-1 ow per ecn 75900 | Lockheed Martin Corporation (81755) | |
16L364-3 16L3643 | 1560-01-081-5176 | Bumper Assembly, Arresting Hook | III End Item Identification: Acft model F-16A/B General Characteristics Item Description: Consist of 3 bumper, 1 plate; 8.030 in. oa lg, 4.800 in. oa wd; matl cres 321 per MIL-S-6721 annealed; eff 61 0007 9999; nha 16L005-17; supeperseded P/N 16L364-1 ow per ecn 75900 | Lockheed Martin Corporation (81755) | |
16L364-3 16L3643 | 1560-01-465-6379 | Hook, Arresting, Aircraft | Lockheed Martin Corporation (81755) | ||
16L364-5 16L3645 | 1560-01-465-6379 | Hook, Arresting, Aircraft | Lockheed Martin Corporation (81755) | ||
16M031-1 16M0311 | 1560-01-044-6231 | Plate, Structural, Aircraft | III End Item Identification: Acft model F-16A/B Special Features: Consist of 1 plate, 4 bushing; eff 0001 on; nha 16M030-3 | Lockheed Martin Corporation (81755) | |
16M031-3 16M0313 | 1560-01-172-4844 | Panel, Structural, Aircraft | Aircraft Mission Design Series: F-16C/D Special Features: Nha 16M030-5;EFF 0001-9999 | Aero Components Inc. (59213) Lockheed Martin Corporation (81755) Philip Specialty Company (64683) Schulz Products Inc. (56153) | |
16M036-1 16M0361 | 1560-01-046-5714 | Pivot, Leading Edge Drive System | III End Item Identification: Acft model F-16A/B General Characteristics Item Description: Eff 0001 on; nha 16M030-3 | Lockheed Martin Corporation (81755) | |
16M036-3 16M0363 | 1560-01-173-5307 | Pivot Assembly | End Item Identification: F-16C/D aircraft General Characteristics Item Description: Consist of 9 pivot bearing; matl cres PH13-8MO per ams 5629; finish S423; eff 5C 0001 9999; nha 16M030-5 | Lockheed Martin Corporation (81755) | |
16M039-13 16M03913 | 1560-01-276-1925 | Support, Structural Component, Air | End Item Identification: F-16C/D aircraft Supplementary Features: Functional description:support-forward, leading edge drive | Lockheed Martin Corporation (81755) | |
16M039-17 16M03917 | 1560-01-276-1925 | Support, Structural Component, Air | End Item Identification: F-16C/D aircraft Supplementary Features: Functional description:support-forward, leading edge drive | Lockheed Martin Corporation (81755) | |
16M039-9 16M0399 | 1560-01-043-3795 | Support, Drive | III End Item Identification: Acft model F-16 General Characteristics Item Description: 4.30 in. O/a lg, 4.150 in. O/a W, 0.75 in. O/a H | Lockheed Martin Corporation (81755) | |
16M042-13 16M04213 | 1560-01-469-3341 | Bracket, Structural Component, Air | End Item Identification: Nha: P/N-16M004, CAGE-81755 Part Name Assigned BY Controlling Agency: Mount, asymmetry brake - leading edge drive system Aircraft Mission Design Series: F-16ACFT | Lockheed Martin Corporation (81755) | |
16M042-14 16M04214 | 1560-01-087-8956 | Mount, Asymmetry Brake | End Item Identification: F-16 acft General Characteristics Item Description: 17-4PH cres steel per AMS-5343 | Lockheed Martin Corporation (81755) | |
16M042-15 16M04215 | 1560-01-087-8956 | Mount, Asymmetry Brake | End Item Identification: F-16 acft General Characteristics Item Description: 17-4PH cres steel per AMS-5343 | Lockheed Martin Corporation (81755) | |
16M043-2 16M0432 | 1560-01-043-4629 | Mount, Angle Gear box, Leading Edg | III End Item Identification: Acft model F-16A/B General Characteristics Item Description: Eff 0007 on; nha 16M005-2; superseded P/N 16M043-4 ow per ecn 47080 | Lockheed Martin Corporation (81755) | |
16M043-4 16M0434 | 1560-01-043-4629 | Mount, Angle Gear box, Leading Edg | III End Item Identification: Acft model F-16A/B General Characteristics Item Description: Eff 0007 on; nha 16M005-2; superseded P/N 16M043-4 ow per ecn 47080 | Lockheed Martin Corporation (81755) | |
16M043-6 16M0436 | 1560-01-043-4629 | Mount, Angle Gear box, Leading Edg | III End Item Identification: Acft model F-16A/B General Characteristics Item Description: Eff 0007 on; nha 16M005-2; superseded P/N 16M043-4 ow per ecn 47080 | Lockheed Martin Corporation (81755) |