Airframe Structural Components: 32-19416-603, 32-19419-12, 32-19430-11
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 32-19416-603 3219416603 | 1560-01-089-8905 | Rib cap | III End Item Identification: Acft model F4C General Characteristics Item Description: Aluminum 7075-0 per QQ-A-200/11 COND-0, stock size IM124 X 13.500, installation part used on canted rib assembly inboard leading edge flap | Boeing Company, The (76301) | |
| 32-19416-604 3219416604 | 1560-01-087-3483 | Rib, Airfoil | Aircraft Mission Design Series: F-4C Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250 fed spec single material response | Boeing Company, The (76301) | |
| 32-19419-11 321941911 | 1560-01-053-7724 | Web, Airframe | III End Item Identification: Acft model F-4 | Boeing Company, The (76301) | |
| 32-19419-12 321941912 | 1560-00-614-0053 | Rib, Airfoil | Aircraft Mission Design Series: F4 Overall Length: 70.000 inches nominal Overall Width: 5.600 inches nominal | Boeing Company, The (76301) | |
| 32-19419-15 321941915 | 1560-01-080-8190 | Angle, Beam Assembly | III End Item Identification: Acft model 1F4C General Characteristics Item Description: Alum alloy 2024-0 per QQ-A-362 cohd 0, stock size 0.032 in.thick, 2.000 in.wide, 4.500 in.length, used on inboard leading edge flap, left hand | Boeing Company, The (76301) | |
| 32-19419-16 321941916 | 1560-01-081-1434 | Angle, Beam Assembly | III End Item Identification: Acft model F4C General Characteristics Item Description: Alum alloy 2024-0 per QQ-A-362 cond 0, stock size 0.032 in.thick, 2.00 in.wide, 4.50 in.length, right hand | Boeing Company, The (76301) | |
| 32-19419-19 321941919 | 1560-01-123-7280 | Bracket, Structural Component, Aircraft | Boeing Company, The (76301) | ||
| 32-19421-6 32194216 | 1560-00-788-6603 | Hinge half, Flap | III End Item Identification: Aircraft model F4 | Boeing Company, The (76301) | |
| 32-19421-7 32194217 | 1560-00-064-9399 | Hinge half, Flap | III End Item Identification: Aircraft model F4 | Boeing Company, The (76301) | |
| 32-19423-13 321942313 | 1560-00-114-2747 | Skin, Aircraft | Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/18-T6 fed spec single material response | Boeing Company, The (76301) | |
| 32-19423-13 321942313 | 1560-00-793-9992 | Skin, Aircraft | Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/18-T6 fed spec single material response | Boeing Company, The (76301) | |
| 32-19423-14 321942314 | 1560-00-114-2748 | Skin, Aircraft | III End Item Identification: Aircraft, F-4 Aircraft Mission Design Series: F-4 Material: Aluminum alloy 7075 | Boeing Company, The (76301) | |
| 32-19423-14 321942314 | 1560-00-793-9991 | Skin, Aircraft | Special Features: Aluminum alloy, QQ-A-250/18 7075-T6 | Boeing Company, The (76301) | |
| 32-19423-15 321942315 | 1560-00-114-2747 | Skin, Aircraft | Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/18-T6 fed spec single material response | Boeing Company, The (76301) | |
| 32-19423-16 321942316 | 1560-00-114-2748 | Skin, Aircraft | III End Item Identification: Aircraft, F-4 Aircraft Mission Design Series: F-4 Material: Aluminum alloy 7075 | Boeing Company, The (76301) | |
| 32-19425-3 32194253 | 1560-00-197-3705 | Bracket, Aircraft | III End Item Identification: F-4A/B/C/D acft General Characteristics Item Description: Function-inboard flap mechanism; location-inner wing leading edge | Boeing Company, The (76301) | |
| 32-19425-4 32194254 | 1560-00-917-8533 | Bracket, Inboard Flap | III End Item Identification: Aircraft model F4 General Characteristics Item Description: Aluminum alloy, 356-T6 | Boeing Company, The (76301) | |
| 32-19427-24 321942724 | 1560-00-435-9871 | Cover, Access, Aircraft | Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/13, T6 fed spec single material response Securing Device Type: Threaded fastener | Boeing Company, The (76301) | |
| 32-19427-25 321942725 | 1560-00-537-0522 | Plate, Structural, Aircraft | III End Item Identification: Aircraft model F4 | Boeing Company, The (76301) | |
| 32-19427-28 321942728 | 1560-01-084-0258 | Panel, Structural, Aircraft | Aircraft Mission Design Series: F-4C Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-287-T6 fed spec single material response | Boeing Company, The (76301) | |
| 32-19428-10 321942810 | 1560-01-087-2762 | Angle, Bracket Assembly | III End Item Identification: Acft model F4C General Characteristics Item Description: Alum alloy 2024-0 per QQ-A-362 cond 0, stock size 0.063 in.thick, 2.130 in.wide, 3.300 in.length, right hand | Boeing Company, The (76301) | |
| 32-19430-11 321943011 | 1560-01-222-2979 | Support, Structural Component, Air | Boeing Company, The (76301) |