FSC 4920 Aircraft Maintenance and Repair Shop Specialized Equipment: 4920-01-439-2713, 4920-01-439-5470, 4920-01-439-5528
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 4920-01-439-2713 4920014392713 | 3R1302G01 | Holder, Test Strip | Functional Description: Required to hold the almen test strips in the correct location during intensity verification End Item Identification: F110-GE-100/129/400, F101-GE-102 and F118-GE-100 acft eng age Reference Data and Literature: Serd no. 6031 | General Electric Company (07482) | |
| 4920-01-439-3040 4920014393040 | 18906241100 | Pressure unit, Vacuum | Special Features: 6230 vac; 50 hz; light gray; rack mounted; 550 va power consumption; 52 psig at 0.67 scfm continuous pressure source; 29.7 in. mercury at 1.42 scfm vacuum source; 37 deg flared AN-4 output pressure and 37 deg flared AN-6 output vacuum fitting size | Kollsman Inc. (89944) | |
| 4920-01-439-3134 4920014393134 | 717769750-009 | Test Station, Electrical-Electron | Special Features: Comes within its own cabinets (2 units), has fork lift slots and hoisting eye lifts, is smaller version of depot test station End Item Identification: Lantirn | Lockheed Martin Corporation (04939) | |
| 4920-01-439-3233 4920014393233 | A55S96521-1 | Cable Assembly, Interface Device, | Special Features: Branched cable, special purpose End Item Identification: F-14 aircraft | Northrop Grumman Systems Corporation (61174, 26512) | |
| 4920-01-439-3717 4920014393717 | PWA71289 | Mask, Plasma Spray | Special Features: Fixture, almen test strip.engine P/N;4071223-01, 4081633-01.USED with PWA32704.CIP task 506, 379-20 Functional Description: Krequired to set and verify shotpeen equipment test parameters prior to shotpeen of the front compressor drum rotor. positions almen test STRIPS(PWA32704)AT repair planes of the 1ST, 2ND, and 3RD stage blade slots End Item Identification: F100-PW-229 eng | United Technologies Corporation (77445, 52661) | |
| 4920-01-439-3718 4920014393718 | PWA71290 | Mask, Plasma Spray | Special Features: Fixture, almen test strip-disk drum rotor, front compressor assy. eng P/N;4071223-01, 4081633-01CIPTASK506, 379-20 Functional Description: Required to set and verify shotpeen equipment test parameters prior to shotpeen of front compressor drum rotor End Item Identification: F100-PW-229 engine | United Technologies Corporation (77445, 52661) | |
| 4920-01-439-3733 4920014393733 | PWA71621 | Fixture, Engine Maintenance, Aircr | Special Features: Fixture. BLK03 eng P/N;4083973, 4077671 used on numerical controlled laser machine Functional Description: Fixture is required during reoperation and reidentification of the combustion chamber by replacement of the inner rear section that includes the NO.5 panel and aft flange per SL241599. fixture holds inner assy and locates the kingpin hole that is the construction point for all holes End Item Identification: F100-PW-229 | United Technologies Corporation (77445) | |
| 4920-01-439-3734 4920014393734 | 3R1300G01 | Fixture, Engine Maintenance, Aircr | Special Features: C/O an aluminum mtg plate; steel sleeve; aluminum sleeve; aluminum cover. the mtg plate serves to mount the fixture to the machine table. the steel sleeve supports the fan shaft and masks the shaft inner diameter aft of the forward pilot diameter. the aluminum sleeve masks the shaft outer diameter. the cover masks the shaft inner diameter forward of the pilot diameter Functional Description: During overhaul it may be necessary to thermal spray repair the aft fan shaft forward pilot diameter. it is necessary to mask all surfaces adjacent to the repair surface and support the shaft during the thermal-spray repair operation. this reusable fixture performs these functions End Item Identification: F110-GE-100/129/400 and F118-GE-100 acft engine age | General Electric Company (07482) | |
