Airframe Structural Components: C4T1507-12, C4TM1312-1, C4TM1458-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| C4T1507-12 C4T150712 | 1560-00-072-1057 | 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) DE Havilland Inc. (0HWZ3) | |
| C4T1507-13 C4T150713 | 1560-00-072-1058 | 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) DE Havilland Inc. (0HWZ3) | |
| C4T1507-14 C4T150714 | 1560-00-072-1059 | 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) DE Havilland Inc. (0HWZ3) | |
| C4TM1058-1 C4TM10581 | 1560-00-907-2251 | Hinge, Aircraft | Aircraft Mission Design Series: C-7A Special Features: 6 mtg holes O.188 in. dia, connecting hole 1.249 to 1.2495 in. dia Material: Aluminum alloy 2024 | Bombardier Aerospace Aerospace Div. (71867) | |
| C4TM1060-1 C4TM10601 | 1560-00-907-2250 | Flap Hinge | General Characteristics Item Description: Aluminum alloy, QQ-A-250/4, 5.520 in. lg, 2.580 in. W, 0.580 in. min, 0.583 in. max H, 6 mtg holes 0.188 in. dia, connecting hole 1.2490 in. min, 1.2495 in. max dia | Bombardier Aerospace Aerospace Div. (71867) | |
| C4TM1255-1 C4TM12551 | 1560-00-726-7405 | Hinge, Aircraft | Aircraft Mission Design Series: C-7A Material: Aluminum alloy 2024 Aircraft Location: Rudder | Bombardier Aerospace Aerospace Div. (71867) | |
| C4TM1311-1 C4TM13111 | 1560-00-241-9172 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7A Special Features: Matl:alum alloy plate per QQ-A-3550R, bar per QQ-A-267 Aircraft Location: Top rudder | Bombardier Aerospace Aerospace Div. (71867) | |
| C4TM1312-1 C4TM13121 | 1560-00-484-7256 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C7A Material: Aluminum alloy 2024 Aircraft Location: Center rudder | Bombardier Aerospace Aerospace Div. (71867) | |
| C4TM1330-1 C4TM13301 | 1560-00-020-2676 | Stop, Gust, Rudder | General Characteristics Item Description: Aluminum alloy QQ-A-225/6 2024-T4, 5.350 in.lg, 2.500 in. dia 0.450 in. lg one end, 0.500 in. dia 4.900 in. lg 2ND end, 1/2-20UNF-2A thd 0.600 in. lg thd on 2ND end | Bombardier Aerospace Aerospace Div. (71867) | |
| C4TM1335-3 C4TM13353 | 1560-00-403-8754 | Support, Structural Component, Air | Aircraft Mission Design Series: C-7A | Bombardier Aerospace Aerospace Div. (71867) | |
| C4TM1340-1 C4TM13401 | 1560-00-759-5521 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-7A | Bombardier Aerospace Aerospace Div. (71867) | |
| C4TM1342-3 C4TM13423 | 1560-00-237-9761 | Support, Structural Component, Air | Aircraft Mission Design Series: C-7A | Bombardier Aerospace Aerospace Div. (71867) | |
| C4TM1342-5 C4TM13425 | 1560-00-916-2615 | Support, Structural Component, Air | Aircraft Mission Design Series: C-7A Material Document and Classification: QQ-A-250 fed spec single material response Overall Length: 2.850 inches nominal | Bombardier Aerospace Aerospace Div. (71867) | |
| C4TM1343-5 C4TM13435 | 1560-00-939-7644 | Arm Subassembly, Sta | Bombardier Aerospace Aerospace Div. (71867) | ||
| C4TM1411-1 C4TM14111 | 1560-00-397-7780 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7A Special Features: U/a: rib mounting bracket; matl: aluminum alloy Overall Length: 4.020 inches nominal | Bombardier Aerospace Aerospace Div. (71867) DE Havilland Inc. (0HWZ3) | |
| C4TM1421-11 C4TM142111 | 1560-00-457-0788 | Support, Structural Component, Air | III End Item Identification: Acft model C7A Special Features: Al alloy 2024-T4 per QQ-A-267, 1.500 in.W, 2.960 in.lg, used on elevator tab attachment | Bombardier Aerospace Aerospace Div. (71867) | |
| C4TM1422-11 C4TM142211 | 1560-00-410-1017 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7 | Bombardier Aerospace Aerospace Div. (71867) DE Havilland Inc. (0HWZ3) | |
| C4TM1457-1 C4TM14571 | 1560-00-481-7627 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7A Special Features: Matl: bracket hinge casting P/n: C4TC1457-1 Aircraft Location: Elevator tab | Bombardier Aerospace Aerospace Div. (71867) | |
| C4TM1457-2 C4TM14572 | 1560-00-481-7626 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7A Special Features: C/O:1 bracket hinge 3C4TC1457-2 Aircraft Location: Elevator tab | Bombardier Aerospace Aerospace Div. (71867) DE Havilland Inc. (0HWZ3) | |
| C4TM1458-1 C4TM14581 | 1560-00-428-1004 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7A Special Features: U/a: hinge bracket | Bombardier Aerospace Aerospace Div. (71867) |