Aircraft Maintenance and Repair Shop Specialized Equipment: PWA-71097, PWA71100, PWA71118

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MFG SKUNSNItem NameDetailsManufacturer (CAGE)RFQ
PWA-71097
PWA71097
4920-01-393-0231Mask, ShotpeenFunctional Description: Used to mask the unaffected areas inside of the rr. snap dia of the 4TH/5TH drum rotor during shotpeen operations
End Item Identification: F100-PW-229
Reference Data and Literature: Pw serd no. 7207
United Technologies Corporation (52661,77445)

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PWA71098 4920-01-422-1650Fixture, Engine Maintenance, AircrSpecial Features: Company item name-fixture machine case fan inlet
Functional Description: Used to locate and secure the inlet fan case assy P/N4078176 during rough and finish machining of the aft faring
End Item Identification: F100-PW-229 engine
United Technologies Corporation (77445)

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PWA71099 4920-01-421-9731Fixture, Machining, Aircraft EnginSpecial Features: Company item name-fixture machine case, fan
Functional Description: Used to locate and secure replacement detail (P/N4081223) during machining of electron beam weld prep
End Item Identification: F100-PW-229 engine
United Technologies Corporation (77445)

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PWA71100 4920-01-421-8179Fixture, Engine Maintenance, AircrSpecial Features: Company item name-fixture electron beam weld case fan inlet
Functional Description: Used to locate and secure the inlet fan case assy (P/N4078176) and replacement fairing DETAIL(P/N4081223)DURING electron beam welding of assy
End Item Identification: F100-PW-229 engine
United Technologies Corporation (77445)

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PWA71101 4920-01-425-4656Fixture, Engine Maintenance, AircrSpecial Features: Company name-fixture, stress relief, case, fan inlet
Functional Description: Used as stress relief fixture, during fan inlet case repair
End Item Identification: F100-PW-229 engine
United Technologies Corporation (77445)

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PWA 71102
PWA71102
4920-01-422-9106Fixture, Engine Maintenance, AircrFunctional Description: Required to locate and secure inlet fan case assembly during shotpeening of repaired aft fairing surface
End Item Identification: F100-PW-229 engine
Reference Data and Literature: Serd no 7213
United Technologies Corporation (77445)

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PWA 71103
PWA71103
4920-01-424-7963Holder, Test StripEnd Item Identification: F100-PW-229
General Characteristics Item Description: Consists of an aluminum base having a center hub with two extended arms; a countersunk hole at the underside of the hub fits over the receiver puck of PWA70449; aluminum is anodixed, attachment hardware details are sst, and the fixture is coated with a polymer coating except for the aisi A2 blocks which have a black oxide surface finish; holder is used to set shot peen parameters on the fan inlet case
Overall Length: 36.000 inches nominal
United Technologies Corporation (52661,77445)

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PWA 71104
PWA71104
4920-01-424-2483Mask, ShotpeenEnd Item Identification: F100-PW-229; serd 7215
General Characteristics Item Description: This special tool seals off the area below the repair plane and extends outward and over the inlet case ourter diameter providing protection from the steel shot; consists of a steel ring having (3) press fit dowel pins that fit into the inlet case outer flange holes to locate the mask to case; used with PWA71102 fixture and PWA71105 mask
Overall Diameter: 46.000 inches nominal
United Technologies Corporation (77445)

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PWA71105 4920-01-424-1532Mask, ShotpeenSpecial Features: Inlet fan case, I.D.
Functional Description: Is required to protect the inlet fan assembly inner surface and airfoils during shotpeening of the repaired aft fairing surface
End Item Identification: Support equipment, F100-PWA-229 acft engine
United Technologies Corporation (77445)

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PWA71106 4920-01-423-2182Fixture, Engine Maintenance, AircrSpecial Features: Company item name-fixture, braze
Functional Description: Used to located and secure the inlet fan case and fitting (p/N 4067807 & 4067808) during reinstallation/used W/heat shield PWA71107
End Item Identification: F100-PW-229 engine
United Technologies Corporation (77445)

