Aircraft Maintenance and Repair Shop Specialized Equipment: PWA-71097, PWA71100, PWA71118
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
PWA-71097 PWA71097 | 4920-01-393-0231 | Mask, Shotpeen | Functional 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) | |
PWA71098 | 4920-01-422-1650 | Fixture, Engine Maintenance, Aircr | Special 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) | |
PWA71099 | 4920-01-421-9731 | Fixture, Machining, Aircraft Engin | Special 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) | |
PWA71100 | 4920-01-421-8179 | Fixture, Engine Maintenance, Aircr | Special 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) | |
PWA71101 | 4920-01-425-4656 | Fixture, Engine Maintenance, Aircr | Special 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) | |
PWA 71102 PWA71102 | 4920-01-422-9106 | Fixture, Engine Maintenance, Aircr | Functional 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) | |
PWA 71103 PWA71103 | 4920-01-424-7963 | Holder, Test Strip | End 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) | |
PWA 71104 PWA71104 | 4920-01-424-2483 | Mask, Shotpeen | End 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) | |
PWA71105 | 4920-01-424-1532 | Mask, Shotpeen | Special 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) | |
PWA71106 | 4920-01-423-2182 | Fixture, Engine Maintenance, Aircr | Special 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) | |
PWA71108 | 4920-01-422-9635 | Test set, Aircraft Engine | Special 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) | |
PWA 71110 PWA71110 | 4920-01-417-4459 | Mask, Plasma Spray | Special 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) | |
PWA71111 | 4920-01-417-7718 | Fixture, Engine Maintenance, Aircr | Special 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) | |
PWA71112 | 4920-01-417-7715 | Mask, Shotpeen | Special 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) | |
PWA71113 | 4920-01-417-6040 | Holder, Maintenance Fixture, Multi | Special 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) | |
PWA71114 | 4920-01-416-5713 | Holder, Test Strip | End 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) | |
PWA71115 | 4920-01-416-8798 | Fixture, Machining, Aircraft Engin | Special 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) | |
PWA71116 | 4920-01-416-6230 | Fixture, Engine Maintenance, Aircr | Special 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) | |
PWA71117 | 4920-01-416-9627 | Holder, Test Strip | Functional 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) | |
PWA71118 | 4920-01-420-0217 | Mask, Shotpeen | Special 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) |