Northrop Grumman Systems Corporation NSN Parts: 2-74139-3 - 160D637175-1
FSC 1560 Airframe Structural Components
MFG SKU | NSN | Item Name | Details | CAGE Code | RFQ |
---|---|---|---|---|---|
2-74139-3 2741393 | 1560-01-132-6652 | Arbor, Aileron Control | III End Item Identification: F-5E acft | 76823 | |
128L10011-3 128L100113 | 1560-01-233-1457 | ARM | General Characteristics Item Description: Steel, per MIL-S-18729, comp 4130 and MIL-T-6736, comp 4130, C/O plate and tube; plate 2.874 in. lg, thk 0.125 in.; tube 1.062 in. lg | 26512, 61174 | |
2-73326-503 273326503 | 1560-01-142-3694 | ARM | III End Item Identification: Acft model T38 | 76823 | |
89LM1882-1 89LM18821 | 1560-00-626-1241 | ARM | 26512 | ||
89WM10223-1 89WM102231 | 1560-00-376-2576 | ARM | 26512, 61174 | ||
A51C31079-1 A51C310791 | 1560-00-304-8152 | Arm and Lever Assembly | III End Item Identification: Aircraft model F-14A | 26512, 61174 | |
123AMM11105-1 123AMM111051 | 1560-00-276-8693 | Arm Assembly | 26512, 61174 | ||
128CM10114-1 128CM101141 | 1560-00-970-9857 | Arm Assembly | 26512 | ||
128CM12218-5 128CM122185 | 1560-00-970-9892 | Arm Assembly | 26512, 61174 | ||
2-13712-7 2137127 | 1560-01-161-7177 | Arm Assembly | III End Item Identification: F-5 acft General Characteristics Item Description: Function-thruster and damper; location-forward canopy III Fsc Application Data: Aircraft structural component | 76823 | |
215-38111-6 215381116 | 1560-00-050-7953 | Arm Assembly | General Characteristics Item Description: Consists of one arm P/N 215-38111-7; two bearings P/N MS20201KP4A; one bearing P/N MS27261KSP4; one spacer P/N CVC1991-4-92 End Item Identification: AV8A aircraft | 61174 | |
160D521104-1 160D5211041 | 1560-01-029-7305 | Arm Assembly, Actuator Drive | III End Item Identification: A10A acft General Characteristics Item Description: Consists of 1 arm, MIL-A-21180, 7.520 in. lg, approx 1.250 in W, 0.945 in. hole, 2 bushings | 26512, 61174 | |
160D521104-3 160D5211043 | 1560-01-029-7305 | Arm Assembly, Actuator Drive | III End Item Identification: A10A acft General Characteristics Item Description: Consists of 1 arm, MIL-A-21180, 7.520 in. lg, approx 1.250 in W, 0.945 in. hole, 2 bushings | 26512 | |
2-74157-1 2741571 | 1560-00-766-1315 | Arm Assembly, Aileron | General Characteristics Item Description: Aluminum alloy, QQ-A-601, 4.860 in. lg | 76823 | |
2-74157-2 2741572 | 1560-00-765-1100 | Arm Assembly, Aileron | General Characteristics Item Description: Aluminum alloy, QQ-A-596 | 76823 | |
3-74157-1 3741571 | 1560-00-766-1315 | Arm Assembly, Aileron | General Characteristics Item Description: Aluminum alloy, QQ-A-601, 4.860 in. lg | 76823 | |
3-74157-2 3741572 | 1560-00-765-1100 | Arm Assembly, Aileron | General Characteristics Item Description: Aluminum alloy, QQ-A-596 | 76823 | |
3-40714-5 3407145 | 1560-00-503-7723 | Arm Assembly, cam Re | General Characteristics Item Description: Steel, 4130, MIL-S-18729, condition N, and MIL-S-6758, condition F4, 2.740 in. lg, 1.345 in. W, slot 1.340 in. long, 0.219 in. W on arm, thds no. 10 0.190-32NF-3A on shaft end | 76823 | |
128CE10141-1 128CE101411 | 1560-01-156-1003 | Arm Assembly, Canopy Aft Release | 26512 | ||
160D637175-1 160D6371751 | 1560-01-012-8480 | Arm Assembly, Door Drive, 7AIN Lan | General Characteristics Item Description: Aluminum alloy, QQ-A-250/12, alloy 7075, T7351 End Item Identification: Aircraft model A10 | 26512, 61174 |