Inspection Gages and Precision Layout Tools: PWA81889-1, PWA81948, PWA83167
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| PWA81889-1 PWA818891 | 5220-01-386-2037 | Gage, Profile | Special Features: Wserd 1414;5.3 in. lg by 0.8 in. wd by 0.5 in. HT;0.1 lb;rqrd to inspectlength of sixth stage high pressure compressor blade;master is hardened steel machined blank dimensioned to simulate level of acceptability of A specific blade END Item Identification: 117 engine | United Technologies Corporation (77445) | |
| PWA81889-2 PWA818892 | 5220-01-384-9790 | Gage, Profile | Special Features: Rqrd to inspect length of seventhstage high pressure compressor blade;hardened steel machined BLANK;0.80 in. lg by 0.50 N. wd by 4.40 in. ht END Item Identification: C-17, serd 1415 | United Technologies Corporation (77445) | |
| PWA81889-3 PWA818893 | 5220-01-383-9901 | Gage, Profile | Special Features: 3.900IN height X 0.700IN wide X 0.800IN deep;used to measure the high pressure compressor blade lengths | United Technologies Corporation (77445) | |
| PWA81889-4 PWA818894 | 5220-01-384-9809 | Gage, Profile | Special Features: Rqrd to inspect length of ninth stage high pressure compressor blade;hardened steel machined BLANK;0.80 in. lg by 0.40 in. wd by 3.50 in. ht END Item Identification: C-17, serd 1417 Design Type: Single end | United Technologies Corporation (77445) | |
| PWA81948 | 5220-01-386-9143 | Gage, Profile | Special Features: Gage, TWIST;6.0 in. lg by 2.5 in. wd by 4.5 in. HT;3.5 lbs;rqrd to measure the shroud twist of the fifth stage low pressure turbine;c/O yoke base that attaches to A check and correct fixture, spring operated slide that holds A dial indicator, stable locator, spring operated locator and A plastic storage container END Item Identification: 117 engine;serd 1118 | United Technologies Corporation (77445) | |
| PWA81960 | 5220-01-386-3808 | Gage, Disk, Master Setting | Special Features: Egage, master, inspection;necessary to prepare for the inspection and correction of twist in the 3RD thru the 7TH stage low pressure turbine BLADES;11.300 in. lg X 1.000 in. wd X 1.600 in.hg;serd 1120 END Item Identification: F117-PW-100 | United Technologies Corporation (77445) | |
| PWA81982 | 5220-01-387-5325 | Gage, Profile | Special Features: Rqrd to determine if height of knife edge of low pressure turbine bladeis worn below its minimum limit;gage is A welded steel assy W/bottom and 2 extended surfaces at the top;plastic container is provided for STORAGE;7.3 in. lg by 3.1 in. wd by 2.0 in. HT;5 lbs;serd 1123 END Item Identification: 117 engine Length: 7.300 inches | United Technologies Corporation (77445) | |
| PWA81983 | 5220-01-386-8830 | Gage, Profile | Special Features: Gage used W/PWA81946 fixture to find if height of knife edge of lpt blade is worn below its minimum LIMIT;3.2IN. wd by 2.0 in. HT;5.0 lbs;gage is awelded steel assy W/bottom and two extended surfaces at the top;serd 1124 END Item Identification: 117 engine Design Type: Single end | United Technologies Corporation (77445) | |
| PWA81984 | 5220-01-387-5320 | Gage, Profile | Special Features: 9RQRD to determine height of knifeedge of low pressure turbine blade below its min limit;gage is A welded steel assy W/bottom and 2 extended surfaces at top;plastic container provided for STORAGE;10.6 in. lg by 3.1 in. wd BY2.0 in. HT;5 lbs;serd 1125 END Item Identification: 117 engine Length: 10.600 inches | United Technologies Corporation (77445) | |
| PWA8209 | 5220-00-560-7246 | Gage, Ring, Plain | Special Features: Ring, spline | United Technologies Corporation (77445) | |
| PWA8260 | 5220-00-591-8561 | Gage, Mount Distance | United Technologies Corporation (77445) | ||
| PWA827 | 5220-00-142-7203 | GAGE | United Technologies Corporation (77445) | ||
| PWA8282 | 5220-00-588-6005 | Gage, Profile | Special Features: Gage, ball bearing F | United Technologies Corporation (77445) | |
| PWA8298 | 5220-00-570-1394 | Gage, Profile | Special Features: Gage, accessory driv | United Technologies Corporation (77445) | |
| PWA83029 | 5220-01-393-2387 | Gage, Coating Thickness | END Item Identification: C-17 engine General Characteristics Item Description: Rqrd to check high pressure compressor rear case 13TH stage groove on the pre machine operation prior to plating and finish machine operation afterplating;gage is rectangular steel bar W/brazed tubular holder attached to bar which supports dial indicator;there are 2 rest pads and 2 carbide contact points;serd 1471;26.3 in. lg by 2.0 in. wd by 3.0 in. ht;wt 5 lbs Reference Data AND Literature: Serd 1471 | United Technologies Corporation (77445) | |
| PWA83030 | 5220-01-392-6897 | Gage, Disk, Master Setting | Special Features: Fgage, diameter, master setting;required to set PWA83029 indicator gage to basic diam. to check hpc rear case 13TH stage groove at premachine oper prior to plating and finish machine oper after plating | United Technologies Corporation (77445) | |
| PWA83034 | 5220-01-386-1234 | Gage, Profile | Special Features: Vrqrd to determine if first stage turbine vane airfoil tkns is acceptable;c/O 3 U-shaped templates at 3 airfoil sections of the VANE;2.7 in. lg by 1.5 in. wd by 2.0 in. ht;storage dim. 5.3 in. ln by 5.3 in. wd by 4.0 in. HT;1.2 lb END Item Identification: 117 engine | United Technologies Corporation (77445) | |
| PWA83150 | 5220-01-380-0477 | Gage, Profile | Special Features: Template gage required to check the maximum and minimum height on rubber seals in the 2.5 bleed valve duct Gage Type: Acceptance check Design Type: Double end | United Technologies Corporation (77445) | |
| PWA83166 | 5220-01-390-6915 | Gage, Profile | Special Features: Required to check clearance between the low pressure turbine case and cooling air duct manifold and rear of "p" flange END Item Identification: F117-PW-100 Gage Type: Combination go not go | United Technologies Corporation (77445) | |
| PWA83167 | 5220-01-378-6105 | Gage, Flush Pin, Plain Cylindrical | Special Features: Rqrd to properly locate cooling air duct manifold relative to front flange of low pressure turbine;c/O gage body, three clamp assemblies, two locating pins and two stepped flush pins;matl steel;clamps attach gage to front face of low pressure turbine flange;locating pins psition gage;flush pins bear against cooling air manifold;position of stepped surfaces relative to gage body determine if manifold properly located;plastic container is provided for storage;serd no. 0336 | United Technologies Corporation (77445) |