Airframe Structural Components: DAA3132D902-007, DAA3132D903-006, DAA3132D953-008
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| DAA3132D902-007 DAA3132D902007 | 1560-01-318-7574 | 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 per BMS8-124, class iv, type V, gr 3, thk tolerance plus or minus .006; opposite -008 | The Boeing Company (81205) | |
| DAA3132D902-008 DAA3132D902008 | 1560-01-318-7575 | 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 honeycomp per BMS8-124, cl iv, ty V, gr 3, thk tolerance plus or minus .006; opp -007; dimensions listed are stock size | The Boeing Company (81205) | |
| DAA3132D902-009 DAA3132D902009 | 1560-01-469-7132 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item & smoothness critical; C/o: CORE(-003); matl:core-nomex honeycomb per BMS8-124 class iv, ty V, gr 3; thickness tolerance plus or minus .006; fin: F-14.67 plus F-19.62; opp -010 | The Boeing Company (81205) | |
| DAA3132D902-010 DAA3132D902010 | 1560-01-469-7473 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Nuclear hardness critical item and smoothness critical item;nha DAA3132B900;EFFECTIVITY R0009-R0016;C/O 1 -004 core;nomex honeycomb core per BMS8-124 class iv, type V, grade 3;THKNESS tolerence plus or minus .006;OPPOSITE -009;FINISH F-14.67 plus F-19.62 hcp except bag side surface Material: Plastic aramid | The Boeing Company (81205) | |
| DAA3132D902-011 DAA3132D902011 | 1560-01-469-7475 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Nha DAA3132B900;EFFECTIVITY R0017-R09999;OPPOSITE -012;NUCLEAR hardnesscritcal item and smoothness critical item;c/O 5 core (-013, -015, -017, -019, -023);NOMEX honeycomb core per BMS8-124 class iv, type V, grade 8;THKNESS tolerance plus or minus .006;FINISH F-14.67 plus F-19.62 hcp except bag sidefinish Material: Plastic aramid | The Boeing Company (81205) | |
| DAA3132D902-012 DAA3132D902012 | 1560-01-469-7474 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Nuclear hardness critical item and smoothness critical item;nha DAA3132B900;EFFECTIVITY R0017-R0999;OPPOSITE -011;C/O 5 cores (-014, -016, -018, -020, -024);NOMEX honeycomb core per BMC8-124 class iv, type V, grade 8; thkness tolerence plus or minus .006;FINISH F-14.67 plus F-19/62 hcp except bag side Material: Plastic aramid | The Boeing Company (81205) | |
| DAA3132D903-005 DAA3132D903005 | 1560-01-305-2232 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item & smoothesss 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) | |
| DAA3132D903-006 DAA3132D903006 | 1560-01-305-2233 | 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) | |
| DAA3132D904-007 DAA3132D904007 | 1560-01-305-2234 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Finish F-14.67 plus F-19.62;OPPOSITE -008;NHA DAA3132B900;NUCLEAR hardness critical item, smoothness critical item and hardness critical process Aircraft Location: Outboard trailing edge upper panel assembly | The Boeing Company (81205) | |
| DAA3132D904-008 DAA3132D904008 | 1560-01-305-2235 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Finish F-14.67 plus F-19.62;OPPOSITE -007;NHA DAA3132B900;NUCLEAR hardness critical item, smoothness critical item and hardness critical process Aircraft Location: Outboard trailing edge upper panel assembly | The Boeing Company (81205) | |
| DAA3132D905-001 DAA3132D905001 | 1560-01-305-2236 | 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) | |
| DAA3132D905-002 DAA3132D905002 | 1560-01-305-2237 | 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) | |
| DAA3132D952-007 DAA3132D952007 | 1560-01-318-7576 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item & smoothness critial item; core material: nomex honeycomb iaw BMS8-124, cl iv, ty V, gr 5, thk tolerance plus or minus .006; opposite -010 | The Boeing Company (81205) | |
| DAA3132D952-009 DAA3132D952009 | 1560-01-318-7576 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item & smoothness critial item; core material: nomex honeycomb iaw BMS8-124, cl iv, ty V, gr 5, thk tolerance plus or minus .006; opposite -010 | The Boeing Company (81205) | |
| DAA3132D952-011 DAA3132D952011 | 1560-01-458-7805 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item & smoothness critcal item; core matterial: nomex honeycomb per BMS8-124, cl iv, ty V, gr 5, thk tolerance plus or minus .006; opposite -012 | The Boeing Company (81205) | |
| DAA3132D952-012 DAA3132D952012 | 1560-01-458-7806 | 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 5, thk tolerance plus or minus .006; opposite -011 | The Boeing Company (81205) | |
| DAA3132D952-025 DAA3132D952025 | 1560-01-469-7469 | 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 | The Boeing Company (81205) | |
| DAA3132D952-026 DAA3132D952026 | 1560-01-469-7114 | 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 | The Boeing Company (81205) | |
| DAA3132D953-007 DAA3132D953007 | 1560-01-318-7578 | Panel, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critiacal item & smoothness critical item; core material: nomex honeycomb per BMS8-124, cl iv, ty V, gr 5, thk tolerance plus or minus .006; opposite -008; fin F-25.01 | The Boeing Company (81205) | |
| DAA3132D953-008 DAA3132D953008 | 1560-01-318-7579 | 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, thk tolerance plus or minus .006; fin F-25.01; opposite -007 | The Boeing Company (81205) |