Airframe Structural Components: DAA3132D809-018, DAA3132D812-015, DAA3132D830-023
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| DAA3132D809-018 DAA3132D809018 | 1560-01-469-7134 | 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 -017 | The Boeing Company (81205) | |
| DAA3132D810-015 DAA3132D810015 | 1560-01-318-7566 | 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) | |
| DAA3132D810-016 DAA3132D810016 | 1560-01-318-7567 | 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) | |
| DAA3132D811-001 DAA3132D811001 | 1560-01-318-7568 | 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 -002 | The Boeing Company (81205) | |
| DAA3132D811-002 DAA3132D811002 | 1560-01-318-7569 | 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 -001 | The Boeing Company (81205) | |
| DAA3132D811-009 DAA3132D811009 | 1560-01-469-7466 | 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 -010 | The Boeing Company (81205) | |
| DAA3132D811-010 DAA3132D811010 | 1560-01-469-7111 | 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 -009 | The Boeing Company (81205) | |
| DAA3132D812-015 DAA3132D812015 | 1560-01-305-2231 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Finish F-14.67 plus F-19.62;NHA DAA3132B800;OPPOSITE -016;NUCLEAR hardness critical item, smoothness critical item and hardness critical process Aircraft Location: Bonded part outboard trailing edge lower panel | The Boeing Company (81205) | |
| DAA3132D812-016 DAA3132D812016 | 1560-01-307-6374 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Finish F-14.67 plus F-19.62;OPPOSITE -015;NHA DAA3132B800;NUCLEAR hardness critical item, smoothness critical item and hardness critical process Aircraft Location: Bonded part outboard trailing edge lower panel | The Boeing Company (81205) | |
| DAA3132D812-019 DAA3132D812019 | 1560-01-453-8457 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item; core matl: nomex honeycomb per BMS8-124, cl iv, ty V, gr 3, thk tolerance plus or minus .006; opposite -020 | The Boeing Company (81205) | |
| DAA3132D812-020 DAA3132D812020 | 1560-01-454-2702 | 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 matl: nomex honeycomb per BMS8-124, class iv, ty V, gr 8, thk tolerance plus or minus .006; opposite -019 | The Boeing Company (81205) | |
| DAA3132D813-001 DAA3132D813001 | 1560-01-318-7572 | 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 -002; matl: nomex honeycomb core per bms 8-124 cl iv, ty V, gr 5 thickness tolerance plus or minus .006; C/o: core (-005) | The Boeing Company (81205) | |
| DAA3132D813-002 DAA3132D813002 | 1560-01-318-7573 | 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 -001; matl: nomex honeycomb core per bms 8-124 cl iv, ty V, gr 5, thickness tolerance plus of minus .006; C/o: core (-006) | The Boeing Company (81205) | |
| DAA3132D813-007 DAA3132D813007 | 1560-01-399-8606 | 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-008; matl: nomex honeycomb core per bms 8-124, cl iv, ty V, gr 5, thickness tolerance plus or minus .006; C/o: core (-005) | The Boeing Company (81205) | |
| DAA3132D813-008 DAA3132D813008 | 1560-01-399-6792 | 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-007; matl: nomex honeycomb core per bms 8-124, cl iv, ty V, gr 5, thickness tolerance plus or minus .006; C/o: core (-006) | The Boeing Company (81205) | |
| DAA3132D813-009 DAA3132D813009 | 1560-01-469-7472 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Nuclear hardness critical item & smoothness critical item; opp -010; C/o: CORE(-006); matl: nomex honeycomb core per BMS8-124, cl iv, ty V, gr 5; thkness tolerance plus or minus .006 Material: Plastic aramid | The Boeing Company (81205) | |
| DAA3132D813-010 DAA3132D813010 | 1560-01-469-7872 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item & smoothness critical item; C/o: PANEL(-006); opposite -009; fin F-14.67 plus F-19.62; matl: nomex honeycomb core per BMS8-124 cl iv, ty 5, gr 5, thickness tolerance plus or minus .006 | The Boeing Company (81205) | |
| DAA3132D830 | 1560-01-477-8381 | Support, Structural Component, Air | Aircraft Mission Design Series: B-2 Aircraft Location: Lower trailing edge panel Overall Length: 2.510 inches nominal | The Boeing Company (81205) | |
| DAA3132D830 | 1560-01-477-8390 | Support, Structural Component, Air | Aircraft Mission Design Series: B-2 Aircraft Location: Lower trailing edge panel Overall Length: 1.740 inches nominal | The Boeing Company (81205) | |
| DAA3132D830-019 DAA3132D830019 | 1560-01-477-8381 | Support, Structural Component, Air | Aircraft Mission Design Series: B-2 Aircraft Location: Lower trailing edge panel Overall Length: 2.510 inches nominal | The Boeing Company (81205) | |
| DAA3132D830-023 DAA3132D830023 | 1560-01-477-8390 | Support, Structural Component, Air | Aircraft Mission Design Series: B-2 Aircraft Location: Lower trailing edge panel Overall Length: 1.740 inches nominal | The Boeing Company (81205) |