FSC 1650 Aircraft Hydraulic, Vacuum and De-icing System Components: 1650-00-113-2130, 1650-00-113-6920, 1650-00-114-0067
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1650-00-113-2130 1650001132130 | 4G13761-101A | Cap, Linear Actuating Cylinder | Special Features: 4 mtg holes evenly spaced;fsc application data:landing gear, retractable End Item Identification: Aircraft C5A Outside Diameter: 8.483 inches minimum and 8.488 inches maximum | Lockheed Martin Corporation (98897) | |
| 1650-00-113-2890 1650001132890 | 402756-1 | Seat, Helical Compression Spring | Material Hardness Rating: Not rated | Lucas Western Inc. (09348) BCP Construction Products (88853) | |
| 1650-00-113-6015 1650001136015 | 30610-50 30610-5 | No Item Name Available | E-Systems Inc. (79294) Moog Inc. (19156, 94697) | ||
| 1650-00-113-6354 1650001136354 | SGT520-6 204-010-937-7 2020H-7 204-010-937-007 | Dampener, Flutter | III End Item Identification: UH-1 series helicopters | Bell Helicopter Textron Inc. (97499) Parker Hannifin Corporation (92003) Logistical Support LLC (55064) | |
| 1650-00-113-6888 1650001136888 | 475J722 | Ball, Swivel Joint | III End Item Identification: 16500848670 General Characteristics Item Description: 1.310 in. dia | Grimes Aerospace Co. (00672) | |
| 1650-00-113-6910 1650001136910 | 706792-1 | Spacer, Air Control | General Characteristics Item Description: Aluminum alloy, anodized | Hamilton Sundstrand Corporation (73030) | |
| 1650-00-113-6911 1650001136911 | 417-1GE | Cap, Tank | General Characteristics Item Description: 1.920 in. dia | Parker-Hannifin Corporation (99321) | |
| 1650-00-113-6912 1650001136912 | 5-75001-1 | Bellows, Reservoir | III End Item Identification: 16507231166 III Fsc Application Data: Acft hydraulic system | Moore Rubber Co. Inc. (0SV43) Northrop Grumman Technical Services (0JRC1) Northrop Grumman Systems Corporation (76823) | |
| 1650-00-113-6913 1650001136913 | 3-43932 5-75001-5 5-75002 | Weight, Bellows, Reservoir | General Characteristics Item Description: Steel AMS5358, 1.370 in. od, 1.80 in. lg, oval shaped | Golden State Rubber and Latex Corp. (09088) Northrop Grumman Technical Services (0JRC1) Northrop Grumman Systems Corporation (76823) | |
| 1650-00-113-6920 1650001136920 | 22-1163-179 2-1163179 2-1163-179 | Retainer, Cylinder | General Characteristics Item Description: Teflon tubing per ams 3651, 0.727 in. od, 0.557 in. id, 0.050 in. thk | Boeing Company, The (76301) Parker-Hannifin Corporation (3H889) Parker Hannifin Corporation (92003) | |
| 1650-00-113-6926 1650001136926 | 1767L003-1 | Piston, Linear Actuating Cylinder | Special Features: Steel AMS5643, 23.420 in. lg, 5-18&16UNS&3A threads one end, 4.998 to 5.000 in. body od | Goodrich Corp. (17576) | |
| 1650-00-113-6927 1650001136927 | 1767L004-1 | Piston, Linear Actuating Cylinder | Special Features: 2.530 in. body OD;2.170 in. jamor body ID;2 16UNEF 3B thd, 0.480 in. to 0.490 in. seal groove width, 0.184 in. seal groove depth Material: Steel Overall Length: 24.990 inches nominal | Goodrich Corp. (17576) | |
| 1650-00-113-6928 1650001136928 | 5C300-005 | Cooler, Hydraulic Oil, Aircraft | Special Features: Aluminum alloy QQ-A-250, 24.00 in.lg, 23.00 in. W, 11.54 in.H, purpose cool hyd fluid, cooling agent ram air-bleed air-fuel, utility power system lh side, replaced by P/N 5C300-007 | Standard-Thomson Corporation (78493) | |
| 1650-00-113-6930 1650001136930 | 5C300-006 | Cooler, Hydraulic Oil, Aircraft | Special Features: Aluminum alloy QQ-A-250, 24.00 in. lg, 23.00 in. W, 11.45 in. H, purpose cool hydraulic fluid, cooling agent ram air-bleed air-fuel, primary power system rh side, replaced by P/N 5C300-006 | Standard-Thomson Corporation (78493) | |
| 1650-00-113-7673 1650001137673 | 3187000-11 A51H9000-11 | Servocylinder | III Fsc Application Data: Hydraulic systems, aircraft Special Features: Left hand installation Design Characteristics: Double acting single cylinder | Allied-Signal Inc. (77068) Moog Inc. (0ZWK8) Northrop Grumman Systems Corporation (26512, 61174) | |
| 1650-00-113-7674 1650001137674 | A51H9000-12 3187000-12 | Servocylinder | III Fsc Application Data: Hydraulic systems, aircraft Special Features: Right hand installation Design Characteristics: Double acting single cylinder | Allied-Signal Inc. (77068) Moog Inc. (0ZWK8) Northrop Grumman Systems Corporation (61174, 26512) | |
| 1650-00-113-7731 1650001137731 | A51H9012-13 PPEV3-011-11 | Power Module, Hydrau | General Characteristics Item Description: Control circuits 28 volts dc, pressure switch setting 1950PSI min, 3050 psi max, thermal switch setting 260 deg F min, 290DEG F max, motor circuit 115 volt ac 400 cycle 3 phase Reference Number Differentiating Characteristics: As differentiated by source control dwg no. | Eaton Aerospace LLC (62983) Northrop Grumman Systems Corporation (26512, 61174) | |
| 1650-00-113-9384 1650001139384 | 53-140050-5 | Shaft Pin Pull | Boeing Company, The (76301) | ||
| 1650-00-114-0048 1650001140048 | HP558106 | Push rod | Teledyne Hydra-Power (84685) Tactair Fluid Controls Inc. (70236) | ||
| 1650-00-114-0067 1650001140067 | C10344 4870344 | Parts kit, Valve | Marotta Controls Inc. (99657) |