Aircraft and Missile Prime Movers Engine Fuel System Components: RG9570M, RR11620-2, RR11810B1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| RG9570M | 2915-01-424-6875 | Pump, Fuel | Lucas Aerospace Power Equipment (31435) | ||
| RG9570R1/M RG9570R1M | 2915-01-580-8679 | Engine Driven Pump | Crane Co. (51663) | ||
| RK440D1 | 2915-00-986-1572 | Parts kit | Honeywell International Inc. (94580) | ||
| RM1088A22 | 2915-01-538-9645 | Mount, Engine Rubbe | Federal Prison Industries Inc. (57865) | ||
| RP693882 | 2915-01-434-2802 | Plunger, Fuel Injector | III End Item Identification: Preprovisioning support navicp is poe | Saab AB Pupl - Electronic Defence (S3514) Saab Aktiebolag (SG836) | |
| RPK2883 | 2915-00-575-8618 | Parts kit, Pump, Depot | III End Item Identification: 29158422574 | Hawker Pacific Aerospace (99473) | |
| RPK2883-1 RPK28831 | 2915-00-575-8618 | Parts kit, Pump, Depot | III End Item Identification: 29158422574 | Hawker Pacific Aerospace (99473) Parker-Hannifin Corporation (26433) | |
| RR11050F | 2915-00-203-6554 | Pump, Submerged, Aircraft | General Characteristics Item Description: Designed for partially submerged operation, non-positive displacement, 27 vdc 20 amp 8000 rpm, 6000 phr at 15 psi rated output W/JP4 fuel, 10.000 in. lg parallel to shaft axis, 7.875 in. dia O/a, 16 holes 0.281 in. dia equally spaced around a 7.875 in. dia mtg flange, 1-1/2 in. mtg facility for internal or external discharge connections, 2 stud terminal block for electrical connection | Crane Co. (51663) | |
| RR11620-1 RR116201 | 2915-00-983-1001 | Pump, Submerged, Aircraft | Reference Number Differentiating Characteristics: Lockheed and georgia co source control dwg no. 695768-1 | Crane Co. (51663) | |
| RR11620-2 RR116202 | 2915-00-983-1001 | Pump, Submerged, Aircraft | Reference Number Differentiating Characteristics: Lockheed and georgia co source control dwg no. 695768-1 | Crane Co. (51663) | |
| RR11620-3 RR116203 | 2915-00-983-1001 | Pump, Submerged, Aircraft | Reference Number Differentiating Characteristics: Lockheed and georgia co source control dwg no. 695768-1 | Crane Co. (51663) | |
| RR11640 | 2915-01-506-2353 | Pump, Submerged, Aircraft | Crane Co. (51663) | ||
| RR11640-1 RR116401 | 2915-01-506-2354 | Pump, Submerged, Aircraft | III End Item Identification: C130 aircraft Special Features: Fuel boost, bladder cell and dump, electric motor driven | Crane Co. (51663) | |
| RR11640A1 | 2915-01-196-4362 | Pump, Submerged, Aircraft | III End Item Identification: C130 acft fuel system General Characteristics Item Description: Centrifugal boost pump for JP-4 jet fuel per MIL-F-5624; capacity 27, 400 phr @ 12 psig, 6, 000 phr @ 28 psig; motor 1.1 hp @ 7200 rpm, 1100 watts max power input, 4.2 amps max current input, continuous duty cycle | Crane Co. (51663) | |
| RR11640A3 | 2915-00-083-9373 | Pump, Submerged, Aircraft | General Characteristics Item Description: Designed for partially submerged operation, non positive displacement, 200/115 vac, 400 cps, 3 phase, 40 psi at 0 phr flow to 12 psi at 27000 phr flow discharge pressure for JP4 fuel, W/thermal protection, 9.800 in. lg, 8.650 in. W, 4.500 in. H O/a dim., 4 holes 0.281 in. dia drilled in mtg ears on 4.700 in. by 3.145 in. ctrs, 4 wire lead electrical connection W/lug type terminals, external discharge port 1.480 in. id W/B4-PASS valve | Crane Co. (51663) | |
| RR11640D | 2915-01-505-9069 | Pump, Submerged, Aircraft | III Part Name Assigned By Controlling Agency: Pump, fuel boost, bladder cell and dump | Crane Co. (51663) | |
| RR11640D1 | 2915-01-196-4362 | Pump, Submerged, Aircraft | III End Item Identification: C130 acft fuel system General Characteristics Item Description: Centrifugal boost pump for JP-4 jet fuel per MIL-F-5624; capacity 27, 400 phr @ 12 psig, 6, 000 phr @ 28 psig; motor 1.1 hp @ 7200 rpm, 1100 watts max power input, 4.2 amps max current input, continuous duty cycle | Crane Co. (51663) | |
| RR11810A | 2915-00-814-4841 | Pump, Submerged, Aircraft | General Characteristics Item Description: Designed for partially submerged operation, non positive displacement, 1 impeller, 27V dc, 18 amps, 8000 rpm, 2000 phr at 21 psi rated capacity using JP4 fuel, 10.550 in. lg, 7.062 in. W, 4.906 in. H O/a dim., 12 mtg holes 0.281 in. dia evenly spaced around a 7.062 in. by 4.906 in. oval mtg flange, W/radio noise filter, 2 wire lead electrical connections processed W/lug type terminals, internal and external discharge bosses 1.500 in. id connection | Crane Co. (51663) GE Aviation Systems LLC (35351) | |
| RR11810B | 2915-00-717-6846 | Pump, Submerged, Aircraft | General Characteristics Item Description: Designed for partially submerged operation, non positive displacement, 1 impeller, 27V dc, 18.0 amps, 8000 rpm, 1450 phr at 27 psi, 2832 phr at 22 psi rated capacity, 8.968 in. lg, 7.062 in. W, 4.906 in. H O/a dim., 12 mtg holes 0.281 in. dia evenly spaced around a 7.062 in. by 4.906 in. mtg flange, W/radio noise filter, 2 thd terminal type electrical connection, 2 wire leads W/terminal lugs 36 in. lg incl., internal or external discharge bosses 1.500 in. id for adapter attachment | Crane Co. (51663) | |
| RR11810B1 | 2915-00-717-6846 | Pump, Submerged, Aircraft | General Characteristics Item Description: Designed for partially submerged operation, non positive displacement, 1 impeller, 27V dc, 18.0 amps, 8000 rpm, 1450 phr at 27 psi, 2832 phr at 22 psi rated capacity, 8.968 in. lg, 7.062 in. W, 4.906 in. H O/a dim., 12 mtg holes 0.281 in. dia evenly spaced around a 7.062 in. by 4.906 in. mtg flange, W/radio noise filter, 2 thd terminal type electrical connection, 2 wire leads W/terminal lugs 36 in. lg incl., internal or external discharge bosses 1.500 in. id for adapter attachment | Crane Co. (51663) |