| 4920-01-439-3735 4920014393735 | 3R1024G01 | Fixture, Machining, Aircraft Engin | Special Features: Serd item name=fixture, machining, shroud interlock-concave, stage 2 Functional Description: Fixture is used to hold and position the fan blade so that accurate machining can be performed. will clamp blade dovetail at one end and the airfoil wear tip shroud end to restrain blade to nominal cinfiguration and position for machining on conclave side End Item Identification: Supports repair of P/N 1276M42G02, nsn 2840-01-146-9445, blade, stage 2, engine F101-GE-102 | General Electric Company (07482) | |
| 4920-01-439-3811 4920014393811 | AD420580G01 | Fixture, Engine Maintenance, Aircr | Functional Description: Holding fixture assy twt cooling loop End Item Identification: F-16 radar Reference Data and Literature: AD420580 | Northrop Grumman Systems Corporation (18323) | |
| 4920-01-439-4072 4920014394072 | PWA56682 | Fixture, Engine Maintenance, Aircr | Special Features: Supercedes PWA51725 Functional Description: Used to lift and handle the low pressure turbine while maintaing the radial position of the roto and stator to prevent damage to airseals and blades End Item Identification: F100-PW-100/200/220/220E engine | United Technologies Corporation (77445) | |
| 4920-01-439-4154 4920014394154 | 18868 18869 | Case, Test set | Special Features: Gray in color Overall Length: 7.900 inches nominal Overall Width: 4.300 inches nominal | Jameco Electronics (2P910) Neogenerations Devices And (08LF6) | |
| 4920-01-439-4298 4920014394298 | 501750-2001 | Panel, Interface Device | FSC Application Data: Special ground servicing equip | Fleet Readiness Center Southwest (91145) | |
| 4920-01-439-4723 4920014394723 | PWA57909 | Fixture, Engine Maintenance, Aircr | Special Features: Characteristics are 30.000 inch length; 24.000 inch width; 12.000 inch height; 120 lbs weight Functional Description: Used to install the 7TH, 8TH, AND9TH stage compressor inner stator shroud segments by pre-positioning the stator segment, damper spring, and shroudsegment into the tool and then rotating the shroud into the stator in a controlled manner; prevents overloading the anti-rotation lugs in the stator End Item Identification: F100-PW-229 | United Technologies Corporation (77445) | |
| 4920-01-439-5126 4920014395126 | 3R1300G02 | Fixture, Engine Maintenance, Aircr | Functional Description: Support the aft fan shaft during thermal spray repair operations, also to mask all surfaces adjacent to the repair surface End Item Identification: Unique to F101-GE-102 engine Reference Data and Literature: Serd 6016 | General Electric Company (07482) | |
| 4920-01-439-5127 4920014395127 | DAA7293G302-001 | Fixture, Aircraft Maintenance | Special Features: Consists of a steel frame with a lifting eye; approx. 10.250 in. l; 20.500 in. w; 0.125 in thickness; mfg. name: lift receiver Functional Description: Used to raise and lower defensive measurement system and electronic counter measurement system componets in the aft bay area End Item Identification: B-2 | Northrop Grumman Systems Corporation (1W025) | |
| 4920-01-439-5128 4920014395128 | DAA7257L015-001 | Fixture, Aircraft Maintenance | Special Features: Submitted name tool kit acft maintenance Functional Description: Provides means to cut a trough inthe foam and form the copper mesh intothe trough End Item Identification: B-2 acft | Northrop Grumman Systems Corporation (1W025) | |
| 4920-01-439-5130 4920014395130 | DAA7257G373-001 | Fixture, Aircraft Maintenance | Special Features: Submitted name manifold set Functional Description: Provide capability to cure the MS-215 type 2 foam adhesive on the core slices End Item Identification: B-2 acft | Northrop Grumman Systems Corporation (1W025) | |
| 4920-01-439-5470 4920014395470 | 1811H165 | Tester, Pitot and Static Systems | Barfield Inc. (21844) | ||
| 4920-01-439-5528 4920014395528 | 3R1023G01 | Fixture, Machining, Aircraft Engin | Functional Description: Hold and position the fan blade, fixture will clamp the blade dovetail at one end and the airfoil wear the tip shroud end to restrain blade to nominal configuration and position for machining on convex side End Item Identification: Supports repair of P/N 1276M42G02, nsn 2840-01-146-9445, blade, stage 2; engine F101-GE-102 Reference Data and Literature: 2J-F101-3-06 wp 047 oo; contract F33657-95-C-0055, serd 6090 | General Electric Company (07482) |