Airframe Structural Components: J014011-511, J113186-1, J11760-17
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| J014011-511 J014011511 | 1560-01-386-3754 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F/A-18 Material: Aluminum alloy 7075 Material Document AND Classification: QQ-A-250/12 fed spec single material response | Boeing Company, The (8V613) | |
| J014011-513 J014011513 | 1560-01-386-3761 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F/A-18 Material: Aluminum alloy 7075 Material Document AND Classification: QQ-A-250/12 fed spec single material response | Boeing Company, The (8V613) | |
| J014011-515 J014011515 | 1560-01-386-3754 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F/A-18 Material: Aluminum alloy 7075 Material Document AND Classification: QQ-A-250/12 fed spec single material response | Boeing Company, The (8V613) | |
| J014088-505 J014088505 | 1560-01-545-0929 | Fairing, Aircraft | III End Item Identification: EF-18 hornet combat aircraft Part Name Assigned BY Controlling Agency: Fairing III FSC Application Data: Ejector unit rack assembly | Superform USA Inc. (66716) | |
| J014187-501 J014187501 | 1560-01-313-0191 | Fairing, Nose | III End Item Identification: Aircraft model F-18 | Boeing Company, The (88277) Superform USA Inc. (66716) | |
| J0K242A10C05176 | 1560-00-181-4554 | Insert, Instrument Panel | III End Item Identification: Aircraft model C5A | J.O. King Incorporated (24973) | |
| J100783-3 J1007833 | 1560-00-080-2875 | Cowling | McDonnell Douglas Corp. (88314) | ||
| J113186-1 J1131861 | 1560-01-211-2262 | Door, Aircraft | III End Item Identification: T-38 Special Features: Replaces pn 6-24301-523; this item has been determined to be a critical application item. in-flight failure of this item would create a hazardous condition Material: Titanium | Barnes Group Inc. (28622,32317) Boeing Company, The (88277) | |
| J113186-2 J1131862 | 1560-01-211-8982 | Door, Aircraft | III End Item Identification: T-38 Special Features: This item has been determined to be a critical application item. in-flight failure of this item would create a hazardous condition Material: Titanium | Barnes Group Inc. (28622,32317) Boeing Company, The (88277) Lockheed Martin Corporation (98897) The Boeing Company (17765) | |
| J114514-69 J11451469 | 1560-01-539-6011 | Fairing, Aircraft | III End Item Identification: Fairing ejection seat structure Special Features: To 13A5-56-11, fig-index 7-15-100; fabricate from AL2024 T-3.032 Material: Aluminum alloy 2024 | AMI Industries Inc. (31218) Universal Propulsion Company Inc. (51998) | |
| J114977-1B J1149771B | 1560-01-539-6010 | Fairing, Aircraft | III End Item Identification: Fairing, drogue compartment Special Features: To 13A5-56-11, fig-index 7-16-89 | AMI Industries Inc. (31218) Universal Propulsion Company Inc. (51998) | |
| J115083-1 J1150831 | 1560-01-336-8162 | Fitting, Structural Component, Air | III End Item Identification: 1680-01-159-9153 acft eject seat, S-3A/B acft Aircraft Mission Design Series: S-3A/B Special Features: Unapproved name, structure assy, aerodynamic vane, escapac | Boeing Company, The (88277) | |
| J115083-2 J1150832 | 1560-01-356-8838 | Fitting, Structural Component, Air | Material: Aluminum alloy 7072 Material Document and Classification: QQ-A-250/13 fed spec single material response Overall Length: 9.000 inches nominal | Boeing Company, The (88277) | |
| J115982-3 J1159823 | 1560-01-479-9148 | Pad Assembly, Back pad Assembly | III End Item Identification: J114582-1D;PAD assembly, back pad assembly | Boeing Company, The (88277) | |
| J115982-5 J1159825 | 1560-01-479-9146 | Pad Assembly, Back pad Assembly | III End Item Identification: J114582-1D;PAD assembly, back pad assembly | Boeing Company, The (88277) | |
| J11760-11 J1176011 | 1560-00-872-6766 | Support, Structural Component, Air | Special Features: Aluminum alloy, QQ-A-250/4, 9.120 in. lg, 1.100 in. W, 6 mtg HOLES0.250 in. min, 0.2515 in. max dia | Lord Corporation (76005) | |
| J11760-12 J1176012 | 1560-00-872-6765 | Support, Structural Component, Air | Special Features: Aluminum alloy, QQ-A-250/4, 9.120 in. lg, 1.100 in. W, 6 mtg HOLES0.250 in. min, 0.2515 in. max dia | Lord Corporation (76005) | |
| J11760-15 J1176015 | 1560-00-878-0328 | Support, Structural Component, Air | Special Features: 9.440 in. lg, 1.250 in. W, 6 mtg holes 0.250 in. min, 0.252 in. max dia | Lord Corporation (76005) | |
| J11760-16 J1176016 | 1560-00-878-0326 | Support, Structural Component, Air | Special Features: Aluminum alloy, QQ-A-225/6, 9.440 in. lg, 1.250 in. W, 6 mtg HOLES0.250 in. min, 0.252 in. max dia | Lord Corporation (76005) | |
| J11760-17 J1176017 | 1560-00-878-0323 | Support, Structural Component, Air | Special Features: 10.180 in.lg, 1.250 in.W, 6 mtg holes 0.250 in.min, 0.2515 in.max dia; | Lord Corporation (76005) |