Aircraft Maintenance and Repair Shop Specialized Equipment: 2C6860G07, 2C7455G02, 2D04282G01
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2C6860G07 | 4920-01-247-8119 | Fixture, Aircraft Maintenance | Functional Description: Vertically supports the high pressure turbine rotor by the control datums during assy for inspection and runout at each step also measures concentricities and perpendicularities End Item Identification: TF39-GE-1C acft engine age | General Electric Company (07482) | |
| 2C6925G03 | 4920-01-559-3512 | Fixture, Engine Maintenance, Aircr | Special Features: Consists of rectangular base plate with a rod at one end, a pin to hold the clevis, and adjustable pin to fit the spherical rod end bearing. black oxide finish Functional Description: Used to set and measure variable stator vane clevis assemblies at their proper installation depth End Item Identification: C-5 aircraft engine CF6-80C2L1F | General Electric Company (07482) | |
| 2C6962G05 | 4920-01-518-4027 | Fixture, Engine Maintenance, Aircr | Functional Description: Used to check for bent variable stator vane(vsv) lever arms on an on-wing engine to determine whether they are bent beyond limits End Item Identification: CF6-80C2L1F ge engines Reference Data and Literature: Serd no. 03-01-0050 | General Electric Company (07482) | |
| 2C6966G07 | 4920-01-518-0861 | Fixture, Engine Maintenance, Aircr | Functional Description: Checks vane actuation arms for distortion or bending End Item Identification: CF6-80C2L1F ge engines Reference Data and Literature: Serd no. 03-01-0051 | General Electric Company (07482) | |
| 2C6967G07 | 4920-01-122-2723 | Tool, Rotor Blade | General Electric Company (07482) | ||
| 2C7042G04 | 4920-01-257-9386 | Fixture, Aircraft Maintenance | Special Features: C/O a rabbeted base plate with a central thd hub which supports a height adjustable plate into which is mtd adjustment screws to round up-support the stator case in the area of the vane slot being reworked Functional Description: Used to restrain the compressor rear case to facilitate repair of worn vane slots End Item Identification: TF39-GE-1C acft engine | General Electric Company (07482) | |
| 2C7334G03 | 4920-01-045-6166 | Fixture, Aircraft Maintenance | Special Features: C/O 12 hardwood segments, outer restraining ring, attached hardware to function W/1C6790G01 hydraulic expander End Item Identification: C5 acft agge. | General Electric Company (07482) | |
| 2C7455G02 | 4920-01-246-9028 | Fixture, Aircraft Maintenance | Special Features: C/O reversible rabbet plate W/adjustable screw pads Functional Description: Used to machine the replaced flange to required contour after it has been welded in place End Item Identification: TF39 engine age. | General Electric Company (07482) | |
| 2C7546G09 | 4920-01-248-3486 | Fixture, Aircraft Maintenance | Special Features: C/O rigid frame and cabinet; motor driven abrasive wheel; 6 guide rollers, cam, and titanium ignitor assy Functional Description: Required when recontouring fan blade leading edge End Item Identification: KC-135R acft age | CFM International Inc. (58828) | |
| 2C7758G01 | 4920-01-116-6822 | Fixture, Aircraft Maintenance | Functional Description: Used to remove worn mounting pin bushings in TF39-1C engine combustor cowl End Item Identification: TF39-1C engine | General Electric Company (07482) | |
| 2C7785 | 4920-01-247-2178 | Fixture, Aircraft Maintenance | Functional Description: Used for thermal sizing of compressor front case for repair of the oversize rabbet, correct distortion from weld repair and improve case roundness End Item Identification: TF-39 engine | General Electric Company (07482) | |
| 2C7785G01 | 4920-01-237-4469 | Fixture, Aircraft Maintenance | Special Features: C/O 1 base P/N 2C7785P02; 2 retaining rings P/N 2C7785P03; 4 thermocouple bolts P/N 2C7785P06; 1 shoulder eye bolt P/N 18506; misc hardware CYAGJA41.500 Functional Description: To thermally round-up and resize the compressor stator front case End Item Identification: TF39 acft engine age | General Electric Company (07482) | |
| 2C8016G02 | 4920-01-531-6719 | Fixture, Engine Maintenance, Aircr | End Item Identification: C5M aircraft engine Part Name Assigned BY Controlling Agency: C5M gage, stage 5/6 variable stator | General Electric Company (03350,07482) Rhinestahl Corporation (5QE71) | |
| 2C8042G06 | 4920-01-118-5127 | Tool set, Wedging Compressor Roto | End Item Identification: TF39 engine General Characteristics Item Description: Titanium bladed, stage 3 to 16 Part Name Assigned BY Controlling Agency: Wedging compressor rotor blade tool set | General Electric Company (07482) | |
| 2C8043G02 | 4920-01-531-1387 | Maintenance kit, Aircraft | Special Features: Critical C5M acft usage Functional Description: Used to clean the engine compressor on wing End Item Identification: C5M acft | General Electric Company (07482) | |
| 2C8072G02 | 4920-01-120-1597 | Tester, Carbon Seal | End Item Identification: CF-6 engine, E-4B acft age. | Ametek Inc. (97424) | |
| 2C8073G05 | 4920-01-520-3853 | Fixture, Engine Maintenance, Aircr | End Item Identification: C-5 engine maintence | General Electric Company (07482) | |
| 2C90536G02 | 4920-01-521-1954 | Adapter set, Aircraft Maintenance | End Item Identification: CT7 aircraft engine Part Name Assigned BY Controlling Agency: Adapter set | General Electric Company (07482) | |
| 2CF18730 | 4920-00-626-5795 | Fixture, Aircraft Maintenance | Fairchild Controls Corporation (01359) | ||
| 2D04282G01 | 4920-01-212-8776 | Fixture, Aircraft Maintenance | Northrop Grumman Systems Corporation (18323) |