Aircraft and Missile Prime Movers Engine Fuel System Components: 557584, 55-7600-2, 558441

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MFG SKUNSNItem NameDetailsManufacturer (CAGE)RFQ
557584 2915-00-596-2515Sleeve, Outer, ThrottHamilton Sundstrand Corporation (73030)

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557595 2915-00-918-9006Selector and InsertHamilton Sundstrand Corporation (73030)
Ontic Engineering & Manufacturing (45934)

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55-7600-1
5576001
2915-01-156-0876Valve, InterconnectEnd Item Identification: Acft model F-18
General Characteristics Item Description: Housing aluminum alloy per MIL-A-21180; 5.938 in. O/a lg; 5.073 in. O/a h; 2.651 in. O/a w; fluid gasoline per MIL-G-5572; 0.0 to 12.0 psig; M65.0 to P160.0 deg F temp rating
Sweeney Engineering Corp. (96736)

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55-7600-2
5576002
2915-01-156-0857Valve, InterconnectIII End Item Identification: Acft model F-18
General Characteristics Item Description: Housing aluminum alloy per MIL-A-21180; 5.938 in. O/a lg; 5.073 in. O/a h; 2.651 in. O/a w; fluid gasoline per MIL-G-5572; 0.0 to 12.0 psig; M65.0 to P160.0 deg F temp rating
Sweeney Engineering Corp. (96736)

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55-7600-3
5576003
2915-01-283-0244Valve, InterconnectEnd Item Identification: Aircraft model F-18
General Characteristics Item Description: 5.750 in. nom O/a lg; 2.803 in. nom O/a w; 4.000 in. nom O/a h; operating pressure 0.0 to 20.0 psi; proof 40.0 psi; burst 60.0 psi
Sweeney Engineering Corp. (96736)

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55-7600-4
5576004
2915-01-268-4169Valve Assembly, InterconnectEnd Item Identification: Aircraft model F-18
Sweeney Engineering Corp. (96736)

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55-7600-5
5576005
2915-01-156-0876Valve, InterconnectEnd Item Identification: Acft model F-18
General Characteristics Item Description: Housing aluminum alloy per MIL-A-21180; 5.938 in. O/a lg; 5.073 in. O/a h; 2.651 in. O/a w; fluid gasoline per MIL-G-5572; 0.0 to 12.0 psig; M65.0 to P160.0 deg F temp rating
Sweeney Engineering Corp. (96736)

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5577790-505
5577790505
2915-01-208-6435Drag cup, MachinedIII End Item Identification: Turbo prop engine model T56
Boeing Company, The (88277)

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558076 2915-00-728-2296Fuel Control, Main, Turbine EngineIII End Item Identification: Engine, jet, J47
United Technologies Corporation (77445)

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558143 2915-00-925-0371Heater, FuelUnited Technologies Corporation (77445)

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558231 2915-00-948-7212Lock, Fuel Nozzle SupportIII End Item Identification: J52 acft engine fuel system, P/N 538038
General Characteristics Item Description: Ams 5645 stainless steel, 0.580 in. min to 0.640 in. max O/a lg, 0.420 to 0.440 in. lg top, concave bottom, groove 0.170 in. min to 0.175 in. max wide top
Alliant Techsystems Inc. (00405)
Habegger AG (S0185)
NOW Corp. (26212)
Precision Speed Manufacturing LLC (56055)
Production Services Corp., The (03788)
SPS Technologies LLC (56878)
Stanadyne Corporation (84760)
United Technologies Corporation (52661,77445)

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558351 2915-00-981-4060Guide, Fuel FlowHamilton Sundstrand Corporation (73030)

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558372 2915-00-738-9191Housing, OrficeIII End Item Identification: 29158603736
General Characteristics Item Description: Aluminum alloy, QQ-266, temper T6 or AMS4121, rockwell hardness rating rb 78 min, heat treated MIL-H-6088 per united aircraft spec no. HS454, 0.680 in. min, to 0.685 in. max, O/a dia, on first end, 0.734 in. min, to 0.736 in. max O/a dia, on second end, 01.68 in. min, to /.700 in. lg
Hamilton Sundstrand Corporation (73030)

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558374 2915-00-738-9189Valve, Idle AdjustingIII End Item Identification: 29158603736
General Characteristics Item Description: Cress, QQ-S-763 per united aircraft spec no. HS178, rockwell hardness rating rc 30-38 min, 3/16-10-32 UNF2A on first end, 0.140 id, 0.300 in. O/a lg, on first end 0.51 in.O/a lg, 0.328 in min, 0.338 in.max, dia, on second end
Hamilton Sundstrand Corporation (73030)

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558387 2915-00-978-3029Valve Assy, PilotHamilton Sundstrand Corporation (73030)

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558404 2915-00-981-1305Plug, Fuel Control, THamilton Sundstrand Corporation (73030)

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558407 2915-00-986-7787Plug, Transfer ValveHamilton Sundstrand Corporation (73030)

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558409 2915-00-983-2499Body, CalibratingHamilton Sundstrand Corporation (73030)

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558410 2915-00-981-3072Retainer, FilterGeneral Characteristics Item Description: Aluminum alloy, QQ-A-225/4, anodized finish, MIL-A-8625, 0.138 in. min, 0.148 in. max O/a lg, stepped od, 0.360 in. min, 0.370 in. max od 1ST STEP1ST end, 0.060 in. min, 0.076 in. max lg 1ST step 1ST end, 0.423 in. min, 0.433 in. max od 2ND step 1ST end, 0.027 in. min, 0.039 in. max lg 2ND STEP1ST end, 0.492 in. min, 0.496 in. max od 2ND end, chamfered od 2ND end, 0.020IN. min, 0.030 in. max lg chamfer, 43 min, 47 max deg chamfer, thd bore, 0.250 IN.-28 unf series class 2B thd, 0.138 in. min, 0.148 in. max lg thd, bore countersunk at 1ST end, 88 min, 92 max deg by 0.310 in. nom diacountersink, 0.030 in. nom depth countersink
Hamilton Sundstrand Corporation (73030)

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558441 2915-00-983-2500Plug, Orifice, RetainHamilton Sundstrand Corporation (73030)

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  • We solve sourcing challenges for 557584, 5577790-505, 558231, 558351, 558372, 558374, 558387, 558407, 558409, 558441 - NSN parts, hard to find, long lead time and obsolete components.