FSC 1650 Aircraft Hydraulic, Vacuum and De-icing System Components: 1650-01-253-3563, 1650-01-253-9930, 1650-01-254-0101
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1650-01-253-3563 1650012533563 | TA30500096 A15HS080 A15HS080-1 | Tube Support Assembly | Kirkhill-TA Co. (84971) The Boeing Company (77272) | ||
| 1650-01-253-4055 1650012534055 | 2810036-101 | Valve, Fluid Pressure Regulating, | Parker Hannifin Corporation (92003) | ||
| 1650-01-253-5019 1650012535019 | 404036-2 404036-002 | Cylinder Assembly, Actuating, line | Raytheon Training Inc. (29778) | ||
| 1650-01-253-5289 1650012535289 | 1211162-004 | Cylinder Assembly, Actuating, line | III End Item Identification: A-10A aircraft III Fsc Application Data: Aircraft hydraulic system Design Characteristics: Single acting single cylinder | Arkwin Industries Inc. (98391) | |
| 1650-01-253-5320 1650012535320 | 351R250 | Disk, Valve | Material: Steel corrosion resisting Overall Height: 1.345 inches nominal Style Designator: 41 poppet | Aerocontrolex Group Inc. (98939) | |
| 1650-01-253-5767 1650012535767 | 51260-11 | Housing, Mechanical Drive | Eaton Corporation (99643) | ||
| 1650-01-253-5836 1650012535836 | 3187000-7 A51H9000-17 3187000-17 A51H9000-7 | Servocylinder | Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. | Allied-Signal Inc. (77068) Honeywell International Inc. (59364) Moog Inc. (0ZWK8) | |
| 1650-01-253-5837 1650012535837 | 3187000-18 A51H9000-18 3187000-8 A51H9000-8 | Servocylinder | Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. | Allied-Signal Inc. (77068) Honeywell International Inc. (59364) Moog Inc. (0ZWK8) | |
| 1650-01-253-6715 1650012536715 | 74A451004-1005 | Swivel Joint, Hydraulic, Aircraft | Special Features: Consist of 1 shaft 2.75 in. X 3.40 in. X 4.50 in. P/N 74A451004-2005, 1 ring P/N MS28775-010, 2 plug P/N ST7M141D7L, 1 adapter P/N ST7M200T4 | Boeing Company, The (76301) | |
| 1650-01-253-6718 1650012536718 | 960329-3 B1474-60 | Ring, Piston | III End Item Identification: 1680-01-055-9509 Features Provided: Wearing edges beveled Ring Style: 1 concentric | Kaydon Ring & Seal Inc. (75370) Parker-Hannifin Corporation (93835) | |
| 1650-01-253-7427 1650012537427 | 128HM10429 128HM10429-1 | Cylinder, Actuating, Linear | Special Features: W/ 4 pin plugs Overall Length: 17.124 inches minimum and 17.287 inches maximum Bore Diameter: 2.121 inches nominal | Wiebel Aerospace /1995/ Inc. (62064) Northrop Grumman Systems Corporation (26512) Triumph Actuation Systems LLC (26437) | |
| 1650-01-253-7848 1650012537848 | L5873400-061 | Servocylinder Assembly, Hydraulic | III End Item Identification: B-1B aircraft III Fsc Application Data: Aircraft hydraulic, vacuum, deicisystems Nuclear Hardness Critical Feature: Hardened | Boeing Company, The (43999) | |
| 1650-01-253-9930 1650012539930 | 63D715796P4 | Clamp, Yoke | General Characteristics Item Description: Material al aly 6061-T6 per QQ-A-250/11 0.12 in. thick, aperature dia. is 4.10 in., width is 4.88 in., length is 4.88 in., 4 mounting holes 0.234 in. dia, finish chemical film per MIL-C-5541, class 3 | Lockheed Martin Corporation (16331) | |
| 1650-01-254-0014 1650012540014 | MF30-3913-30ZE2 | Motor, Hydraulic | III Fsc Application Data: Hydraulic system acft Mounting Type: Flange Mounting Hole Quantity: 4 | Eaton Aerospace LLC (62983) | |
| 1650-01-254-0044 1650012540044 | 737225GC | Piston, Hydraulic Motor-Pump | III End Item Identification: F-16 aircraft III Fsc Application Data: Aircraft hydraulic, vacuum, deicing systems | Hamilton Sundstrand Corporation (99167) | |
| 1650-01-254-0045 1650012540045 | 737225GA | Piston, Hydraulic Motor-Pump | III End Item Identification: F-16 aircraft III Fsc Application Data: Aircraft hydraulic, vacuum, deicing systems | Hamilton Sundstrand Corporation (99167) | |
| 1650-01-254-0046 1650012540046 | 737225GH | Piston, Hydraulic Motor-Pump | III End Item Identification: F-16 aircraft III Fsc Application Data: Aircraft hydraulic, vacumm, deicing systems | Hamilton Sundstrand Corporation (99167) | |
| 1650-01-254-0047 1650012540047 | 737225GD | Piston, Hydraulic Motor-Pump | III End Item Identification: F-16 aircraft III Fsc Application Data: Aircraft hydraulic, vacuum, deicing systems | Hamilton Sundstrand Corporation (99167) | |
| 1650-01-254-0100 1650012540100 | 412-061-611-101 | Boot, Dust and Moisture Seal | Bell Helicopter Textron Inc. (97499) | ||
| 1650-01-254-0101 1650012540101 | 412-061-612-101 | Boot, Dust and Moisture Seal | Bell Helicopter Textron Inc. (97499) |