Ontic Engineering & Manufacturing NSN Parts: 123226-100-04 - 701294-1
FSC 2915 Engine Fuel System Components, Aircraft and Missile Prime Movers
| MFG SKU | NSN | Item Name | Details | CAGE Code | RFQ |
|---|---|---|---|---|---|
| 123226-100-04 12322610004 | 2915-00-691-1385 | Pump, Submerged, Aircraft | General Characteristics Item Description: Designed for partially submerged operation, non positive displacement, 1 impeller, 200V, 400 cps, 3 ph, 1.7 amps, 5000 phr at 5 psi W/JP4 fuel, 8.400 in. lg, 5.380 in. W, 3.630 in. H O/a dim., 4 mtg holes 0.264 in. dia drilled thru sq flange on 2.500 in. ctrs, 4 wire electrical lead processed W/4 terminal lugs, external 90 deg 1.000 in. id discharge hose connection | 45934 | |
| 123226-100-05 12322610005 | 2915-00-691-1385 | Pump, Submerged, Aircraft | General Characteristics Item Description: Designed for partially submerged operation, non positive displacement, 1 impeller, 200V, 400 cps, 3 ph, 1.7 amps, 5000 phr at 5 psi W/JP4 fuel, 8.400 in. lg, 5.380 in. W, 3.630 in. H O/a dim., 4 mtg holes 0.264 in. dia drilled thru sq flange on 2.500 in. ctrs, 4 wire electrical lead processed W/4 terminal lugs, external 90 deg 1.000 in. id discharge hose connection | 45934 | |
| 123226-130-01 12322613001 | 2915-00-986-7884 | Pump, Submerged, Aircraft | General Characteristics Item Description: Designed for partially submerged operation, non positive displacement, 1 impeller, 200V ac, 400 cps, 3 ph, 5000 phr at 5 psi rated capacity, 8.400 in. lg, 5.130 in. W, 3.260 in. H O/a dim., 4 holes 0.265 in. dia equally spaced on sq mtg flange on 2.500 in. by 2.500 in. ctrs, 4 wire insulated lead electrical connection processed W/terminal lugs, W/3 thermal protectors, 1.000 in. id hose discharge connection | 45934 | |
| 123510-010-01 12351001001 | 2915-01-579-2811 | Pump, Submerged, Aircraft | 45934 | ||
| 123510-011-01 12351001101 | 2915-00-073-8891 | Pump, Submerged, Aircraft | General Characteristics Item Description: Designed for partially submerged operation, non positive displacement, 200/115 vac 400 cps 3 phase, 28 PS1 at 6000 pph, 12 PS1 at 27, 400 pph, rated discharge pressure and flow, 9.900 in. lg parallel to shaft axis, 8.515 in. lg, 4.782 in. W perpendicular to shaft axis, 4 holes 0.281 in. dia spaced on 4.705 in. by 3.150 in ctrs on mtg flange, external straight flange type discharge port | 45934 | |
| 123510-014-01 12351001401 | 2915-01-185-1847 | Pump, Submerged, Aircraft | III End Item Identification: C130E aircraft fuel system | 45934 | |
| 2PR400BRDE1 | 2915-00-203-8096 | Pump, Water, Alcohol | III End Item Identification: Aircraft engine model R2800-52W General Characteristics Item Description: Steel, 3.190 in. O/a lg, 2.880 in. O/a dia | 45934 | |
| 591653 | 2915-01-481-4915 | Push bar and Bellcrank | III End Item Identification: Turbo prop engines (T58) III Part Name Assigned By Controlling Agency: Push bar and bellcrank | 45934 | |
| 542439 | 2915-00-918-8899 | Push rod, Valve | 45934 | ||
| 502227 | 2915-00-723-7500 | Rack, Actuating | III End Item Identification: Fuel control 510000 General Characteristics Item Description: Cres AMS5610, rockwell hardness rating rc 30-46, 4.000 in. lg, 15 teeth | 45934 | |
| 539963 | 2915-01-208-7801 | Regulator, Bleed Pressure | 45934 | ||
| 701295-1 7012951 | 2915-00-944-8255 | Restrictor, Fuel Flow | III End Item Identification: Aircraft engine fuel system, P/N 597700-1 General Characteristics Item Description: Operational flow 33 to 41 pph at 80 to 90 deg F W/98 to 102 psig pressure drop, optional flow direction, O/a dim. 0.348 in. min to 0.367 in. max lg by 0.360 in. min to 0.370 in. max dia, internal thd size 0.112-40 UNC-2B, small end 0.051 in. min to 0.061 in. max dia | 45934 | |
| 02-12015 0212015 | 2915-00-798-8288 | Retainer | 45934 | ||
| 02-13464 0213464 | 2915-00-798-8290 | Retainer | 45934 | ||
| 02-505 02505 | 2915-00-696-6522 | Retainer | 45934 | ||
| 349-20A 34920A | 2915-00-118-6905 | Retainer | 45934 | ||
| 575561 | 2915-00-979-6368 | Retainer and Bearin | 45934 | ||
| 599337 | 2915-00-020-0288 | Retainer and Bearing Assembly | III End Item Identification: Engine model T64 | 45934 | |
| 579229 | 2915-00-074-2276 | Retainer and Pin Assembly | General Characteristics Item Description: Consists of P/N 579226 and P/N 69522-4C8 | 45934 | |
| 701294-1 7012941 | 2915-00-944-8263 | Retainer and Screen Restrictor, F | III End Item Identification: Aircraft engine fuel system, P/N 597700-1 General Characteristics Item Description: O/a dim. 0.465 in. min to 0.480 in. max dia by 0.397 in. min to 0.407 in. max lg, groove 0.095 in. min to 0.105 in. max W by 0.112 in. min to 0.127 in. max deep around middle, inside 0.218 in. min to 0.220 in. max dia by 0.035 in. min to 0.042 in. max deep, 0.321 in. min to 0.325 in. max dia by 0.095 in. min to 0.105 in. max deep, 0218 in. min to 0.220 in. max dia by 0.242 in. min to 0.252 in. max deep and mesh W/0.009 in. dia wire plain weave screen 0.353 in. min to 0.063 in. max dia by 0.025 in. min to 0.035 in. max deep | 45934 |
