Hand Tools, Nonedged, Non-Powered: 17G110656-5, 17G120058-1, 17G130057-1
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
17G110656-5 17G1106565 | 5120-01-390-3247 | Jack, Hydraulic, hand | Special Features: C-17A support equipment; fixture, aircraft maintenance-draw bar | Boeing Company, The (88277) | |
17G110679-1 17G1106791 | 5120-01-615-9699 | Inserter and Remover, Spring | END Item Identification: C-17A support equipment Part Name Assigned BY Controlling Agency: Inserter and remover C-17A support equipment | Boeing Company, The (88277) | |
17G110813-1 17G1108131 | 5120-01-371-8024 | Tool set, Staking Bearing | General Characteristics Item Description: Used for staking bearings by deformation process prior to insertion. set contains two groove staking tools, fifteen 8-POINT staking tools, and 11 pilot tools | Boeing Company, The (88277) | |
17G110816-1 17G1108161 | 5120-01-371-1377 | Adapter set, Torque Wrench | Functional Description: To remove or install (6) six winglet spline bolts Supplementary Features: Place adapter over spline bolt to be removed (or installed) and attach A standard 1/2 inch drive wrench (or torque wrench) at the opposite end; spline bolts are now ready to be removed (or installed); case size: 30" L by 24" W by 6" h; WEIGHT:40.0 lbs approx; material: 4130 alloy steel Usage Design: C-17 aircraft is equipped with vortex diffusers | Boeing Company, The (88277) | |
17G110818-1 17G1108181 | 5120-01-381-1176 | Compressor, Spring | Special Features: Body is carbon steel with boss area and forked tines two 1/2 section brackets with threaded rod attached to one bracket and hex nut, also used as rigging aide for cargo latch fittings END Item Identification: C-17 aircraft Functional Description: Used to compress the helical spring to remove the spring guide link ramp assy and replace spring | Boeing Company, The (88277) | |
17G110826-1 17G1108261 | 5120-01-390-7243 | Adapter, Torque Wrench | END Item Identification: C117 troop entry door Functional Description: 6USED to tighten or loosen the spring adjustment shaft located on the counterbalance until the correct torque is applied and locking devices engaged. constructed of steel, 1/2 inch drive, height 5 inches, width 5 inches, depth 5 inches, weight 2 lbs. | Boeing Company, The (88277) | |
17G110836-1 17G1108361 | 5120-01-398-0044 | Inserter and Remover set, Bearing | Special Features: Contains all necessary staking and pilot tools housed in one foam-lined case; size: 25IN X 25IN X 10IN; weight: 35 lbs; color: case, gray no 16473 END Item Identification: C-17 aircraft Functional Description: To remove, install, and stake bearings by multi-point and groove or roller staking methods | Boeing Company, The (88277) | |
17G110847-1 17G1108471 | 5120-01-407-8733 | Inserter and Remover, Spring | Special Features: Consists of three items;an 11 in rod having A 7/8 in octagon head at one end and 4 in of 5/8 in course threadat the oter;a flat plate grooved to fit the spring with thru holr to accept rod;a flat plate grooved to fit springwith 5/8 in thread to accept rod END Item Identification: C-17 Functional Description: Used to remove two hatch damper springs which have to be removed prior to removing the bolts that retain the hatch hinges | Boeing Company, The (88277) | |
17G110874-1 17G1108741 | 5120-01-415-4495 | Clamp, C | Special Features: Dim.: 10 in. lg, 2.0 in. W, 2 in.h; matl: steel END Item Identification: C-17 acft Functional Description: Used during installation of troopdoors to temporarily secure the left and right troop doors in the aft fuselage door cutout area for final rigging | Boeing Company, The (88277) | |
17G110910-1 17G1109101 | 5120-01-418-6981 | Wrench, Spanner | Special Features: Length 50 inches, capacity 3.750 inches Style Designator: Face hole Overall Width: 2.000 inches nominal | Boeing Company, The (88277) | |
17G110910-501 17G110910501 | 5120-01-458-4544 | Wrench, Spanner | Special Features: Used to load or unload the counterbalance spring tension while rigging the crew door; size: 50L X 2W X 3H inches; 8 lbs; steel; passivated finish; operating temp: -40 to +125 deg f; wrench is A fixed hook type, one piece spanner wrench; hook will interface with the slots on the torsion spring flange pn 17P1A4429; capacity: 3.750 in dia; 4 ft handle section END Item Identification: C-17 aircraft | Boeing Company, The (88277) | |
17G110966-1 17G1109661 | 5120-01-423-5624 | Wrench set, Combination box and O | Special Features: Wrench set, used to hold the cargodoor hook nuts during installation/removal of the cargo door HOOKS/28SPLINE Component Quantity: 3 Usage Design: Wrench set cargo door hooks | Boeing Company, The (88277) | |
17G120058-1 17G1200581 | 5120-01-384-7539 | Tool set, Vra Calabration | Special Features: Operation: bolt the retainer to the vra; install the vra int the holding fixture; insert driver trough retainer and into 17P2G1044 screw; perform calibration procedure, using the driverto turn the screw; remove vra from holding fixture; remove retainer fr vra END Item Identification: C-17 aircraft, aerial delivery system General Characteristics Item Description: Tool kit is in two parts; retainer (adapter) - size is 1.3 in. by 1.3 in. by 0.4 in. thick, square in shape, with threaded center hole for socket, socket wrench style driver; driver (socket, socket wrench) - size is 1 in. dia. by 2 in. length, threaded end is enternal involute spline per ansi B92.1-1970, socket end is 1/4 - drive femaleper ansi B107.4-1982 | Boeing Company, The (88277) | |
17G130003-1 17G1300031 | 5120-01-244-1248 | Wrench, Spanner | END Item Identification: C-17 acft | Amro Fabricating Corporation (8V199) Boeing Company, The (88277) Protonics Engineering Corp. (62684) | |
17G130045-1 17G1300451 | 5120-01-297-3646 | Adapter, Torque Wrench | Overall Length: 4.000 inches nominal Style Designator: Socket to socket Functional Description: Used to replace internal seals 0F shock strut assembly on the C-17 aircraft nose landing gear | Boeing Company, The (88277) | |
17G130046-1 17G1300461 | 5120-01-297-3647 | Adapter, Torque Wrench | Overall Length: 3.000 inches nominal Style Designator: Socket to socket Functional Description: For repair or replacement of internal support tube P/N 17P1C2020-1/C-17 aircraft | Boeing Company, The (88277) | |
17G130047-1 17G1300471 | 5120-01-298-5652 | Adapter, Torque Wrench | Material: Steel overall Overall Length: 2.000 inches nominal Style Designator: Socket to socket | Boeing Company, The (88277) | |
17G130048-1 17G1300481 | 5120-01-299-1092 | Adapter, Torque Wrench | Wrenching Surface Shape: Spline single end internal Functional Description: For shock strut dissambly in order to replace SEALS/C17 acft Wrenching Surface Flute Quantity: 4 | Boeing Company, The (88277) | |
17G130049-1 17G1300491 | 5120-01-298-5653 | Adapter, Torque Wrench | Overall Length: 2.600 inches nominal Style Designator: Socket to socket Functional Description: Used during repair of piston assembly of the shock strut assembly on the nose landing gear on C17 acft | Boeing Company, The (88277) | |
17G130057-1 17G1300571 | 5120-01-298-7521 | Adapter, Torque Wrench | Overall Length: 27.500 inches nominal Style Designator: Socket to socket Functional Description: Used to rmove and install nut assembly on shock strut on landing gear (front) on C17 acft | Boeing Company, The (88277) |