Aircraft and Missile Prime Movers Engine Fuel System Components: 540905-37, 540953, 540979

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MFG SKUNSNItem NameDetailsManufacturer (CAGE)RFQ
540905-37
54090537
2915-00-675-9148Restrictor Assembly, Fluid FlowGeneral Characteristics Item Description: 0.0147 in. dia of restrictor hole, 37 pph flow rate, W/screen on one end
Hamilton Sundstrand Corporation (73030)

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540906 2915-00-986-7784Screw, Lever PositioHamilton Sundstrand Corporation (73030)

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540911 2915-00-719-8629Cover, Position AdjuHamilton Sundstrand Corporation (73030)
Ontic Engineering & Manufacturing (45934)

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540915 2915-00-723-7443Nozzle Assy, AspiratorGeneral Characteristics Item Description: Aluminum alloy, QQ-A-200-8 temper T6 or ams 4150, anodized per MIL-A-8625, 1.500 in. lg, 0.800 in W, 0.860 in. H
Hamilton Sundstrand Corporation (73030)

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540916 2915-00-723-7444Housing Assembly, TemperatureIII End Item Identification: 29159539325
General Characteristics Item Description: Steel, surface finish per MIL-A-8625 type I, rockwell hardness rating RB45
Hamilton Sundstrand Corporation (73030)

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54092 2915-00-177-8246Valve, Rocket, By PassIII End Item Identification: 29156328972
General Characteristics Item Description: Steel
Parker Hannifin Corporation (92003)
Parker-Hannifin Corporation (3H889,59211)

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540935-114
540935114
2915-00-657-8056Strainer Element, SedimentHamilton Sundstrand Corporation (73030)

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540935-118
540935118
2915-00-657-8057Strainer Element, SedimentHamilton Sundstrand Corporation (73030)

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540935-94
54093594
2915-00-657-8059Strainer Element, SedimentEND Item Identification: Fuel control, engine, acft
Filtering Media Design: MESH
Hamilton Sundstrand Corporation (73030)

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540935-98
54093598
2915-00-657-8060Strainer Element, SedimentHamilton Sundstrand Corporation (73030)

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540945 2915-00-654-2508Body Assembly, Aft, AfterburnerIII End Item Identification: Control assembly, fuel afterburner, P/N 540115L1, engine, J79, turbojet aircraft
Hamilton Sundstrand Corporation (73030)

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540946 2915-00-654-2519Bracket and SpringIII End Item Identification: Control assembly, afterburner, fuel P/N 540115L1, engine J 79, turbojet acft
Hamilton Sundstrand Corporation (73030)

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540948 2915-00-654-2524Lever and Pin AssemblyIII End Item Identification: Control assembly, fuel after burner, engine, J79, turbojet aircraft
General Characteristics Item Description: Braze per hamilton standard spec no 198, heat treatment per MIL-H-6875 and hamilton standard spec no 461, 0.397 in. min, 0.402 in. max O/a lg, 0.094 in. min, 0.096 in. max dia 2 holes
Hamilton Sundstrand Corporation (73030)

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540949 2915-00-654-2718Screw, Adjusting, AfterburnerIII End Item Identification: 29156750157
General Characteristics Item Description: Cres, ams 5610 per united aircraft spec no hs 178, 1.560 in. O/a lg, left end 0.300 in. lg of thread, right side tapered end 0.060 in dia
Hamilton Sundstrand Corporation (73030)

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540951 2915-00-700-6626Nut and Pin Assy, AdHamilton Sundstrand Corporation (73030)

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540952 2915-00-654-2374Screw and hub AjusterIII End Item Identification: 29156542394
Hamilton Sundstrand Corporation (73030)

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540953 2915-00-654-2430Base and Plate, RetainingIII End Item Identification: 29156750157
Hamilton Sundstrand Corporation (73030)

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540974 2915-00-673-8171Quadrant, Locking Screw PositionGeneral Characteristics Item Description: Cres per AMS5513 or AMS5515 and hamilton standard spec no. HS178, heat treatment per MIL-H-6875 and hamilton standard spec no. HS461
Hamilton Sundstrand Corporation (73030)

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540977 2915-00-724-2623Valve Assy, FilterIII End Item Identification: Engine acft, J75
Hamilton Sundstrand Corporation (73030)

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540979 2915-00-776-0305Cap and Shaft, ValveGeneral Characteristics Item Description: Cres, AMS5613, rockwell hardness RC30-46, 1.077 in. min, 1.083 in. max O/a lg
Hamilton Sundstrand Corporation (73030)

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