Aircraft Hydraulic, Vacuum and De-icing System Components: 81402, 81549, 815585-2
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
81402 | 1650-00-781-9602 | Tappet, Cylinder | GST Industries Inc. (55822) Lockheed Martin Corporation (81755) | ||
81405 | 1650-00-116-1319 | Valve, Linear, Directional Control | III End Item Identification: Aircraft model A-4 Special Features: Cognizant service:navy Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. | Eaton Aerospace LLC (09790) | |
81408-2 814082 | 1650-00-184-5154 | Cylinder, Actuating, Linear | III Fsc Application Data: Aircraft hydraulic system (Non-Core Data) First Piston rod End Lubrication Facility: Not included (Non-Core Data) second Piston rod End Lubrication Facility: Not included | Boeing Company, The (76301) GST Industries Inc. (55822) | |
814248-1 8142481 | 1650-01-476-1913 | Cap, Linear Actuating Cylinder | Special Features: Note: type 1 cl 1, apply EC234974 Overall Length: 1.320 inches nominal End Item Identification: F-18 E/F | Hamilton Sundstrand Corporation (73030) | |
81435 | 1650-00-782-9955 | Adapter, Switch Actu | Boeing Company, The (76301) GST Industries Inc. (55822) | ||
81436 | 1650-00-782-9956 | Actuator Switch, cyl | Boeing Company, The (76301) GST Industries Inc. (55822) | ||
81437 | 1650-00-782-9947 | Piston, Linear Actuating Cylinder | III End Item Identification: 1650-00-052-9344 81375-6 cylinder assy Special Features: Unthreaded; fsc application data:cylinder assy, linear actuating, acft hyd | GST Industries Inc. (55822) | |
81438 | 1650-00-782-9948 | Lock Finger, Piston | GST Industries Inc. (55822) | ||
8148 | 1650-00-594-3500 | Disk, Valve | Material: Steel comp 440C Overall Height: 0.082 inches nominal Outside Diameter: 0.218 inches nominal | E-Systems Inc. (79294) Moog Inc. (19156,94697) | |
8-1-500 81500 | 1650-00-855-8441 | Filter Element, Fluid | III Fsc Application Data: Hydraulic system, aircraft Material: Steel corrosion resisting filtering medium Design Type: Reusable | Western Filter A Division Of (13520) | |
8150-1 81501 | 1650-00-129-9113 | Bushing, Cylinder as | III End Item Identification: C-141 aircraft | Goodrich Aerospace Canada LTD (02121) | |
8151-1 81511 | 1650-00-129-9133 | Sleeve | III End Item Identification: C-141 aircraft | Goodrich Aerospace Canada LTD (02121) | |
8153-1 81531 | 1650-00-129-9135 | Sleeve | Goodrich Aerospace Canada LTD (02121) | ||
81542 | 1650-00-923-1075 | Head, Tank | Hydro-Aire Inc. (81982) | ||
81547 | 1650-00-922-8773 | Piston, Tank | Hydro-Aire Inc. (81982) | ||
81549 | 1650-01-005-6284 | Body, Tank, Hydraulic Fluid | III End Item Identification: 1650008049192 General Characteristics Item Description: Must mate with plate P/N 81550 and end P/N 83511 P/O tank P/N 71141-11 | Hydro-Aire Inc. (81982) | |
81550 | 1650-00-923-1076 | Cover, Tank | General Characteristics Item Description: Al alloy 6061-T6;ANODIZE per MIL-A-8625 type I;6.483 IN.OD;0.740 IN.THK;2 ports 0.690 in.dia, located 5.000 in.ctr to ctr | Hydro-Aire Inc. (81982) | |
815583-1 8155831 | 1650-00-730-2228 | Ring and Spacer Ass | Lockheed Martin Corporation (98897) | ||
815585-1 8155851 | 1650-01-504-3684 | Actuator, Electro-Pneumatic | End Item Identification: Variable pitch aircraft propeller Part Name Assigned BY Controlling Agency: Actuator assembly, change code 28 Special Features: Data from component maint manual and ipl 61-13-12;PAGE 1037 fig 5 item 1C supersedes the -1, -2, -3 (1, 1A, 1B);PAGE 1036 ipl figure 5 variable pitch actuator assembly;page 1015 of fig 1 item 330C supersedes the -3 (330A, 330B);CHANGE code 28;PAGE 1012 ipl figure 1 variable pitch aircraft propeller;manual dated jan 07 | Hamilton Sundstrand Corporation (73030) | |
815585-2 8155852 | 1650-01-504-3684 | Actuator, Electro-Pneumatic | End Item Identification: Variable pitch aircraft propeller Part Name Assigned BY Controlling Agency: Actuator assembly, change code 28 Special Features: Data from component maint manual and ipl 61-13-12;PAGE 1037 fig 5 item 1C supersedes the -1, -2, -3 (1, 1A, 1B);PAGE 1036 ipl figure 5 variable pitch actuator assembly;page 1015 of fig 1 item 330C supersedes the -3 (330A, 330B);CHANGE code 28;PAGE 1012 ipl figure 1 variable pitch aircraft propeller;manual dated jan 07 | Hamilton Sundstrand Corporation (73030) |