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PWA71108 4920-01-422-9635Test set, Aircraft EngineSpecial Features: Calibrate per T.O. 33K6-4-184-1 every 12 months
Functional Description: Pressure test tubes to verify overall integrity of the brazed tube assemblies
End Item Identification: F100-PW-100, 200, 220, 220E, 229 engines
United Technologies Corporation (77445)

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PWA 71110
PWA71110
4920-01-417-4459Mask, Plasma SpraySpecial Features: Used to properly mask the sixth stage disk and hub for application of PW53-69 (cuni) and PWA53-37 followed by PWA53-11 on the knife edge seals; serd no. 7221
End Item Identification: Support equipment, F100-PW-229 aircraft engine
Overall Diameter: 17.300 inches nominal
United Technologies Corporation (77445)

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PWA71111 4920-01-417-7718Fixture, Engine Maintenance, AircrSpecial Features: Characteristics length 19 inch; width 19 inch; height 24 inch; weight 118 lbs; articles requiring support is fscm 77445 & P/N 4070846
Functional Description: Used to hold and mask the 6TH stage compressor disk and hub assembly during plasma spray
End Item Identification: F100-PW-229 engine-asy turbofan
United Technologies Corporation (77445)

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PWA71112 4920-01-417-7715Mask, ShotpeenSpecial Features: C/O aluminum base & cover assembly, with locating bung hole & 4 hold down holes, an aluminum riser, a center post
Functional Description: Used to secure and mask the 6TH stage disk and hub when removing coating from the knife edge seals
End Item Identification: F100-PW-229 engine-asy turbofan
United Technologies Corporation (77445)

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PWA71113 4920-01-417-6040Holder, Maintenance Fixture, MultiSpecial Features: Used to set up the plasma spray parameters prior to spraying an engine part; sixth stage disk and hub compressor; test plate
End Item Identification: Support equipment, F100-PW-229 aircraft engine
Overall Height: 24.000 inches nominal
United Technologies Corporation (77445)

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PWA71114 4920-01-416-5713Holder, Test StripEnd Item Identification: F100-PW-229
Reference Data and Literature: Serd 7225
General Characteristics Item Description: Base plate machined dia thru center for locating on bung of plasma spray TABLE;2 sets of hold down holes are provided;one W/3 hole pattern and one W/4 hole pattern;recessed pocket W/bolt holes is machined in top of plate to locate and hold post assy which has 6 spacer plates and a sheet metal cover;container provided
United Technologies Corporation (77445)

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PWA71115 4920-01-416-8798Fixture, Machining, Aircraft EnginSpecial Features: Company item name-fixture machining, disk and hub compressor 6TH stage
Functional Description: Locate and clamp 6TH stage disk and hub assy in order to mill off damaged or bent tangs
End Item Identification: F100-PW-229
United Technologies Corporation (77445)

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PWA71116 4920-01-416-6230Fixture, Engine Maintenance, AircrSpecial Features: Bottom of plate has machined I.D.for locating on pedestal PWA70449
Functional Description: Properly locate the 6TH stage disk and hub assy during the shotpeening process prior to application of PWA53-69 (CU-N1)
End Item Identification: F100-PW-229
United Technologies Corporation (77445)

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PWA71117 4920-01-416-9627Holder, Test StripFunctional Description: Holder, test strip disk and hub compressor 6TH stage assy, intent of tool is to properly hold (2) test stripsto qualify the shotpeen process
End Item Identification: F100-PW-229
Reference Data and Literature: Serd no. 7228; T.O. 2J-F100-94
United Technologies Corporation (77445)

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PWA71118 4920-01-420-0217Mask, ShotpeenSpecial Features: Used to mask the sixth stage disk and hub in order to shotpeen the area prior to copper-nickel coating process; serd no. 7229
End Item Identification: Support equipment, F100-PW-229 aircraft engine
Overall Length: 3.500 inches nominal
United Technologies Corporation (52661,77445)

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