Airframe Structural Components: DAA3132D707-005, DAA3132D710-015, DAA3132D712-015
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
DAA3132D707-005 DAA3132D707005 | 1560-01-305-2217 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: C/O 1 core;nha DAA3132B700;OPPOSITE -006;FINISH F-14.67 plus F-19.62;NUCLEAR hardness critical item, smoothness critical item and hardness critical process | The Boeing Company (81205) | |
DAA3132D707-006 DAA3132D707006 | 1560-01-305-2218 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: C/O 1 core;nha DAA3132B700;OPPOSITE -005;FINISH F-14.67 plus F-19.62;NUCLEAR hardness critical item, smoothness critical item and hardness criticalprocess | The Boeing Company (81205) | |
DAA3132D708-005 DAA3132D708005 | 1560-01-318-7590 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: C/O 1 core;nha DAA3132B700;OPPOSITE -006;FINISH F-14.67 plus F-19.62;NUCLEAR hardness critical item, smoothness critical item and hardness criticalprocess Aircraft Location: Bonded part outboard trailing edge upper panel | The Boeing Company (81205) | |
DAA3132D708-006 DAA3132D708006 | 1560-01-318-7591 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: C/O 1 core;nha DAA3132B700;OPPOSITE -005;FINISH F-14.67 plus F-19.62;NUCLEAR hardness critical item, smoothness critical item and hardness critical process Aircraft Location: Bonded part outboard trailing edge upper panel | The Boeing Company (81205) | |
DAA3132D709-013 DAA3132D709013 | 1560-01-305-2219 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb; opp -014 | The Boeing Company (81205) | |
DAA3132D709-014 DAA3132D709014 | 1560-01-305-2220 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item & smoothness critical item; opp -013 | The Boeing Company (81205) | |
DAA3132D709-027 DAA3132D709027 | 1560-01-459-1271 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item & smoothness critical item; opp -028; core material: nomex honeycomb | The Boeing Company (81205) | |
DAA3132D709-028 DAA3132D709028 | 1560-01-459-1714 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Nuclear hardness critical item & smoothness critical item; opp -027; core material: nomex honeycomb Material: Plastic aramid | The Boeing Company (81205) | |
DAA3132D710-013 DAA3132D710013 | 1560-01-305-2221 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb; opposite -014 | The Boeing Company (81205) | |
DAA3132D710-014 DAA3132D710014 | 1560-01-305-2222 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb; opposite -013 Material: Plastic aramid | The Boeing Company (81205) | |
DAA3132D710-015 DAA3132D710015 | 1560-01-458-9943 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb; opposite -016 | The Boeing Company (81205) | |
DAA3132D710-016 DAA3132D710016 | 1560-01-459-1716 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb; opposite -015 | The Boeing Company (81205) | |
DAA3132D711-019 DAA3132D711019 | 1560-01-305-2223 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb; opposite -020 | The Boeing Company (81205) | |
DAA3132D711-020 DAA3132D711020 | 1560-01-305-2224 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item; core material: nomex honeycomb; opposite -019 | The Boeing Company (81205) | |
DAA3132D711-021 DAA3132D711021 | 1560-01-459-1713 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item; core material: nomex honeycomb; opposite -022 | The Boeing Company (81205) | |
DAA3132D711-022 DAA3132D711022 | 1560-01-458-9946 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb; opposite -021 | The Boeing Company (81205) | |
DAA3132D712-010 DAA3132D712010 | 1560-01-305-2226 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Finish F-14.67 plus F-19.62;C/O 2CORE;OPPOSITE -009;NHA DAA3132B700;NUCLEAR hardness critical item, smoothness critical item and hardness critical process Aircraft Location: Bonded part outboard trailing edge upper panel | The Boeing Company (81205) | |
DAA3132D712-013 DAA3132D712013 | 1560-01-305-2227 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Nha DAA3132B700;OPPOSITE -014;FINISH F-14.67 plus F-19.62;NUCLEAR hardness critical item, smoothness critical item and hardness critical process Aircraft Location: Bonded part outboard trailing edge upper panel | The Boeing Company (81205) | |
DAA3132D712-014 DAA3132D712014 | 1560-01-305-2228 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Opposite -013;NHA DAA3132B700;FINISH F-14.67 plus F-19.62;NUCLEAR hardness critical item, smoothness critical item and hardness critical process Aircraft Location: Bonded part outboard trailing edge upper panel | The Boeing Company (81205) | |
DAA3132D712-015 DAA3132D712015 | 1560-01-459-1710 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Nuclear hardness critical item, smoothness critical item;opposite -016 Aircraft Location: Bonded part outbd trailing edge upper panel | The Boeing Company (81205) |