Aircraft and Missile Prime Movers Engine Fuel System Components: 558766, 558789, 560917-1

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MFG SKUNSNItem NameDetailsManufacturer (CAGE)RFQ
558766 2915-00-737-8839Lever, ResetIII End Item Identification: 29158603738
General Characteristics Item Description: 3.050 in. min, 3.090 in. max lg, irregular shape
Hamilton Sundstrand Corporation (73030)

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558773 2915-00-737-0974Guide and Pivot, ResetIII End Item Identification: 29158603738
General Characteristics Item Description: Irregular shape
Hamilton Sundstrand Corporation (73030)

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558776 2915-00-986-7785Plunger and Pin AssHamilton Sundstrand Corporation (73030)

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558781 2915-00-986-0043Guide and Pivot, ResHamilton Sundstrand Corporation (73030)
Ontic Engineering & Manufacturing (45934)
The Durol Company (7D869)

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558789 2915-00-986-7822Retainer, PlateHamilton Sundstrand Corporation (73030)

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558792 2915-00-991-7570Shaft and Sleeve, Mounting nutGeneral Characteristics Item Description: Shaft, steel, AMS6415, rockwell C scale 32 min, 38 max hardness, cadmium plated finish QQ-P-416, sleeve, nylon zytel category C fscm 73030, 8.920 in. min, 8.960 in. max O/a lg, 1ST STEP0.740 in. max lg 1ST step 1ST end, 2ND .740 in. max lg 1ST step 1ST end, 2ND step 1ST end tapered, 0.310 in. nom smallest od 2ND step 1ST end, 6.940 in. min, 7.060 in. max lg 2ND step 1ST end, 0.860 in. nom lg 3RD step 1ST end, 2ND end hex shape, 0.380 in. nom lg 2ND end, 0.500 in. nom W across flats, int thd 1ST end, 0.3125 IN.-24 series unf 2B thd, 0.450 in. min depth thd countersunk 85 deg min, 95 deg max to 0.320 in. min, 0.360 in. max dia at 1ST end, 1 hole 0.050 in. nom dia through hex flats 2ND end, 0.150 in. nom distance from 2ND end to hole center
Hamilton Sundstrand Corporation (73030)

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559-0005-01
559000501
2915-01-171-0282Vane AssemblyAllen R C Instruments Inc. (06275)
Kelly Manufacturing Company (08AF1)

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559-0010-01
559001001
2915-01-171-0281Vane AssemblyAllen R C Instruments Inc. (06275)
Kelly Manufacturing Company (08AF1)

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5592239 2915-00-486-7832Arm-Rocker Fuel PumTest Data Document: 81580-10469 drawing (this is the basic governing drawing, such as a contractor drawing, original equipment manufacturer drawing, etc.; excludes any specification, standard or other document that may be referenced in a basic governing drawing)
General Motors Corp. (70040)

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5594706-1
55947061
2915-01-257-2132Housing, SpecialTriumph Controls LLC (78710)

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559A6D40 2915-00-949-1948Valve, Pressure Relief, FuelIII End Item Identification: F111 aircraft engine fuel system
General Characteristics Item Description: Aluminum alloy W/anodized finish, 2 gpm at 55 psid rated flow, pressures, operating 60 psi, proof 120 psi, burst 180 psi, 30 psi min reset pressure, 45 psi max cracking pressure, 0.810 in. O/a lg, 0.650 in. dia top end, 0.810 in. dia hex, end fitting inlet per MS33656E6, thd and 0.350 in. lg
Circor Aerospace Inc. (91816)

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560780 2915-00-915-2706Housing Assy, Fuel DUnited Technologies Corporation (52661,77445)

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560781 2915-00-408-3553Valve, Fuel Pressurizing and DrainIII End Item Identification: Engine, aircraft, model TF30
United Technologies Corporation (77445)

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56084 2915-00-073-7302Valve Assembly, NozzleIII End Item Identification: Nozzle assembly P/N 5232270
Delavan Inc. (71895)

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560880 2915-00-562-2112Valve Body, AfterburnerGeneral Characteristics Item Description: C/O body, studs, screw thread inserts, plugs and pin
United Technologies Corporation (77445)

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560903 2915-00-716-2602CAPHamilton Sundstrand Corporation (73030)
Ontic Engineering & Manufacturing (45934)
Reliable Manufacturing Company (2U656)

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560910 2915-00-716-2593PistonHamilton Sundstrand Corporation (73030)

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560911 2915-00-716-2599RetainerHamilton Sundstrand Corporation (73030)

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560912 2915-00-716-2594RetainerHamilton Sundstrand Corporation (73030)

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560917-1
5609171
2915-00-716-2663ValveHamilton Sundstrand Corporation (73030)

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  • We solve sourcing challenges for 558766, 558781, 558789, 559-0010-01, 5592239, 560781, 560903, 560911, 560912, 560917-1 - NSN parts, hard to find, long lead time and obsolete components.