Measuring Tools, Craftsmen's: PWA81694, PWA81996, PWA9826

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MFG SKUNSNItem NameDetailsManufacturer (CAGE)RFQ
PWA81694 5210-01-384-9275Gage, AngleSpecial Features: Rqrd to check final bend angle of 6TH stage high pressure compressor for conformance to engine assy;gage is clear plastic plate W/2 steel locating pins;line scribed into plastic for checking bend ANGLES;3.2 in. ln by 3.0 in. wd by 0.9 in. HT;0.5 LB;75 deg marked on gage
END Item Identification: 117 engine, serd 1407
Part Name Assigned BY Controlling Agency: Gage, angle, bend
United Technologies Corporation (77445)

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PWA81695 5210-01-384-9103Gage, AngleSpecial Features: Required to check final bend angle of 7TH stage hpc blade lock
Blade Quantity: 1
United Technologies Corporation (77445)

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PWA8171 5210-00-607-8110Indicator, DialSpecial Features: Gage, coupling;item consists of 1 body, aluminum casting, 22.75 in. LG;1 locator, mach STEEL;1 block 1.0625 in. by 1.250 in. by 1.75 IN.;1 dial indicator
United Technologies Corporation (77445)

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PWA81929 5210-01-388-4907Gage, HeightSpecial Features: To measure axial deflection of 3RD stage turbine vane cluster
END Item Identification: F117-PW-100
Material: Steel
United Technologies Corporation (77445)

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PWA81930 5210-01-387-5483Gage, Thickness, Dial IndicatingEND Item Identification: F117-PW-100
General Characteristics Item Description: Overall height 5.000IN X 10.500INDEEP X 4.000IN wide;gage required to measure axial deflection of 4TH stage turbine vane cluster;serd 1114
United Technologies Corporation (77445)

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PWA81931 5210-01-387-5468Gage, Thickness, Dial IndicatingEND Item Identification: F117-PW-100
General Characteristics Item Description: Overall height 6.200IN X 13.000INDEEP X 5.500IN wide;gage required to measure axial deflection of 5TH stage turbine vane cluster;serd 1115
United Technologies Corporation (77445)

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PWA81933 5210-01-387-4279Gage, Thickness, Dial IndicatingEND Item Identification: 117 engine
General Characteristics Item Description: Axial deflection gage is an assy that holds A seventh stage vane cluster at the outer shroud, and has A metertype dimension gage positioned above the inner shroud of the vane cluster;the indicator shaft impinges on the inner front surface of the vane CLUSTER;15.6 in. lg by 6.0 in. wd by 6.5 in. HT;26.0 lbs;rqrd to measure axial deflection of the seventh stage vane clustersof the low pressure turbine;serd 1826
United Technologies Corporation (77445)

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PWA81934 5210-01-385-7601Gage, Thickness, Dial IndicatingGeneral Characteristics Item Description: Gage measures deflection of rear retaining plate of high pressure turbine second stage rotor after riveting;size 9.000IN height X 2.800IN wide X 5.000IN deep; plastic case included
United Technologies Corporation (77445)

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PWA81947 5210-01-387-5492Gage, Thickness, Dial IndicatingEND Item Identification: F117-PW-100
General Characteristics Item Description: Overall height 4.500IN X 2.500IN wide X 6.000IN deep;gage required to measure shroud twist of 3RD and 4TH stage low pressure turbine blades before and after twist is corrcted;serd 1659
United Technologies Corporation (77445)

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PWA81949 5210-01-387-4354Gage, Thickness, Dial IndicatingEND Item Identification: 117 engine
General Characteristics Item Description: C/O yoke base that attaches to A check and correct fixture, spring loaded slide that holds A dial indicator, and spring operated locator;container provided for storage; 6.0 in. lg by 2.5 in. wd by 4.5 in. HT;4.0 lbs;rqrd tomeasure shroud twist of seventh stage low pressure turbine blade before and after twist is corrected;serd 1119
United Technologies Corporation (77445)

