Airframe Structural Components: DAA3144D397-093, DAA3146A575-016, DAA3146P102-114
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| DAA3144D397-093 DAA3144D397093 | 1560-01-304-2938 | Door, Access, Aircraft | End Item Identification: B-2 pacer special | Northrop Grumman Systems Corporation (1W025) | |
| DAA3144D397-105 DAA3144D397105 | 1560-01-304-2930 | Cover, Access, Aircraft | End Item Identification: B-2 pacer special | Northrop Grumman Systems Corporation (1W025) | |
| DAA3144D397-107 DAA3144D397107 | 1560-01-304-2938 | Door, Access, Aircraft | End Item Identification: B-2 pacer special | Northrop Grumman Systems Corporation (1W025) | |
| DAA3146A575-009 DAA3146A575009 | 1560-01-344-0335 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Nuclear hardness critical item;c/O 1 skin assy, 1 retainer panel, 1 inner skin, 207 rivet, 279 collar, 280 pin, 1 hex nut Aircraft Location: Removable panel assembly | Northrop Grumman Systems Corporation (1W025) | |
| DAA3146A575-010 DAA3146A575010 | 1560-01-344-0334 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Nuclear hardness critical item;c/O 1 skin assy, 1 retainer panel, 1 inner skin, 207 rivet, 279 collar, 280 pin, 1 hex nut Aircraft Location: Removable panel assembly | Northrop Grumman Systems Corporation (1W025) | |
| DAA3146A575-013 DAA3146A575013 | 1560-01-344-0335 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Nuclear hardness critical item;c/O 1 skin assy, 1 retainer panel, 1 inner skin, 207 rivet, 279 collar, 280 pin, 1 hex nut Aircraft Location: Removable panel assembly | Northrop Grumman Systems Corporation (1W025) | |
| DAA3146A575-014 DAA3146A575014 | 1560-01-344-0334 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Nuclear hardness critical item;c/O 1 skin assy, 1 retainer panel, 1 inner skin, 207 rivet, 279 collar, 280 pin, 1 hex nut Aircraft Location: Removable panel assembly | Northrop Grumman Systems Corporation (1W025) | |
| DAA3146A575-015 DAA3146A575015 | 1560-01-353-0905 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Nuclear hardness critical item and low observable item;nha DAA3640A001;C/O 1 skin assy, 1 retainer panel, 1 inner skin, 184 rivet, 270 collar, 270 pin Aircraft Location: Removable panel assembly | Northrop Grumman Systems Corporation (1W025) | |
| DAA3146A575-016 DAA3146A575016 | 1560-01-350-1412 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Nuclear hardness critical item and low observable;nha DAA3640A001;C/O 1SKIN assy, 1 retainer panel, 1 inner skin, 184 rivet, 270 collar, 270 pin Aircraft Location: Removable panel assembly | Northrop Grumman Systems Corporation (1W025) | |
| DAA3146P101-113 DAA3146P101113 | 1560-01-452-3079 | Windshield Panel, Aircraft | III End Item Identification: B-52 aircraft Nuclear Hardness Critical Feature: Hardened | Northrop Grumman Systems Corporation (1W025) | |
| DAA3146P101-114 DAA3146P101114 | 1560-01-452-3031 | Windshield Panel, Aircraft | Northrop Grumman Systems Corporation (1W025) | ||
| DAA3146P101-115 DAA3146P101115 | 1560-01-452-3079 | Windshield Panel, Aircraft | III End Item Identification: B-52 aircraft Nuclear Hardness Critical Feature: Hardened | Northrop Grumman Systems Corporation (1W025) | |
| DAA3146P101-116 DAA3146P101116 | 1560-01-452-3031 | Windshield Panel, Aircraft | Northrop Grumman Systems Corporation (1W025) | ||
| DAA3146P101-117 DAA3146P101117 | 1560-01-533-1463 | Windshield Panel, Aircraft | Northrop Grumman Systems Corporation (1W025) | ||
| DAA3146P101-118 DAA3146P101118 | 1560-01-532-8037 | Windshield Panel, Aircraft | Aircraft Mission Design Series: B-2 Special Features: Right front window Nuclear Hardness Critical Feature: Hardened | Northrop Grumman Systems Corporation (1W025) | |
| DAA3146P102-103 DAA3146P102103 | 1560-01-310-2054 | Windshield Panel, Aircraft | Northrop Grumman Systems Corporation (1W025) | ||
| DAA3146P102-107 DAA3146P102107 | 1560-01-310-2054 | Windshield Panel, Aircraft | Northrop Grumman Systems Corporation (1W025) | ||
| DAA3146P102-109 DAA3146P102109 | 1560-01-310-2054 | Windshield Panel, Aircraft | Northrop Grumman Systems Corporation (1W025) | ||
| DAA3146P102-113 DAA3146P102113 | 1560-01-452-2968 | Windshield Panel, Aircraft | III End Item Identification: B-52 aircraft Nuclear Hardness Critical Feature: Hardened | Northrop Grumman Systems Corporation (1W025) | |
| DAA3146P102-114 DAA3146P102114 | 1560-01-455-7044 | Windshield Panel, Aircraft | III End Item Identification: B-2 bomber Aircraft Mission Design Series: B-2 Aircraft Location: Window assembly - side, laminated | Northrop Grumman Systems Corporation (1W025) |