FSC 1650 Aircraft Hydraulic, Vacuum and De-icing System Components: 1650-01-242-3375, 1650-01-242-4960, 1650-01-242-9823
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1650-01-242-3375 1650012423375 | 41005925-102 | Cylinder, Actuating, Linear | III End Item Identification: B-1B aircraft III Fsc Application Data: Aircraft hydraulic vacuum deicing systems Special Features: Consist of housing, piston directional valve 1, screen 1, orfice 1, silver solder a/r;grind orfice to 0.865 min.to 0.885 maximum;nha 41003320;USED on servovalve NR52003-3B | Woodward HRT Inc. (81873) | |
| 1650-01-242-4749 1650012424749 | M8815/4-10 MIL-F-8815/4A | Filter, Fluid | Design Type: Reusable Style Designator: C32 tee type Filtration Rating in Microns: 5.0 absolute | Military Specifications (81349) | |
| 1650-01-242-4960 1650012424960 | 713504 | Retainer, Slipper | Hamilton Sundstrand Corporation (99167) | ||
| 1650-01-242-5168 1650012425168 | 30100443 | Gland, Stop Hydraulic | III End Item Identification: B-1B aircraft General Characteristics Item Description: Dimensions in inches, 0.452 thick, 1.051 outside diameter, 0.875 relief diameter, 0.250 wide relief, 0.468 diameter bore 0.250 deep-one end only, 0.400 diameter by 0.075 high boss other end;material 304 cres per QQ-S-763 cond a;passivate per ess 001;NHA 41003320-101;USED on NR52003-03B servovalve III Fsc Application Data: Aircraft hydraulic vacuum deicing systems | Woodward HRT Inc. (81873) | |
| 1650-01-242-5169 1650012425169 | 41005926-102 | Gland, Hydraulic | III End Item Identification: B-1B aircraft General Characteristics Item Description: Consist of housing, gland directional valve, screen 1, orfice 1, silver solder a/r;final orfice size shall allow a flow of 160-190 cc/min with 1500 psid;used on NR52003-03B servovalve III Fsc Application Data: Aircraft hydraulic vacuum deicing systems | Woodward HRT Inc. (81873) | |
| 1650-01-242-5193 1650012425193 | S300100-002 S300100-2 | Piston, Linear Actuating Cylinder | Raytheon Training Inc. (29778) | ||
| 1650-01-242-5298 1650012425298 | 41005443-104 | Disk, Valve | Special Features: Consist of poppet valve 1, seat 2, spacer seat 1;FURNISH as matched set only;used on NR52003-03B servovalve End Item Identification: B-1B aircraft Fsc Application Data: Aircraft hydraulic vacuum deicing systems | Woodward HRT Inc. (81873) | |
| 1650-01-242-6491 1650012426491 | 68A412800-1005 68A412800-1001 68A412800-1003 | Cylinder Assembly, Actuating, line | III End Item Identification: F-15E aircraft Design Characteristics: Single acting single cylinder III Part Name Assigned By Controlling Agency: Cylinder assy | Goodrich Corporation (13002) Boeing Company, The (76301) | |
| 1650-01-242-7817 1650012427817 | 4100712-2 | Piston and cam Assembly | III End Item Identification: 1650011482152 General Characteristics Item Description: Consists of 1 4100137-1 retainer, BEARING;1 4100138-1 retainer, aux CAM;1930361 PISTON;1 929035 bearing, ball THRUST;1 930359 aux CAM;1 920359-1 shim;as REQUIRED;1 920359-2 shim, as REQUIRED;3 4100136-1 KEYS;1 930364 piston III Fsc Application Data: Aircraft hydraulic system | Triumph Actuation Systems LLC (1SR57) Honeywell International Inc. (06848) | |
| 1650-01-242-7864 1650012427864 | 800710 702640 | Bladder, Accumulator, Hydraulic | AR BEE Corp. (52993) Parker-Hannifin Corporation (26337) Wheeler Bros. Inc. (55683) | ||
| 1650-01-242-7951 1650012427951 | 7588210 | Head, Linear Actuating Cylinder | Special Features: Fsc application data:aircraft hydraulic system End Item Identification: C5B aircraft | PTI Technologies Inc. (05228) | |
| 1650-01-242-8299 1650012428299 | 593516-3 593576-3 | Parts kit, fan Overhaul | III End Item Identification: F-111 aircraft General Characteristics Item Description: Kit consist of; pin 2, packing 3; screw 12, nut 5, bearing 3, spring 2, seal 1, ring 1, retainer 1, sleeve 1, adapter 1, insert 1 | Honeywell International Inc. (70210) | |
| 1650-01-242-8920 1650012428920 | 7588234 | Case, Hydraulic | III End Item Identification: C5B aircraft III Fsc Application Data: Aircraft hydraulic system | PTI Technologies Inc. (05228) | |
| 1650-01-242-9577 1650012429577 | A15HS055-1 Q2013-01 | Valve, Regulating, Fluid Pressure | Body Material: Aluminum alloy and steel Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. Temp Rating: -50.0 deg celsius minimum and 160.0 deg celsius maximum | Aerocontrolex Group Inc. (98939) The Boeing Company (77272) | |
| 1650-01-242-9702 1650012429702 | AA-B211-8D2A | Filter Body, Fluid | Style Designator: C37 unthreaded shell Body Outside Diameter: 2.160 inches nominal Mounting Type: Threaded stud top | Pall Aeropower Corporation (18350) | |
| 1650-01-242-9703 1650012429703 | AC-3258-109Y2 A02HS123-3 | Filter Element, Fluid | Pall Aeropower Corporation (18350) The Boeing Company (77272) | ||
| 1650-01-242-9704 1650012429704 | A02HS161-3 AC-7665-12Y2 | Filter Element, Fluid | Design Type: Nonreusable Style Designator: A14 cylindrical W/integral outer casing Filtration Rating in Microns: 5.0 absolute | The Boeing Company (77272) Pall Aeropower Corporation (18350) | |
| 1650-01-242-9808 1650012429808 | 52894 | Piston | Parker-Hannifin Corporation (93835) | ||
| 1650-01-242-9809 1650012429809 | 281925 | Tube, Transfer | Valcor Engineering Corp. (96487) | ||
| 1650-01-242-9823 1650012429823 | 135065 | Housing | Eaton Aerospace LLC (62983) |