Airframe Structural Components: 89T2002-7, 89TM1006-1, 89TM1810-4
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 89T2002-7 89T20027 | 1560-00-670-2525 | Elevator Assy | Northrop Grumman Systems Corporation (26512) | ||
| 89T2002-8 89T20028 | 1560-00-670-2526 | Elevator Assy | Northrop Grumman Systems Corporation (26512) | ||
| 89T2008-1 89T20081 | 1560-00-098-0949 | Tab, Balance | Northrop Grumman Systems Corporation (26512) | ||
| 89T2008-2 89T20082 | 1560-00-098-0950 | Tab Assembly | General Characteristics Item Description: Consists of one spotweld assy P/N 89T2008-4; one half hinge P/N89T2008-14; one half hinge P/N 89T2008-16; one half hinge P/N 89T2008-18; one rib P/N 89T2025-2; one rib P/N 89T2025-4; one beam P/N 89T2046-2; one beam P/N 89T2046-4; one beam P/N 89T2046-6; one fitting P/N 89TM2059-1Z; one fitting P/N 89TM2075-1; one block P/N 89PH2010-1; one block P/N 89PH2010-2; rivets | Northrop Grumman Systems Corporation (26512) | |
| 89TM1002-1 89TM10021 | 1560-00-047-1981 | Flap Hinge, Tail Ele | III End Item Identification: S-2 aircraft | Northrop Grumman Systems Corporation (26512) | |
| 89TM1003-1 89TM10031 | 1560-00-047-1982 | Flap Hinge, Tail Elevatator | General Characteristics Item Description: 3.527 in. min and 3.529 in. max lg, 2.730 in. min and 2.732 in. max distance btw knuckles, two holes reamed 0.311 in. min and 0.313 in. max dia | Northrop Grumman Systems Corporation (26512) | |
| 89TM1004-5 89TM10045 | 1560-00-670-2558 | Flap Hinge, Tail Ele | Special Features: Flap hinge, tail elevator | Northrop Grumman Systems Corporation (26512) | |
| 89TM1005-1 89TM10051 | 1560-00-454-0231 | Flap Hinge | Northrop Grumman Systems Corporation (26512) | ||
| 89TM1006-1 89TM10061 | 1560-00-455-9929 | Flap Hinge | Northrop Grumman Systems Corporation (26512) | ||
| 89TM1084-1 89TM10841 | 1560-00-047-1985 | Fitting Assy | III End Item Identification: Models 52F and X52F General Characteristics Item Description: 5.000 in. lg, two knuckles 0.435 in. min and 0.439 in. lg | Northrop Grumman Systems Corporation (26512) | |
| 89TM1089-1 89TM10891 | 1560-00-047-1986 | Fitting Assembly | III End Item Identification: OV-10 aircraft General Characteristics Item Description: Consists of 1 fitting, aluminum alloy, P/N 89TM1089-3; 4 seals, P/N G-S13K-1; 4 retainers, P/N G-R11A-1; 2 bearings | Northrop Grumman Systems Corporation (26512) | |
| 89TM1194-1 89TM11941 | 1560-00-373-5394 | Bolt Asy | Northrop Grumman Systems Corporation (26512) | ||
| 89TM1286-5 89TM12865 | 1560-00-454-0232 | Fitting Assy, Stabil | Northrop Grumman Systems Corporation (26512) | ||
| 89TM1539-1 89TM15391 | 1560-00-670-2559 | Horn Assy | Northrop Grumman Systems Corporation (26512) | ||
| 89TM1571-1 89TM15711 | 1560-00-047-1987 | Fitting Assembly | III End Item Identification: OV-10 aircraft General Characteristics Item Description: Consists of 1 fitting made of aluminum alloy P/N 89TM1571-3; 1 bearing | Northrop Grumman Systems Corporation (26512) | |
| 89TM1573-1 89TM15731 | 1560-00-047-1988 | Fitting Assy | III End Item Identification: Model S2F, tf and XS2F General Characteristics Item Description: Aluminum alloy, 8.505 in. lg; two holes reamed 0.232 in. min and 0.250 in. max dia, 0.995 in. min and 1.000 in. max lg | Northrop Grumman Systems Corporation (26512) | |
| 89TM1610-1 89TM16101 | 1560-00-047-1989 | Hinge Assembly | III End Item Identification: S-2 aircraft General Characteristics Item Description: Consists of 1 aluminum alloy hinge P/N 89TM1610-5; 1 bearing P/N B-4 | Northrop Grumman Systems Corporation (26512) | |
| 89TM1610-3 89TM16103 | 1560-00-047-1990 | Flap Hinge, Tail Rudder, Hinge, top | III End Item Identification: S-2 aircraft | Northrop Grumman Systems Corporation (26512) | |
| 89TM1751-1 89TM17511 | 1560-00-458-1731 | Fitting, Rudder tab | Associated Aircraft Manufacturing (56540) Northrop Grumman Systems Corporation (26512) | ||
| 89TM1810-4 89TM18104 | 1560-00-094-2935 | HORN | Northrop Grumman Systems Corporation (26512) |