Airframe Structural Components: DAA3150D362-028, DAA3211A012-002, DAA3211D106-003
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| DAA3150D362-028 DAA3150D362028 | 1560-01-458-3908 | Plate, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item; manufacturer suggested name-rub strip; opp -027; N/A:DAA3150A515; heat treat to th 1050 per H-110;U/O 01002 & subq | Northrop Grumman Systems Corporation (1W025) | |
| DAA3150D362-029 DAA3150D362029 | 1560-01-458-3916 | Plate, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item; manufacturer suggested name-rub strip; opp -030; N/A:DAA3150A515; heat treat to th 1050 per H-110;U/O 01002 & subq | Northrop Grumman Systems Corporation (1W025) | |
| DAA3150D362-030 DAA3150D362030 | 1560-01-458-0372 | Plate, Structural, Aircraft | III End Item Identification: Pacer special Aircraft Mission Design Series: B-2 Special Features: Nuclear hardness critical item; manufacturer suggested name: rub strip; matl: cres sht, 17-7PH cond a; ht to th 1050 per H-110; opposite -029 | Northrop Grumman Systems Corporation (1W025) | |
| DAA3150D603-029 DAA3150D603029 | 1560-01-360-1272 | Fairing, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Nuclear hardness critical item, next assembly DAA3150A640 Material: Titanium | Northrop Grumman Systems Corporation (1W025) | |
| DAA3150D603-035 DAA3150D603035 | 1560-01-360-1277 | Fairing, Aircraft | Aircraft Mission Design Series: B-2 pacer special Special Features: Nuclear hardness critical item; nha DAA3150A640;USED as fairing lower rudder blade seal Overall Length: 47.000 inches nominal | Northrop Grumman Systems Corporation (1W025) | |
| DAA3150P363-111 DAA3150P363111 | 1560-01-449-5693 | Fairing, Aircraft | III End Item Identification: B-2 bomber Aircraft Mission Design Series: B-2 Special Features: This item contains hardness critical processes (hcp) for the nuclear effect(s) of over pressure/thermal | Northrop Grumman Systems Corporation (1W025) | |
| DAA3150P363-113 DAA3150P363113 | 1560-01-439-4914 | Fairing, Aircraft | End Item Identification: B-2 bomber aircraft Criticality Code Justification: NHCF Aircraft Location: Control surface fairing | Northrop Grumman Systems Corporation (1W025) | |
| DAA3211A011-001 DAA3211A011001 | 1560-01-350-5767 | Support, Structural Component, Air | III End Item Identification: B-2 bomber Aircraft Mission Design Series: B-2 Aircraft Location: Lower leakage sensing element | Northrop Grumman Systems Corporation (1W025) | |
| DAA3211A011-002 DAA3211A011002 | 1560-01-361-0069 | Support Assembly, Sensing Element | III End Item Identification: B-2 bomber General Characteristics Item Description: Cres, 0.500 in. thick; assembly C/O tube, brackets and clips | Northrop Grumman Systems Corporation (1W025) | |
| DAA3211A012-001 DAA3211A012001 | 1560-01-349-5323 | Support, Structural Component, Air | III End Item Identification: B-2 bomber, atb Aircraft Mission Design Series: B-2 Overall Length: 4.140 inches nominal | Northrop Grumman Systems Corporation (1W025) | |
| DAA3211A012-002 DAA3211A012002 | 1560-01-352-3756 | Support, Structural Component, Air | III End Item Identification: B-2 bomber Aircraft Mission Design Series: B-2 Aircraft Location: Lower leakage sensing element | Northrop Grumman Systems Corporation (1W025) | |
| DAA3211A0125-002 DAA3211A0125002 | 1560-01-352-3756 | Support, Structural Component, Air | III End Item Identification: B-2 bomber Aircraft Mission Design Series: B-2 Aircraft Location: Lower leakage sensing element | Northrop Grumman Systems Corporation (1W025) | |
| DAA3211A013-009 DAA3211A013009 | 1560-01-351-3761 | Support, Structural Component, Air | III End Item Identification: B-2 bomber/atb Aircraft Mission Design Series: B-2 Special Features: Material ams 5510 | Northrop Grumman Systems Corporation (1W025) | |
| DAA3211A013-010 DAA3211A013010 | 1560-01-350-5762 | Support, Structural Component, Air | III End Item Identification: B-2 bomber Aircraft Mission Design Series: B-2 | Northrop Grumman Systems Corporation (1W025) | |
| DAA3211A014-009 DAA3211A014009 | 1560-01-350-5766 | Support, Structural Component, Air | III End Item Identification: B-2 bomber Aircraft Mission Design Series: B-2 Aircraft Location: Upper leakage sensing element | Northrop Grumman Systems Corporation (1W025) | |
| DAA3211A014-010 DAA3211A014010 | 1560-01-350-5765 | Support, Structural Component, Air | III End Item Identification: B-2 bomber Aircraft Mission Design Series: B-2 Aircraft Location: Upper leakage sensing element | Northrop Grumman Systems Corporation (1W025) | |
| DAA3211A015-015 DAA3211A015015 | 1560-01-352-3755 | Support, Structural Component, Air | III End Item Identification: B-2 bomber Aircraft Mission Design Series: B-2 Aircraft Location: Mounted leakage valve sensing element | Northrop Grumman Systems Corporation (1W025) | |
| DAA3211A015-019 DAA3211A015019 | 1560-01-455-4079 | Support, Structural Component, Air | III End Item Identification: B-2 bomber Aircraft Mission Design Series: B-2 Aircraft Location: Support assembly - sensing element, leakage, valve mounted | Northrop Grumman Systems Corporation (1W025) | |
| DAA3211D106-001 DAA3211D106001 | 1560-01-433-2973 | Bracket, Structural Component, Air | III End Item Identification: B-1 aircraft III Part Name Assigned BY Controlling Agency: Retainer | Northrop Grumman Systems Corporation (1W025) | |
| DAA3211D106-003 DAA3211D106003 | 1560-01-433-2969 | Bracket, Structural Component, Air | III End Item Identification: B-1 bomber aircraft Special Features: Retainer | Northrop Grumman Systems Corporation (1W025) |