Airframe Structural Components: 42911-41, 4-3908-8, 4-3999-22
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 42911-41 4291141 | 1560-01-600-6719 | Fitting, Structural Component, Air | Special Features: Stowage container instalation Material: Steel comp 4130 Overall Length: 3.5 inches nominal | Ancra International LLC (31272) | |
| 42-96115 4296115 | 1560-01-599-3145 | Panel, Structural, Aircraft | END Item Identification: C-130 aircaft Special Features: Form, fit and function Criticality Code Justification: FEAT | Hydro-Aire Inc. (81982) | |
| 42-96115-11 429611511 | 1560-01-599-9564 | Panel, Structural, Aircraft | END Item Identification: C-130 Criticality Code Justification: AGAV | Hydro-Aire Inc. (81982) | |
| 4303-G5315 4303G5315 | 1560-01-594-0370 | Serial Interfa, Spec | Measurement Systems Inc. (22978) | ||
| 4316984-144 4316984144 | 1560-01-590-3950 | Heat Shield, Exhaust | END Item Identification: F-22 raptor Part Name Assigned BY Controlling Agency: Heat, shield exhaust | United Technologies Corporation (77445) | |
| 4317576-827 4317576827 | 1560-01-589-0246 | Heat Shield, Exhaust | END Item Identification: F-22 raptor acft Reference Number Differentiating Characteristics: Sorce control drawing | United Technologies Corporation (77445) | |
| 4317576-828 4317576828 | 1560-01-589-0247 | Heat Shield, Exhaust | END Item Identification: F-22 raptor acft | United Technologies Corporation (77445) | |
| 4317576-829 4317576829 | 1560-01-589-0243 | Heat Shield, Exhaust | End Item Identification: F-22A raptor Special Features: Used on amns liner Reference Number Differentiating Characteristics: Source control drawing | United Technologies Corporation (77445) | |
| 4322293-08 432229308 | 1560-01-619-3224 | Duct Assembly, Bleed Air | End Item Identification: F119 Criticality Code Justification: AGAV | United Technologies Corporation (77445) | |
| 4-3426-1026 434261026 | 1560-01-617-5606 | Stiffener, Aircraft | END Item Identification: B-52 Part Name Assigned BY Controlling Agency: Stiffener rudder access panel | The Boeing Company (81205) | |
| 4-3426-1058 434261058 | 1560-01-617-5602 | Stiffener, Aircraft | END Item Identification: B-52 Part Name Assigned BY Controlling Agency: Stiffener rudder access panel | The Boeing Company (81205) | |
| 4-3426-1060 434261060 | 1560-01-617-5604 | Stiffener, Aircraft | END Item Identification: B-52 Part Name Assigned BY Controlling Agency: Stiffener rudder access panel | The Boeing Company (81205) | |
| 4-3426-1061 434261061 | 1560-01-617-5605 | Stiffener, Aircraft | END Item Identification: B-52 Part Name Assigned BY Controlling Agency: Stiffener rudder access panel | The Boeing Company (81205) | |
| 4-3426-1063 434261063 | 1560-01-617-5607 | Stiffener, Aircraft | END Item Identification: B-52 Part Name Assigned BY Controlling Agency: Stiffener rudder access panel | The Boeing Company (81205) | |
| 4-3426-1064 434261064 | 1560-01-617-5608 | Stiffener, Aircraft | END Item Identification: B-52 Part Name Assigned BY Controlling Agency: Stiffener rudder access panel | The Boeing Company (81205) | |
| 4-3426-1065 434261065 | 1560-01-618-0658 | Stiffener, Aircraft | END Item Identification: B-52 aircraft Part Name Assigned BY Controlling Agency: Stiffener rudder access panel | The Boeing Company (81205) | |
| 4-3426-501 43426501 | 1560-01-617-5600 | Stiffener, Aircraft | END Item Identification: B-52 Part Name Assigned BY Controlling Agency: Stiffener rudder access panel | The Boeing Company (81205) | |
| 4-3908-8 439088 | 1560-01-605-7129 | Spar, Aircraft | END Item Identification: B-52 aircraft Aircraft Mission Design Series: B52 Special Features: Heat treat T62 per ams 2270 or BAC5602 stock size bac 1517-441 X 59.0 | The Boeing Company (81205) | |
| 4391B1610-1 4391B16101 | 1560-01-615-3880 | Panel, Structural, Aircraft | The Boeing Company (81205) | ||
| 4-3999-22 4399922 | 1560-01-618-1135 | Stiffener, Aircraft | The Boeing Company (81205,82918) |