Airframe Structural Components: C4WM1174-4, C4WM1245-11, C4WM1247-3
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| C4WM1174-4 C4WM11744 | 1560-00-908-0912 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7A Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250 fed spec single material response | Bombardier Aerospace Aerospace Div. (71867) | |
| C4WM1177-1 C4WM11771 | 1560-00-916-2531 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7A Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250 fed spec single material response | Bombardier Aerospace Aerospace Div. (71867) | |
| C4WM1177-2 C4WM11772 | 1560-00-979-3681 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7A Special Features: U/a:hinge bracket assy Aircraft Location: WING | Bombardier Aerospace Aerospace Div. (71867) DE Havilland Inc. (0HWZ3) | |
| C4WM1178-1 C4WM11781 | 1560-00-916-2554 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7A Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250 fed spec single material response | Bombardier Aerospace Aerospace Div. (71867) | |
| C4WM1178-2 C4WM11782 | 1560-00-868-5797 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7A Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250 fed spec single material response | Bombardier Aerospace Aerospace Div. (71867) | |
| C4WM1195-5 C4WM11955 | 1560-00-952-8269 | Arm Assembly, Hinge, Door | General Characteristics Item Description: Aluminum alloy, QQ-A-250/4 | Bombardier Aerospace Aerospace Div. (71867) | |
| C4WM1195-6 C4WM11956 | 1560-00-952-8221 | Arm Assembly, Hinge, Door | General Characteristics Item Description: Aluminum alloy, QQ-A-250/4 | Bombardier Aerospace Aerospace Div. (71867) | |
| C4WM1198-1 C4WM11981 | 1560-00-751-8750 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-7A Aircraft Location: Landing gear door Material Document and Classification: MIL-S-18729 mil spec single material response | Bombardier Aerospace Aerospace Div. (71867) DE Havilland Inc. (0HWZ3) | |
| C4WM1198-2 C4WM11982 | 1560-00-751-8751 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-7A Aircraft Location: Landing gear door Material Document and Classification: MIL-S-18729 mil spec single material response | Bombardier Aerospace Aerospace Div. (71867) | |
| C4WM1210-5 C4WM12105 | 1560-00-916-2489 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7A Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250 fed spec single material response | Bombardier Aerospace Aerospace Div. (71867) | |
| C4WM1210-6 C4WM12106 | 1560-00-435-1669 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7 Material: Aluminum alloy 2024 Aircraft Location: WING | Bombardier Aerospace Aerospace Div. (71867) | |
| C4WM1214-1 C4WM12141 | 1560-00-759-7522 | Plate, Flap arm | General Characteristics Item Description: Aluminum alloy, 2024-T4, QQ-A-250/4, 1.900 in. l, 0.880 in. W, 0.800 in. thk, 4 0.125 in. dia mtg holes | Bombardier Aerospace Aerospace Div. (71867) | |
| C4WM1225-3 C4WM12253 | 1560-00-866-9537 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-7A Material Document and Classification: QQ-A-250 fed spec single material response Overall Length: 4.160 inches nominal | Bombardier Aerospace Aerospace Div. (71867) | |
| C4WM1226-3 C4WM12263 | 1560-00-400-4418 | Hinge, Aircraft | Aircraft Mission Design Series: C-7A Overall Length: 3.700 inches nominal Overall Width: 3.510 inches nominal | Bombardier Aerospace Aerospace Div. (71867) | |
| C4WM1227-1 C4WM12271 | 1560-00-308-4417 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-7A Aircraft Location: Flap arm hinge Overall Length: 7.150 inches nominal | Bombardier Aerospace Aerospace Div. (71867) | |
| C4WM1227-3 C4WM12273 | 1560-00-308-4417 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-7A Aircraft Location: Flap arm hinge Overall Length: 7.150 inches nominal | Bombardier Aerospace Aerospace Div. (71867) | |
| C4WM1245-1 C4WM12451 | 1560-00-878-0315 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7A Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250 fed spec single material response | Bombardier Aerospace Aerospace Div. (71867) | |
| C4WM1245-11 C4WM124511 | 1560-00-369-7081 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7A featgmatl: aluminum | Bombardier Aerospace Aerospace Div. (71867) | |
| C4WM1246-1 C4WM12461 | 1560-00-240-4507 | Adapter, Aileron Control | General Characteristics Item Description: Aluminum, 5.190 in. lg, 4.160 in. W, 0.900 in. H | Bombardier Aerospace Aerospace Div. (71867) | |
| C4WM1247-3 C4WM12473 | 1560-00-707-6948 | Striker Plate Assem | Bombardier Aerospace Aerospace Div. (71867) |