FSC 1650 Aircraft Hydraulic, Vacuum and De-icing System Components: 1650-01-212-9528, 1650-01-213-2217, 1650-01-213-2263
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1650-01-212-9528 1650012129528 | 37437 | Lap Assy, Transfer m | Eaton Corporation (99643) | ||
| 1650-01-212-9534 1650012129534 | JETA1875120D | Orifice, Transfer Mo | The LEE Company (92555) | ||
| 1650-01-212-9792 1650012129792 | 3831454-1 | Clevis Assembly, Servocylinder | III End Item Identification: Aircraft F15 General Characteristics Item Description: Steel 15-5PH, ams 5659; C/O 3831454-3 clevis machining; 3831452-1 pin, retaining, roller; 3831453-1 roller | Parker-Hannifin Corporation (59211, 93835, 82106) | |
| 1650-01-212-9794 1650012129794 | 3831437-1 | Control, Pressurizing set | Parker-Hannifin Corporation (93835) | ||
| 1650-01-212-9795 1650012129795 | 3831444-1 | Retainer, cap Assembly | III End Item Identification: Aircraft F15 General Characteristics Item Description: Steel 15-5PH, ams 5659; 0.370 in. lg; 0.9375-16 UNJ-3A in. od thd; 0.680 in. id; 4 grooves 0.125 in. deep; 0.250 in. W | Parker-Hannifin Corporation (59211, 82106, 93835) | |
| 1650-01-212-9861 1650012129861 | 3831447-2 | Sleeve, Directional Control linea | Parker-Hannifin Corporation (82106, 59211, 93835) | ||
| 1650-01-213-0851 1650012130851 | 75A613807-2001 | Seat, Helical Compression Spring | Boeing Company, The (76301) | ||
| 1650-01-213-2012 1650012132012 | 123H40102-601 | Actuator Assembly | Northrop Grumman Systems Corporation (26512) | ||
| 1650-01-213-2014 1650012132014 | 123H40126-601 | Reservoir Assembly | Northrop Grumman Systems Corporation (26512) | ||
| 1650-01-213-2216 1650012132216 | 123SCEC100-601 25S-7D5074-23 | Boot, Deicer | III End Item Identification: Aircraft model C-2A Special Features: 67.000 in. lg, 17.000 in. W, 0.300 in. H, wt 4.40 lb | Bfgoodrich Co., The (03481) Goodrich Corporation (3K820, 0AJJ0) Northrop Grumman Systems Corporation (26512) | |
| 1650-01-213-2217 1650012132217 | 25S-7D5074-24 123SCEC100-602 | Boot, Deicer | III End Item Identification: Aircraft model C-2A Special Features: Height: 0.300IN Overall Length: 67.000 inches nominal | Northrop Grumman Systems Corporation (26512) Bfgoodrich Co., The (03481) | |
| 1650-01-213-2218 1650012132218 | 123SCEC100-619 26S-7D5074-17 | Boot, Deicer | III End Item Identification: Aircraft model C-2A Special Features: Height: 0.300IN Overall Length: 98.000 inches nominal | Goodrich Corporation (0AJJ0) Northrop Grumman Systems Corporation (26512) Bfgoodrich Co., The (03481) | |
| 1650-01-213-2219 1650012132219 | 123SCEC100-620 26S-7D5074-18 | Boot, Deicer | III End Item Identification: Aircraft model C-2A Special Features: Height: 0.300IN Overall Length: 98.000 inches nominal | Goodrich Corporation (0AJJ0) Northrop Grumman Systems Corporation (26512, 61174) | |
| 1650-01-213-2220 1650012132220 | 123SCEC100-625 26S-7D5074-20 | Boot, Deicer | III End Item Identification: Aircraft model C-2A Special Features: Height: 0.030IN Overall Length: 98.000 inches nominal | Bfgoodrich Co., The (03481) Northrop Grumman Systems Corporation (26512) Goodrich Corporation (0AJJ0) | |
| 1650-01-213-2221 1650012132221 | 123SCEC100-623 26S-7D5074-21 123CEC100-623 | Boot, Deicer | III End Item Identification: Aircraft model C-2A Special Features: Height: 0.030IN Overall Length: 98.000 inches nominal | Bfgoodrich Co., The (03481) Goodrich Corporation (0AJJ0) Northrop Grumman Systems Corporation (26512, 61174) | |
| 1650-01-213-2222 1650012132222 | 123SCEC100-624 26S-7D5074-22 | Boot, Deicer | III End Item Identification: Aircraft model C-2A Special Features: Height: 0.300 Overall Length: 98.000 inches nominal | Goodrich Corporation (0AJJ0) Northrop Grumman Systems Corporation (26512) Bfgoodrich Co., The (03481) | |
| 1650-01-213-2252 1650012132252 | 74A410804-1009 | Rod, Piston, Linear Actuating Cyli | Boeing Company, The (76301) | ||
| 1650-01-213-2253 1650012132253 | 74A450704-1009 | Rod, Piston, Linear Actuating Cyli | Boeing Company, The (76301) Blair Industries Inc. (2U518) | ||
| 1650-01-213-2262 1650012132262 | 41003207 | Cylinder, Actuating, Linear | Woodward HRT Inc. (81873) | ||
| 1650-01-213-2263 1650012132263 | 123H40100-601 | Cylinder Assembly, Actuating, line | Northrop Grumman Systems Corporation (26512) |