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PWA81961 5210-01-384-9048Gage, Thickness, Dial IndicatingEND Item Identification: C-17
General Characteristics Item Description: Gage is A flat steel plate W/bolted and doweled supports, 2 pin locators, set of fixed and moveable contacts and dial indicator W/holder;built in feature to zero dial indicator;lever operated slide to load and unload part;rqrd to measure 9TH through the 17TH stage high pressure compressor blade airfoil THICKNESS;4.50 in. lg by 3.50 in. wd by 2.20 in. ht
Reference Data AND Literature: Serd 1521
United Technologies Corporation (77445)

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PWA81962 5210-01-384-2715Gage, Thickness, Dial IndicatingGeneral Characteristics Item Description: Overall size 4.50IN X 3.50IN X 2.20IN;REQUIRED to measure the 7TH and 8TH stage high pressure compressor blade airfoil thickness
United Technologies Corporation (77445)

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PWA81963 5210-01-387-5482Gage, Thickness, Dial IndicatingEND Item Identification: F117-PW-100
General Characteristics Item Description: Overall height 4.500IN X 6.000IN deep X 2.500IN wide; gage required to measure shroud twist of 6TH stage low pressure turbine blade before and after twist is corrected;serd 1121
United Technologies Corporation (77445)

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PWA81970 5210-01-378-9606Gage, Depth, Dial IndicatingSpecial Features: C/O steel rectangular tube W/feet extending at each end, sliding indicator assy attached at center;gages low pressure turbine running position at rear flange of high pressure turbine case, while driveshaft has rearward load applied;used for maintenance on F117-PW-100 ENGINE;4 in. HT;31 lbs;periodic dial indicator calibration rqrd;serd no. 0386
Base Length: 36.000 inches nominal
Base Width: 10.000 inches nominal
United Technologies Corporation (77445)

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PWA81981 5210-01-387-5484Gage, HeightSpecial Features: Overall length 6.000IN X 3.300IN wide X 2.000IN high; gage required to determine if height of knife edge of low pressure turbine blade is worn below minimum limit;serd 1122
END Item Identification: F117-PW-100
Material: Steel
United Technologies Corporation (77445)

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PWA81985 5210-01-387-5476Gage, HeightSpecial Features: 11.100IN overall length X 2.900INWIDE X 2.000IN high; gage used to determine if height of knife edge of low pressure turbine blade is worn below its minimum limit;serd 1126
END Item Identification: F117-PW-100
Material: Steel
United Technologies Corporation (77445)

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PWA81996 5210-01-388-4039Caliper, Indicator, OutsideEND Item Identification: 117 engine
General Characteristics Item Description: 8.0 in. lg by 2.0 in. wd by 1.0 in. ht O/a;rqrd to measure wear on sixth through ninth stage variable vanes of high pressure compressor;gage is A dial caliper W/modified jaws;serd 1594
United Technologies Corporation (77445)

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PWA83201 5210-01-384-9796Gage, AngleSpecial Features: E16.0 in. lg by 8.0 in. wd by 6.0 in. ht;protractor assy rqrd to set angle of turn on sixth stage high pressure compressor tie rod nut;c/O socket wrench and includes protractor scale andtorque lever
END Item Identification: C-17, serd 1584
Design Type: Single blade
United Technologies Corporation (77445)

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PWA83237 5210-01-386-2207Gage, AngleSpecial Features: Serd 1002;GAGE is A steel assy W/removable gage block, upper and lower body, lock ring, leg plunger and 3 leg clamps;rqrd to check for proper angle offfuel nozzle guides after repair of combustion chamber fuel nozzle GUIDES;3.5 in. ht by 2.3 in. DIA;1 lb
END Item Identification: 117 engine
Part Name Assigned BY Controlling Agency: Gage, angle, fuel
United Technologies Corporation (77445)

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PWA9826 5210-00-772-3781Gage, AnglePart Name Assigned BY Controlling Agency: Gage, vane angle
United Technologies Corporation (77445)

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