FSC 1650 Aircraft Hydraulic, Vacuum and De-icing System Components: 1650-01-125-7353, 1650-01-125-7656, 1650-01-126-7067
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1650-01-125-7353 1650011257353 | 3370051-1 | Sleeve and Slide, Directional Con | Parker-Hannifin Corporation (93835) | ||
| 1650-01-125-7360 1650011257360 | 3003128-5 | Cylinder, Actuating, Linear | Parker-Hannifin Corporation (93835) | ||
| 1650-01-125-7361 1650011257361 | 287800-1001 | Servocylinder | III End Item Identification: Aircraft model F-18 | Parker-Hannifin Corporation (82106) | |
| 1650-01-125-7362 1650011257362 | 34001890-107 | Servocylinder | Design Characteristics: Double acting single cylinder Extended Length: 18.460 inches nominal Compressed Length: 14.080 inches nominal | Woodward HRT Inc. (81873) | |
| 1650-01-125-7512 1650011257512 | 65391-11780-041 | Filter, Fluid | Drop Pressure: Not rated Differential Pressure: Not rated Maximum Operating Pressure: Not rated | Sikorsky Aircraft Corporation (78286) | |
| 1650-01-125-7655 1650011257655 | 4100206-1 | Cam Assembly | III End Item Identification: Aircraft model F-18 | Honeywell International Inc. (06848) | |
| 1650-01-125-7656 1650011257656 | 4100213-1 C61678-001 | Plate, Port | III End Item Identification: Aircraft model F-18 | Honeywell International Inc. (06848) Moog Inc. (94697) Triumph Actuation Systems LLC (26437, 1SR57) | |
| 1650-01-125-7657 1650011257657 | 4100214-1 C61737-001 | Piston, Balance | III End Item Identification: Aircraft model F-18 | Honeywell International Inc. (06848) Moog Inc. (94697) Triumph Actuation Systems LLC (1SR57, 26437) | |
| 1650-01-125-7743 1650011257743 | 74A411582-2001 | Adapter, Swivel, Hydraulic Mlg | III End Item Identification: Aircraft model F-18 General Characteristics Item Description: 7075 al alloy per mms 159, cond T-7351; 0.590 in. nom h; 0.500 in. nom w; 2.630 in. O/a lg | Pioneer Machine Products Inc. (12829) Boeing Company, The (76301) | |
| 1650-01-125-7751 1650011257751 | 74A690240-1001 | Swing Joint, Hydraulic Brake Mlg | III End Item Identification: Aircraft model F-18 | Boeing Company, The (76301) | |
| 1650-01-125-7841 1650011257841 | 3191010 | Arm, Pivot | III End Item Identification: Aircraft model F-14A | Allied-Signal Inc. (77068) Moog Inc. (0ZWK8) | |
| 1650-01-125-8861 1650011258861 | 2022100-3-2 | Drive unit, Hydraulic | III End Item Identification: Aircraft model F-18 Criticality Code Justification: AGAV | Honeywell International Inc. (70210) Moog Inc. (0ZWK8) | |
| 1650-01-125-8902 1650011258902 | 2040676-4 4100184-3 | Motor, Hydraulic | Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. Mounting Type: PAD Mounting Hole Quantity: 4 | Honeywell International Inc. (06848, 70210) Moog Inc. (0ZWK8) | |
| 1650-01-125-9176 1650011259176 | 123SCEC100-530 25S-7D5074-16 52 SP 199-8 | Boot, Deicer | III End Item Identification: Aircraft model E-2C | Bfgoodrich Co., The (03481) Goodrich Corporation (0AJJ0) Aerazur (F6101) | |
| 1650-01-125-9396 1650011259396 | 361-10299-1 | Cylinder Sleeve | III End Item Identification: B-52 | The Boeing Company (82918) | |
| 1650-01-125-9397 1650011259397 | 818702-1 361-26106-6 | Dampener, Flutter | III End Item Identification: B-52 | The Boeing Company (82918) Pacific Scientific Energetic (06331) | |
| 1650-01-125-9398 1650011259398 | 361-10299-2 | Cylinder Sleeve | III End Item Identification: B-52 | The Boeing Company (82918) | |
| 1650-01-125-9445 1650011259445 | P5119T3-2-2 | Rub Strip, Damper Assembly | III End Item Identification: Aircraft F-111 General Characteristics Item Description: Plastic TEFLON;6.270 in. LG;2.220 in. W III Fsc Application Data: Damper assembly, hydraulic | Coorstek, Inc. (07128) | |
| 1650-01-126-5561 1650011265561 | 2751661-2 | Barrel, Reservoir | Parker Hannifin Corporation (92003) Parker-Hannifin Corporation (82106, 59211, 9383) | ||
| 1650-01-126-7067 1650011267067 | 3321050 | Housing, Input Stroke Control | III End Item Identification: 1650-01-081-5420, F/FB111 acft General Characteristics Item Description: Anodize per MIL-A-8625, type 2, class 1;O/A dim 2.400 in. nom. lg;first end 4 mounting holes 0.337 in. min. and 0.347 in. max. dia thru;second end 4 mounting holes 0.215 in. min. and 0.223 in. max. dia thru, csk 85.0 deg. to 95.0 deg. X 0.270 in. min. and 0.300 in. max. dia, 0.2500-28UNJF-3B thds. thru | Allied-Signal Inc. (77068) Honeywell International Inc. (59364) |