Aircraft and Missile Prime Movers Engine Fuel System Components: 60-371, 60-371D, 6038T62P07
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 60-371 60371 | 2915-01-506-2355 | Pump, Submerged, Aircraft | Hydro-Aire Inc. (81982) | ||
| 60-37110 6037110 | 2915-00-404-3769 | Housing Assembly, Fuel | III End Item Identification: U/O fuel booster pump, fscm 81982, pn 60-371B, nsn 2915-00-971-9131 III Fsc Application Data: Engine fuel system components, aircraft | Hydro-Aire Inc. (81982) | |
| 60-37112 6037112 | 2915-00-915-2712 | Cap, Fuel Booster Pu | Hydro-Aire Inc. (81982) | ||
| 60-37114 6037114 | 2915-00-915-2713 | Inlet Adapter, Fuel | Hydro-Aire Inc. (81982) | ||
| 60-37118 6037118 | 2915-00-915-2715 | Cable Fitting, Fuel | Hydro-Aire Inc. (81982) | ||
| 60-37152 6037152 | 2915-00-916-6984 | Impeller, Pump, Centrifugal | III Part Name Assigned By Controlling Agency: Impeller-fuel booster pump Design Type: Double width Overall Diameter: 2.014 inches nominal | Hydro-Aire Inc. (81982) | |
| 60-37154 6037154 | 2915-00-891-3637 | Spacer, Fuel Pump | Hydro-Aire Inc. (81982) R. R. Templeton Corporation (34659) | ||
| 60-371B 60371B | 2915-00-971-9131 | Pump, Submerged, Aircraft | General Characteristics Item Description: Designed for partially submerged operation, non positive displacement, 1 impeller, 115/200V ac, 400 cps, 3 ph, 27400 phr at 12 psi rated capacity using JP4 fuel, 10.000 in. lg, 8.512 in. W, 4.000 in. H approx O/a dim., 4 holes 0.281 in. dia drilled thru 4 mtg feet on 3.145 in. by 4.700 in. ctrs, 4 wire insulated electrical lead processed W/4 terminal lugs, W/3 thermal protectors, W/bypass valve, internal discharge boss 1.500 in. id | Hydro-Aire Inc. (81982) | |
| 60-371B901A 60371B901A | 2915-00-939-9536 | Parts kit, Pump Overhaul, Fuel Con | III End Item Identification: Pump, P/N 60-371C, C13 support General Characteristics Item Description: Includes 24 parts, bearing assys, boots, cement bonding, disc, holder-bearings, insert-roson, leadwires, lock ring, packing, plugs, pin-drive, pin-coiled, retaining rings, screws, shim lams, sleeving, terminal assy and washer-thrust | Hydro-Aire Inc. (81982) | |
| 60-371C 60371C | 2915-00-971-9131 | Pump, Submerged, Aircraft | General Characteristics Item Description: Designed for partially submerged operation, non positive displacement, 1 impeller, 115/200V ac, 400 cps, 3 ph, 27400 phr at 12 psi rated capacity using JP4 fuel, 10.000 in. lg, 8.512 in. W, 4.000 in. H approx O/a dim., 4 holes 0.281 in. dia drilled thru 4 mtg feet on 3.145 in. by 4.700 in. ctrs, 4 wire insulated electrical lead processed W/4 terminal lugs, W/3 thermal protectors, W/bypass valve, internal discharge boss 1.500 in. id | Hydro-Aire Inc. (81982) | |
| 60-371D 60371D | 2915-01-160-8283 | Pump, Submerged, Aircraft | End Item Identification: Areospace support accessories Criticality Code Justification: AGAV General Characteristics Item Description: 2FOR submerged service; positive displacement; 115/230V ac, 400 hz, 3 phase; 10.000 in. lg; 8.512 in. dia; 4 wire lead W/4 terminal lugs facing 180 deg opposite discharge port; W/3 thermal protectors; W/bypass valve; discharge 1.500 in. I/D B0SS | Hydro-Aire Inc. (81982) | |
| 60372E | 2915-00-991-5987 | Fitting, Inlet | ITT Corporation (73760) | ||
| 60378-2 603782 | 2915-01-189-0276 | Pump Assembly, Submerged, Aircraft | General Characteristics Item Description: 4.060 in. lg; 0.650 in. dia holes 0.180 in. dp; 1 ea 27828; 204157; 27832; 27946; MS29513-033; 5 ea 28211; MS35218-27; MS29513-018; NAS620A6; 10 ea MS171431 | Argo-Tech Corporation Costa Mesa (86090) | |
| 6037T07P01 | 2915-01-023-4300 | Fuel Control, Main, Turbine Engine | III End Item Identification: Engine model TF34-GE-2 Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. | General Electric Company (99207) | |
| 6037T08P01 | 2915-01-021-8113 | Fuel Control, Main, Turbine Engine | General Characteristics Item Description: 12.855 in. max height Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. | General Electric Company (99207) | |
| 603813-2 6038132 | 2915-01-548-6456 | Pump, Fuel, cam Actuated | III End Item Identification: Ef 2000 fighter aircraft | Eaton Aerospace LLC (97484) | |
| 6038T62P01 | 2915-01-087-4376 | Fuel Control, Main, Turbine Engine | Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. | General Electric Company (99207) | |
| 6038T62P04 | 2915-01-105-5879 | Fuel Control, Main, Turbine Engine | General Characteristics Item Description: Used on UH-60A, utility helicopter | General Electric Company (99207) | |
| 6038T62P06 | 2915-01-120-7677 | Fuel Control, Main, Turbine Engine | General Electric Company (99207) | ||
| 6038T62P07 | 2915-01-122-8992 | Fuel Control, Main, Turbine Engine | III End Item Identification: UH-60 helicopter Specification/Standard Data: 99207-4046T52G06 manufacturers standard | General Electric Company (99207) |