Airframe Structural Components: 89FM1062-1, 89HM10069-1, 89L1010-33
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 89FM1062-1 89FM10621 | 1560-00-047-1850 | Fitting, Structural Component, Air | III End Item Identification: S-2 aircraft Material: Aluminum | Northrop Grumman Systems Corporation (26512) | |
| 89FM1062-3 89FM10623 | 1560-00-047-1851 | Fitting Assembly | General Characteristics Item Description: Onsists of one fitting aluminum alloy QQ-A-354 P/N 89FM1062-7; two bearings P/N 89FM1110-1; one bearing P/N HAB-509 | Northrop Grumman Systems Corporation (26512) | |
| 89FM1928-1 89FM19281 | 1560-00-098-0881 | Handle | Northrop Grumman Systems Corporation (26512) | ||
| 89FM1929-3 89FM19293 | 1560-00-676-5136 | Support | Northrop Grumman Systems Corporation (26512) | ||
| 89FM1994-5 89FM19945 | 1560-00-626-0823 | Lever Assy, Arrestin | Northrop Grumman Systems Corporation (26512) | ||
| 89H1078-1 89H10781 | 1560-00-373-7765 | Pan, Drip, Tank Hydra | Northrop Grumman Systems Corporation (26512) | ||
| 89HM10067-1 89HM100671 | 1560-00-098-0889 | Bell Crank | Bore Diameter: 0.249 inches minimum and 0.250 inches maximum Bore Length: 1.220 inches minimum and 1.223 inches maximum Material: Steel | Northrop Grumman Systems Corporation (26512) | |
| 89HM10068-1 89HM100681 | 1560-00-373-5332 | CAM | Northrop Grumman Systems Corporation (26512) | ||
| 89HM10068-2 89HM100682 | 1560-00-373-5333 | CAM | Northrop Grumman Systems Corporation (26512) | ||
| 89HM10069-1 89HM100691 | 1560-00-373-5334 | Lever | Northrop Grumman Systems Corporation (26512) | ||
| 89HM10069-2 89HM100692 | 1560-00-373-5335 | Lever | Northrop Grumman Systems Corporation (26512) | ||
| 89HM10128-1 89HM101281 | 1560-00-373-5336 | PIN | Northrop Grumman Systems Corporation (26512) | ||
| 89HM10128-2 89HM101282 | 1560-00-373-5337 | PIN | Northrop Grumman Systems Corporation (26512) | ||
| 89HM10757-1 89HM107571 | 1560-00-631-8668 | Retainer, Hydraulic | Northrop Grumman Systems Corporation (26512) | ||
| 89HM1461-1 89HM14611 | 1560-00-373-5341 | Terminal | General Characteristics Item Description: Chrome-molybdenum steel, 4130, MIL-S-6758, 3.913 in. lg | Northrop Grumman Systems Corporation (26512) | |
| 89HM1558-1 89HM15581 | 1560-00-373-5342 | Terminal Assembly, Hydraulic, Wing | General Characteristics Item Description: Aluminum alloy 2014-T6, QQ-A-200/2, 3.056 in. lg, 1.250 in. dia ea end | Northrop Grumman Systems Corporation (26512) | |
| 89L1010-1 89L10101 | 1560-00-047-1892 | Door Asy | Northrop Grumman Systems Corporation (26512) | ||
| 89L1010-21 89L101021 | 1560-00-098-0903 | Door Asy | Northrop Grumman Systems Corporation (26512) | ||
| 89L1010-22 89L101022 | 1560-00-098-0904 | Door, Access, Aircraft | FSC Application Data: Airframe structural component | Northrop Grumman Systems Corporation (26512) | |
| 89L1010-33 89L101033 | 1560-00-630-8567 | Door Assy | Northrop Grumman Systems Corporation (26512) |