Airframe Structural Components: 16T7303-17, 16T7305-17, 16T7306-11
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 16T7303-17 16T730317 | 1560-01-045-1834 | Core, Rudder | III End Item Identification: Acft model F-16 General Characteristics Item Description: Stock size 4.00 in.width, 4.00 in.height, 22.00 in.length | Lockheed Martin Corporation (81755) | |
| 16T7303-19 16T730319 | 1560-01-045-1835 | Core, Rudder | III End Item Identification: Acft model F-16 General Characteristics Item Description: Stock size 1.00 in.width, 2.00 in.heigth, 7.00 in.length | Lockheed Martin Corporation (81755) | |
| 16T7303-27 16T730327 | 1560-01-044-1789 | Former, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: Frame assembly; C/O -43 shim 2.6 X 2 in.; P/N 16T7304-15 spar; P/N 16T7305-19 and -21 ribs; -23 shim, -15 -17 -19 core P190-1D, -13 adhesive FMS-1116 form 3, -21 adhesive P6150-1, -29 prime FMS-3018 form 2;NHA 16T7303-809;EFF on 0008 on Aircraft Location: Rudder assembly | Lockheed Martin Corporation (81755) | |
| 16T7303-39 16T730339 | 1560-01-044-1789 | Former, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: Frame assembly; C/O -43 shim 2.6 X 2 in.; P/N 16T7304-15 spar; P/N 16T7305-19 and -21 ribs; -23 shim, -15 -17 -19 core P190-1D, -13 adhesive FMS-1116 form 3, -21 adhesive P6150-1, -29 prime FMS-3018 form 2;NHA 16T7303-809;EFF on 0008 on Aircraft Location: Rudder assembly | Lockheed Martin Corporation (81755) | |
| 16T7303-49 16T730349 | 1560-01-044-1789 | Former, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: Frame assembly; C/O -43 shim 2.6 X 2 in.; P/N 16T7304-15 spar; P/N 16T7305-19 and -21 ribs; -23 shim, -15 -17 -19 core P190-1D, -13 adhesive FMS-1116 form 3, -21 adhesive P6150-1, -29 prime FMS-3018 form 2;NHA 16T7303-809;EFF on 0008 on Aircraft Location: Rudder assembly | Lockheed Martin Corporation (81755) | |
| 16T7303-55 16T730355 | 1560-01-044-1789 | Former, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: Frame assembly; C/O -43 shim 2.6 X 2 in.; P/N 16T7304-15 spar; P/N 16T7305-19 and -21 ribs; -23 shim, -15 -17 -19 core P190-1D, -13 adhesive FMS-1116 form 3, -21 adhesive P6150-1, -29 prime FMS-3018 form 2;NHA 16T7303-809;EFF on 0008 on Aircraft Location: Rudder assembly | Lockheed Martin Corporation (81755) | |
| 16T7303-59 16T730359 | 1560-01-044-1789 | Former, Aircraft | Aircraft Mission Design Series: F-16A/B Special Features: Frame assembly; C/O -43 shim 2.6 X 2 in.; P/N 16T7304-15 spar; P/N 16T7305-19 and -21 ribs; -23 shim, -15 -17 -19 core P190-1D, -13 adhesive FMS-1116 form 3, -21 adhesive P6150-1, -29 prime FMS-3018 form 2;NHA 16T7303-809;EFF on 0008 on Aircraft Location: Rudder assembly | Lockheed Martin Corporation (81755) | |
| 16T7303-811 16T7303811 | 1560-01-527-5710 | Rudder, Aircraft | Part Name Assigned BY Controlling Agency: Rudder assembly | Lockheed Martin Corporation (81755) | |
| 16T7303-817 16T7303817 | 1560-01-419-3717 | Rudder, Aircraft | Aircraft Mission Design Series: F-16 Material: Aluminum alloy Aircraft Location: Vertical stabilizer | Lockheed Martin Corporation (81755) | |
| 16T7303-9 16T73039 | 1560-01-500-3518 | Trailing Edge, Aircraft | Lockheed Martin Corporation (81755) | ||
| 16T7304-13 16T730413 | 1560-01-043-0949 | Spar, Rudder | III End Item Identification: Aircraft model F-16 Special Features: For vertical stabilizer | Lockheed Martin Corporation (81755) | |
| 16T7304-15 16T730415 | 1560-01-043-0949 | Spar, Rudder | III End Item Identification: Aircraft model F-16 Special Features: For vertical stabilizer | Lockheed Martin Corporation (81755) | |
| 16T7304-7 16T73047 | 1560-01-043-0949 | Spar, Rudder | III End Item Identification: Aircraft model F-16 Special Features: For vertical stabilizer | Lockheed Martin Corporation (81755) | |
| 16T7304-9 16T73049 | 1560-01-043-0949 | Spar, Rudder | III End Item Identification: Aircraft model F-16 Special Features: For vertical stabilizer | Lockheed Martin Corporation (81755) | |
| 16T7305-11 16T730511 | 1560-01-043-0947 | Rib, Airfoil | III End Item Identification: F-16 Material Document and Classification: Fms 3002 T851 mfr ref single material response Overall Length: 33.000 inches nominal | Lockheed Martin Corporation (81755) | |
| 16T7305-15 16T730515 | 1560-01-043-0947 | Rib, Airfoil | III End Item Identification: F-16 Material Document and Classification: Fms 3002 T851 mfr ref single material response Overall Length: 33.000 inches nominal | Lockheed Martin Corporation (81755) | |
| 16T7305-17 16T730517 | 1560-01-043-0947 | Rib, Airfoil | III End Item Identification: F-16 Material Document and Classification: Fms 3002 T851 mfr ref single material response Overall Length: 33.000 inches nominal | Lockheed Martin Corporation (81755) | |
| 16T7305-21 16T730521 | 1560-01-043-0947 | Rib, Airfoil | III End Item Identification: F-16 Material Document and Classification: Fms 3002 T851 mfr ref single material response Overall Length: 33.000 inches nominal | Lockheed Martin Corporation (81755) | |
| 16T7305-7 16T73057 | 1560-01-043-0947 | Rib, Airfoil | III End Item Identification: F-16 Material Document and Classification: Fms 3002 T851 mfr ref single material response Overall Length: 33.000 inches nominal | Lockheed Martin Corporation (81755) | |
| 16T7306-11 16T730611 | 1560-01-043-4666 | Rib, Rudder | III End Item Identification: Acft model F-16 | Lockheed Martin Corporation (81755) |