FSC 4920 Aircraft Maintenance and Repair Shop Specialized Equipment: 4920-01-489-1417, 4920-01-490-3895, 4920-01-490-3919
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 4920-01-489-1417 4920014891417 | 15845 915-15845 | Trim tab Bending to | Honeywell International Inc. (99866) | ||
| 4920-01-489-1420 4920014891420 | 214-240-001-101 | Hanger, Simulator, Ta | Special Features: Required to align the three tailboom bearing hangers End Item Identification: Helicopters (H1) Part Name Assigned BY Controlling Agency: Hanger, simulator, tail rotor driveshaft | Bell Helicopter Textron Inc. (97499) | |
| 4920-01-489-1421 4920014891421 | 214-240-002-101 | Hangar Simulator, Ta | Special Features: Used to confirm the alignment of the 214-030-346 tail boom bearing support fittings after an aligned tailboom is installed on the aircraft End Item Identification: Support equipment for the UH-1Y Overall Length: 7.500 inches nominal | Bell Helicopter Textron Inc. (97499) | |
| 4920-01-489-1424 4920014891424 | CUTA1870306C | Tool set Installati | Special Features: The tool set contains a body tool, a pin installation tool, a pin extration tool and a striker and tapset. the first three tools are threaded at the end to engage internal threads of the pin of the valve body as required.the striker slides on the shaft of either of the first two tools and is used to strike the head, thus driving out the pin or valve body. the body tool is used to to push the rfi valve insert firmly into the reamed bore of the valve bodythe pin installation tool is then used to press the expander pin into the valve body so that the external lands bite into the cavity wall to seal and lock the insert into place. the body insert of some lee check valves normally removed using this set may not be threaded. the tapset is provided so that the insere can be threaded to accomodate the threads of the body tool when removal of the insert is necessary End Item Identification: F/A-18 Part Name Assigned BY Controlling Agency: Tool set, installation/extraction | The LEE Company (92555) | |
| 4920-01-489-5355 4920014895355 | L9751-101-001 | Modification kit, Maintenance and | Special Features: Hardware and software required to modify VP5025D hydraulic pump/motor test system 4920-01-262-1413 for B-2 application End Item Identification: Pacer special Part Name Assigned BY Controlling Agency: Modification kit, hydraulic pump/motor test system | Dayton T. Brown Inc. (96362) | |
| 4920-01-489-5461 4920014895461 | CUTA2180203A | Tool, Installation, a | Special Features: Tool set contains a body tool, pin extraction tool, a pin installation tool, and a striker. the three tools are threaded at the end to engage internal threads of the pin or the restrictor as required. the striker slides on the shaft of either of the first two tools and is used to strike the head, thus driving out the restriker body. the body tool is also used to push the rfi restriker insert firmly into the reamed bore of the manifold. the pin installation tool is then used to press the expander pin into the restriker body so that the external lands bite into the cavity wall to seal and lock the insert in place. End Item Identification: F/A-18 Part Name Assigned BY Controlling Agency: Tool, installation | The LEE Company (92555) | |
| 4920-01-489-5817 4920014895817 | 914521-1 | Transducer | Special Features: Stanless steel; 1.125" dia, 3.5" L W/O conn; response time less than one millisecond; input power not toexceed 2 watts; output impedance less than 500 ohms; full scale output 5.0 vdc; excitation 28 vdc; infinite resolution; operating temp M40 deg C to P52 deg c; oper. End Item Identification: F-16 a/B acft ege Precious Material: GOLD | Honeywell International Inc. (06848, 70210) | |
| 4920-01-490-0083 4920014900083 | DCU-301/E PWA59201 | Control Panel, Test | Special Features: Company item name controller End Item Identification: F119 acft, F-22 engine | United Technologies Corporation (77445) Aeronautical and Support Equipment (07878) | |
| 4920-01-490-0084 4920014900084 | PWA59216 | Control Panel, Test | Special Features: Company item name-controller End Item Identification: F-119 acft, F-22 engine | United Technologies Corporation (77445) | |
