Airframe Structural Components: DAA3132D712-016, DAA3132D802-009, DAA3132D809-017
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| DAA3132D712-016 DAA3132D712016 | 1560-01-458-9945 | 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 -015 | The Boeing Company (81205) | |
| DAA3132D713-001 DAA3132D713001 | 1560-01-305-2229 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special | The Boeing Company (81205) | |
| DAA3132D713-002 DAA3132D713002 | 1560-01-305-2230 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special | The Boeing Company (81205) | |
| DAA3132D713-007 DAA3132D713007 | 1560-01-305-2229 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special | The Boeing Company (81205) | |
| DAA3132D713-008 DAA3132D713008 | 1560-01-305-2230 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special | The Boeing Company (81205) | |
| DAA3132D801-005 DAA3132D801005 | 1560-01-319-3732 | 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, cl iv, ty V, gr 3, thk tolerance plus or minus .006; opposite -006; dimensions listed are stock size | The Boeing Company (81205) | |
| DAA3132D801-006 DAA3132D801006 | 1560-01-319-3733 | 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, cl iv, ty V, gr 3, thk tolerence plus or minus .006; opposite -005; dimensions listed are stock size | The Boeing Company (81205) | |
| DAA3132D802-009 DAA3132D802009 | 1560-01-319-3734 | 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, cl iv, ty V, gr 3, thk tolerance plus or minus .006; opposite -010; dimensions listed are stock size | The Boeing Company (81205) | |
| DAA3132D802-010 DAA3132D802010 | 1560-01-319-3735 | 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, cl iv, ty V, gr 3, thk tolerance plus or minus .006; opposite -009; dimensions listed are stock size | The Boeing Company (81205) | |
| DAA3132D803-009 DAA3132D803009 | 1560-01-319-3736 | 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, cl iv, ty V, gr 3, thk tolerance plus or minus .006; opposite -010; dimensions listed are stock size | The Boeing Company (81205) | |
| DAA3132D803-010 DAA3132D803010 | 1560-01-319-3737 | 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, cl iv, ty V, gr 3, thk tolerance plus or minus .006; opposite -009; dimensions listed are stock size | The Boeing Company (81205) | |
| DAA3132D804-001 DAA3132D804001 | 1560-01-319-3738 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Nuclear hardness critical item Criticality Code Justification: FEAT | The Boeing Company (81205) | |
| DAA3132D804-002 DAA3132D804002 | 1560-01-319-3739 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Nuclear hardness critical item Criticality Code Justification: FEAT | The Boeing Company (81205) | |
| DAA3132D805-001 DAA3132D805001 | 1560-01-319-3740 | 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 per BMS8-124, cl iv, ty V, gr 3, thk tolerance plus or minus .006; opposite -002 | The Boeing Company (81205) | |
| DAA3132D805-002 DAA3132D805002 | 1560-01-318-7561 | 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 per BMS8-124, cl iv, ty V, gr 3, thk tolerance plus or minus .006; opposite -001 | The Boeing Company (81205) | |
| DAA3132D808-005 DAA3132D808005 | 1560-01-318-7562 | 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 per BMS8-124, cl iv, ty V, gr 3, thk tolerance plus or minus .006; opposite -006 | The Boeing Company (81205) | |
| DAA3132D808-006 DAA3132D808006 | 1560-01-318-7563 | 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 per BMS8-124, cl iv, ty V, gr 3, thk tolerance plus or minus .006; opposite -005 | The Boeing Company (81205) | |
| DAA3132D809-015 DAA3132D809015 | 1560-01-318-7564 | 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) | |
| DAA3132D809-016 DAA3132D809016 | 1560-01-318-7565 | 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) | |
| DAA3132D809-017 DAA3132D809017 | 1560-01-469-8428 | 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 -018 | The Boeing Company (81205) |