FSC 4920 Aircraft Maintenance and Repair Shop Specialized Equipment: 4920-00-472-0778, 4920-00-472-1165, 4920-00-472-1757

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NSNMFG SKUItem NameDetailsManufacturer (CAGE)RFQ
4920-00-472-0778
4920004720778
PWA51180Test Plug, Aircraft ComponentSpecial Features: Company item name-plug, pressure test
End Item Identification: F100-PW-100/200/220/220E/229 engine oil tank
Reference Data and Literature: To 7J10-18-3
United Technologies Corporation (77445)

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4920-00-472-0791
4920004720791
PWA51181Test Plug, Aircraft ComponentSpecial Features: Company item name-plug, pressure test
General Characteristics Item Description: Rubber, aisi 1018-1020 steel, 10.000 in. lg, 1.500 in. dia
United Technologies Corporation (77445)

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4920-00-472-0797
4920004720797
PWA51182Test Plug, Aircraft ComponentSpecial Features: Company item name-plug, pressure test
End Item Identification: F100-PW-100/200/220/220E/229 engine oil tank
Reference Data and Literature: To 7J10-18-3
United Technologies Corporation (77445)

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4920-00-472-0970
4920004720970
11393Housing, Tape Reader AssemblyGeneral Characteristics Item Description: 19.000 in. lg, 15.157 in. W
Tally Printer Corporation (12344)

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4920-00-472-0973
4920004720973
11552Housing, Tape Reader AssemblyGeneral Characteristics Item Description: 1.250 in. lg, 1.250 in. W, 1.000 in. H
Tally Printer Corporation (12344)

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4920-00-472-0988
4920004720988
11553Adjusting Shaft, Read HeadGeneral Characteristics Item Description: 0.640 in. lg, 0.2495 in. dia, steel, passivated finish
Tally Printer Corporation (12344)

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4920-00-472-1037
4920004721037
GSE631001-03Fixture, Aircraft MaintenanceSpecial Features: Steel; company name-fixture, torque adjustment-clutch assembly
Functional Description: Used to support the clutch assy and pin the input gear to prevent rotation during loading of the clutch washer and torquing of clutch gearshaft
End Item Identification: F/TF15 a acft
Eaton Corporation (17472)

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4920-00-472-1042
4920004721042
3831000F101-1
3831000F101
Fixture, Hydraulic System ComponeSpecial Features: Steel and aluminum; company name-test fixture, servo-cylinder, stabilator
Functional Description: Used to support the stabilator servocylinder and provide axial alignment fo the servocylinder rod end during testing and cycling
End Item Identification: F-15 acft
Parker-Hannifin Corporation (93835)

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4920-00-472-1116
4920004721116
917E521G01Frame, Electronic System Test ConNorthrop Grumman Systems Corporation (18323)

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4920-00-472-1125
4920004721125
996D970G01Control Panel, Power, Test ConsoleEnd Item Identification: AN/ALQ-101 peculiar
General Characteristics Item Description: 400 hz, three phase
Northrop Grumman Systems Corporation (18323)

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4920-00-472-1136
4920004721136
997D869G01Monitor Panel, Test PanelEnd Item Identification: AN/ALQ-101 peculiar
General Characteristics Item Description: Three identical ammeters dual range 0 to 10A and 0 to 30A range, 1 frequency meter calibrated for 400 hz
Northrop Grumman Systems Corporation (18323)

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4920-00-472-1140
4920004721140
995D466G02Control Panel, Power, Test ConsoleEnd Item Identification: AN/ALQ-101 peculiar
General Characteristics Item Description: 50 or 60 hz, 115 volts, single phase
Northrop Grumman Systems Corporation (18323)

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4920-00-472-1165
4920004721165
0-49001-12Power SupplyFSC Application Data: Test set, electronic systems, specially designed, acft
Output Voltage Rating: 18.0 dc volts minimum 1ST power output and 22.0 dc volts maximum 1ST power output
Output Voltage Rating: 22.0 dc volts minimum 2ND power output and -18.0 dc volts maximum 2ND power output
Reliance Electric (50380)

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4920-00-472-1384
4920004721384
PWA24772Support, Compressor RotorReference Data and Literature: T.O. TF30P1-3-7-9
General Characteristics Item Description: Steel 50.000 in. lg, 11.500 in. W, 5.750 in. H
United Technologies Corporation (77445)

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4920-00-472-1543
4920004721543
A25A951-724-103Module AssemblyLockheed Martin Corporation (99696)

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4920-00-472-1545
4920004721545
AN/APM-381
31-020304-52
Test set, Countermeasures setEnd Item Identification: AN/ALE-38
Reference Data and Literature: T.O. 33D7-36-11-4
Test Type for Which Designed: Power; receiving
Joint Electronics Type Designation (80058)
Northrop Grumman Systems Corporation (26916, 15280)

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4920-00-472-1748
4920004721748
68D230023-1001
CD23A1521-2
Test set, IndicatorFunctional Description: Use to externally control the position of the landing gear proximity switches (weight on wheels) to facilitate maintenance of acft systems inhibited by these switches
End Item Identification: F-15 acft
Reference Data and Literature: Serd 0697; to 33D-1-104
Boeing Company,, The (76301)

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4920-00-472-1751
4920004721751
PWA23841Fixture, Aircraft MaintenanceSpecial Features: Approx 9.000 IN.H;40.000 in.dia;
United Technologies Corporation (77445)

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4920-00-472-1752
4920004721752
PWA23842Fixture, Aircraft MaintenanceFunctional Description: Used in support of acft maintenance on the TF30P-100 engine
Nominal Overall Height: 9.000 inches
Nominal Overall Diameter: 36.000 inches
United Technologies Corporation (77445)

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4920-00-472-1757
4920004721757
68D310016-1001Test box, Fuel GagingGeneral Characteristics Item Description: Aluminum, orange-yellow paint finish, 12.000 in. lg, 8.000 in. W, 7.500 in. H, C/O control panel, two test cables and a ground cable
Boeing Company,, The (76301)

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