FSC 1650 Aircraft Hydraulic, Vacuum and De-icing System Components: 1650-01-240-4731, 1650-01-241-3161, 1650-01-241-8143
NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
1650-01-240-4731 1650012404731 | 4A037-18 | Fitting, Hydraulic | III End Item Identification: C5B aircraft III Fsc Application Data: Aircraft hydraulic system | Arkwin Industries Inc. (98391) | |
1650-01-240-6623 1650012406623 | 0711354-101 | Spool, Sleeve Assembly | Arkwin Industries Inc. (98391) | ||
1650-01-240-6624 1650012406624 | 0711354-202 | Retainer, Hydraulic | Arkwin Industries Inc. (98391) | ||
1650-01-240-9021 1650012409021 | 2006811-105 2006811-105R | Cylinder Assembly, Actuating, line | III End Item Identification: F-16 aircraft; T.O.4AA1-8-4; main landing gear downlock Special Features: MLG | Goodrich Corp. (17576) | |
1650-01-240-9262 1650012409262 | AE84722G | Swivel Joint, Hydraulic, Aircraft | End Item Identification: F-18 aircraft | Eaton Corporation (00624) | |
1650-01-241-0341 1650012410341 | 66-19187-2 66-19187-1 | Adapter, Safety Valve | The Boeing Company (81205) | ||
1650-01-241-2336 1650012412336 | 1159CM20621-3 | Yoke Assy, Flap Driv | Gulfstream Aerospace Corporation (59734) | ||
1650-01-241-2337 1650012412337 | 1159CM20621-1 | Yoke Assy, Flap Driv | Gulfstream Aerospace Corporation (59734) | ||
1650-01-241-3130 1650012413130 | 28-40057-7 | Piston, Hydraulic Accumulator | III End Item Identification: C-5B aircraft General Characteristics Item Description: Dimensions in inches, 4.338 outside diameter, 1.320 thick;piston has 2-GROOVES 1-0.424 wide 2-0.120 wide, also hole stepped thru center 0.531 smallest diameter, 0.800 largest diameter;material aluminum 2024-T351 per QQ-A-22516;HEAT treat per nad ps 15535 after machining;anodize per nad ps 13201TYPE ii class I MIL-A-8625;USED on hydraulic accumulator 28-6005 III Fsc Application Data: Aircraft hydraulic vacuum deicing systems | York Industries Inc. (81616) Tactair Fluid Controls Inc. (70236) | |
1650-01-241-3131 1650012413131 | 2840088008 28-40088-7 | Rod, Piston, Hydraulic Accumulator | III End Item Identification: C-5B aircraft General Characteristics Item Description: Consist of rod piston 1, piston assembly 1, O-ring 3, cup, fluid 1, nut, self locking 1, ring back-up 2;NHA 2860005 accumulator 1650012177890 III Fsc Application Data: Aircraft hydraulic, vacuum, deicing systems | York Industries Inc. (81616) Tactair Fluid Controls Inc. (70236) | |
1650-01-241-3161 1650012413161 | 68A692511-1001 68A692511-1007 | Cylinder Assembly, Actuating, line | III End Item Identification: F15 aircraft III Fsc Application Data: Aircraft hydraulic system Design Characteristics: Single acting single cylinder | Boeing Company, The (76301) | |
1650-01-241-3224 1650012413224 | 28-40062-8 | Accumulator, Hydraulic | III End Item Identification: 1650012177898 III Fsc Application Data: Aircraft hydraulic system Overall Length: 36.725 inches nominal | York Industries Inc. (81616) Tactair Fluid Controls Inc. (70236) | |
1650-01-241-3633 1650012413633 | 65651-11059 65651-11059-101 | Retainer Block | General Characteristics Item Description: Aluminum alloy QQ-A-250-4;3 holes 1.000 in. dia;first end 0.156 in. thk;second end 0.312 in. thk | Sikorsky Aircraft Corporation (78286) | |
1650-01-241-6025 1650012416025 | 123P10387-507 123P10387-509 | Beam Assembly, Power | III End Item Identification: Aircraft model C-2, E-2 | Northrop Grumman Systems Corporation (26512, 61174) | |
1650-01-241-6582 1650012416582 | MS28776M2-67 MS28776 | Ring, Wiper | Material: Copper alloy overall Material Document and Classification: MIL-S-6049A mil spec single material response overall Inside Diameter: 11.000 inches nominal | Military Standards (96906) | |
1650-01-241-7733 1650012417733 | 3307561-1 | Boot, Aircraft Components | III End Item Identification: C-130 aircraft; ski equiped Material: Cotton | Lockheed Martin Corporation (98897) | |
1650-01-241-7947 1650012417947 | 28-40085-7 | Stop, Piston | York Industries Inc. (81616) Tactair Fluid Controls Inc. (70236) | ||
1650-01-241-8061 1650012418061 | 68A452800-1001 | Cylinder Assembly, Actuating, line | III End Item Identification: F-15E aircraft III Fsc Application Data: Aircraft hydraulic system Design Characteristics: Single acting single cylinder | Boeing Company, The (76301) | |
1650-01-241-8062 1650012418062 | 68A692516-1001 68A962516-1007 68A692516-1003 68A962516-1005 | Cylinder Assembly, Actuating, line | III End Item Identification: F15 aircraft Design Characteristics: Single acting single cylinder Pressure Rating: 3000.0 pounds per square inch nominal | Boeing Company, The (76301) | |
1650-01-241-8143 1650012418143 | 42093R187 | Accumulator, Pneumatic | III End Item Identification: C5B aircraft III Fsc Application Data: Aircraft pneumatic system Shape: Cylindrical | Triumph Gear Systems Inc. (82402) |