| 4920-01-490-0708 4920014900708 | NBM | Fixture, Aircraft Maintenance | Special Features: 4 forklift pockets and tow bar, 4 heavy duty swivel casters and brake, non skid work surfaces, adjustable ground clearance, accessory storage, min height 47.250IN, min width 48.000, airdrive hydraulic pump Functional Description: Aircraft component changer used in removal/installation of items such as landing gear assemblies. performs as landing gear changer, transporter, holding fixture End Item Identification: C-130 aircraft and others | D-Check Developments Inc. (1T0V3) | |
| 4920-01-490-2941 4920014902941 | E73073001 184000-715 | Test Stand, Hydraulic System Comp | Special Features: Company item name-hydraulic test stand console Functional Description: Used to provide the hydraulic fluid pressure to perform extention, retraction, and static proof pressure tests on the various actuator assdmblies End Item Identification: B-2 acft | Moog Inc. (94697, 19156) | |
| 4920-01-490-2969 4920014902969 | 184000-720 | Fixture, Hydraulic System Compone | Special Features: Company item name-loading test fixture; materail steel and aluminum Functional Description: Used to perform the required extention and retraction tests of various acuator assemblies End Item Identification: B-2 acft | Moog Inc. (94697, 19156) | |
| 4920-01-490-2973 4920014902973 | PWA72613 | Fixture, Engine Maintenance, Aircr | Special Features: Requested name-fixture, grit blastplasma spray-lpt case Functional Description: Positions and holds turbine case End Item Identification: F100-PW-100/200/220/220E | United Technologies Corporation (77445) | |
| 4920-01-490-3033 4920014903033 | PWA72612 | Fixture, Machining, Aircraft Engin | Special Features: Requested name-fixture, machine-lpt case Functional Description: Positions and holds turbine case on a rotary grind machine table duringpreliminary and final machining of therepair diameters End Item Identification: F100-PW-100/200/220/220E | United Technologies Corporation (77445) | |
| 4920-01-490-3894 4920014903894 | PWA72633 | Fixture, Machining, Aircraft Engin | Special Features: Requested name-fixture, machine-rear compressor stator inlet shroud, id snap repair Functional Description: Required for nickel plate repair of a worn snap diameter on P/N4052250, rear compressor stator inlet shroud (inner rear) End Item Identification: F100-PW-220, 220E | United Technologies Corporation (77445) | |
| 4920-01-490-3895 4920014903895 | PWA72637 | Fixture, Engine Maintenance, Aircr | Special Features: Requested name-fixture, test STRIP4TH stage turbine air seal Functional Description: Required for inner flange shotpeen of 4TH turbine air seal P/N4086505, consists of (3) PWA32704 test strip block details that simulate the face locations/elevations of the air seal inner diameter flange End Item Identification: F100-PW-100/200/220/220E | United Technologies Corporation (77445) | |
| 4920-01-490-3901 4920014903901 | 184000712 | Fixture, Hydraulic System Compone | Special Features: Company item name-cycling fixture; made of two long rectangular beams, steel and aluminum Functional Description: Used to hold hydraulic actuators during extention and retraction for testing and repair End Item Identification: B-2 acft | Moog Inc. (94697, 19156) | |
| 4920-01-490-3909 4920014903909 | E13911-001 | Adapter, Test Block | Special Features: Interfaces B33497 pilot valve assy with B7557 nozzle pushing test stand. consists of E13772-1 test block and AT-2133-001 adapter block End Item Identification: B-2 aircraft flight control system Reference Data and Literature: Serd 2894 | Northrop Grumman Systems Corporation (1W025) Moog Inc. (94697) | |
| 4920-01-490-3910 4920014903910 | E60271-001 | Adapter, Test Block | Special Features: Interfaces B33497-1 or B33647-1 check valve to B7557 nozzle pushing test stand during testing. consists of E05015-1 test block, E05019-1 test block, AT-2133-001 adapter block, fittings, tubings, valves, and adapters End Item Identification: B-2 aircraft flight control system Reference Data and Literature: Serd 2915 | Moog Inc. (94697) Northrop Grumman Systems Corporation (1W025) | |
| 4920-01-490-3919 4920014903919 | PWA72615 | Mask, Plasma Spray | United Technologies Corporation (77445) |