Triumph Actuation Systems NSN Parts
| CAGE | Address | Type | Status |
|---|---|---|---|
| 1QC67 | 175 ADDISON RD, WINDSOR, CT, 06095-2178, UNITED STATES | A | A |
| 33068 | 175 ADDISON RD, WINDSOR, CT, 06095-2178, UNITED STATES | A | A |
| 33UN4 | 22922 NE ALDER CREST DR, REDMOND, WA, 98053-5894, UNITED STATES | A | A |
| 57850 | 1395 BLUE HILLS AVE, BLOOMFIELD, CT, 06002-1309, UNITED STATES | A | C |
FSC 1560 Airframe Structural Components
| MFG SKU | NSN | Item Name | Details | CAGE Code | RFQ |
|---|---|---|---|---|---|
| 0AS5451-15 0AS545115 | 1560-01-345-7321 | Strut, Aircraft | Special Features: Used on the nose landing gear End Item Identification: Merlin 111A acft | 33068 | |
| 0AS5453-105 0AS5453105 | 1560-01-483-3523 | Strut, Aircraft | 33068 | ||
| 0AS5453-5 0AS54535 | 1560-01-345-7322 | Strut, Aircraft | Special Features: Used on the nose landing gear End Item Identification: Merlin 111A acft | 33068 |
FSC 1615 Helicopter Rotor Blades, Drive Mechanisms and Components
| MFG SKU | NSN | Item Name | Details | CAGE Code | RFQ |
|---|---|---|---|---|---|
| 114H6824-1 114H68241 | 1615-00-021-2720 | End Cover, Shock Absorber | General Characteristics Item Description: Phosphor bronze astm B139-5B comp a or QQ-B-750 comp a temper hard, dim., 3.615 in. min, 3.616 in. max left end flange od, 0.501 in. nom flange lg, 3.114 in. min, 3.115 in. max right end body od, 0.552 in. nom body lg, 1.365 in. nom O/a lg, 1.937 in. nom left end body od, 0.312 in. nom left end body lg, 1.2490 in. min, 1.2495 in. max td, 1.636 in. nom left end counterbore dia.by 0.156 in. deep, left end flange center-grooved 0.188 in. W by 3.375 in. nom dia, right end body center-grooved 0.225 in. W by 2.875 in. nom dia, nine holes on right face 0.375 in. dia by 0.680 in. deep equally spaced on 2.250 in. bolt circle dia, item used as end cover for blade lag shock absorber | 33068 | |
| 114H6821-1 114H68211 | 1615-00-069-3299 | Sleeve, Cylinder | General Characteristics Item Description: Aluminum alloy QQ-A-200/2 comp 2014-T6, chromium-plated id QQ-C-320 class 2, chemical film MIL-C-5541 type 2 class 1 grade C all other surfaces, dim., 5.812 in. nom lg, 3.373 in. min, 3.375 in. max od, 3.608 in. min, 3.616 in. max flange od, 0.438 in. lg left flange W, 0.847 in. lg center flange W, 0.531 in. lg right flange W, 0.225 in. flange W by 3.375 in. dia W/one grooveper left and right flanges and two grooves on center flange, twelve holes 0.081 in. dia equally spaced 1.185 in.from left end W/2ND row of twelve holes 0.209 in. distance between centers offset 15.0 deg, similar set of twelve holes 0.633 in. from right end, sleeve used on blade lag shock absorber | 33068 |
FSC 1620 Aircraft Landing Gear Components
| MFG SKU | NSN | Item Name | Details | CAGE Code | RFQ |
|---|---|---|---|---|---|
| 0MP2826-62 0MP282662 | 1620-00-941-0812 | Actuator, Hyd Assy | General Characteristics Item Description: Consists of 1 each housing; 1 ea piston; 1 ea bearing, plain, rod end; 1 ea shaft; 1 ea swivel, joint, hydraulic; 1 ea cover, housing; 2 ea ring, externally threaded; 1 ea cylinder, balancing; 1 ea plate, identification; 1 ea lock, shaft, swivel; 2 ea pin, grooved, headless; 2 ea lock, bushing, sleeve; 1 ea nut, drilled jam; 1 ea lock-rod end; 2 ea ring, retaining, internal; 1 ea scraper, hydraulic piston rod; 1 ea pin-spring, cres; 22 ea ring, packing backup; 11 ea packing, preformed, hydraulic; 1 ea filter, hydraulic air vent; as required, wire, lock and felt strip, packing gland End Item Identification: Acft nose landing gear | 33068 | |
| 70250-13164-102 7025013164102 | 1620-01-114-6135 | Adapter, Tail Landin | 33068 | ||
| 70250-13164-104 7025013164104 | 1620-01-114-6135 | Adapter, Tail Landin | 33068 | ||
| 14-41642-1 14416421 | 1620-00-008-6418 | Arm, Torque, Landing Gear | General Characteristics Item Description: Steel, 14.200 in. O/a lg, 6.551 in. min to 6.561 in. max O/a W, machined surfaces 32 to 125 microinch finish, heat treat 180000 to 200000 FSC Application Data: Landing gear, retractable | 33068 | |
| 3863046-1 38630461 | 1620-00-162-0242 | Arm, Valve, Steering | General Characteristics Item Description: Aluminum alloy, 1.855 in. lg, 0.820 in. W, 0.500 in. thk | 33068 | |
| 65265-02026-101 6526502026101 | 1620-01-150-7064 | Axle, Landing Gear | Overall Length: 23.924 inches nominal Aircraft for Which Designed: Helicopter model CH-53E Basic Material: Steel | 33068 | |
| S6125-50509 S612550509 | 1620-00-700-1648 | Axle, Landing Gear | Special Features: Offset with dia. 1.4995 after plating | 33068 | |
| 4091004-1 40910041 | 1620-01-161-8356 | Bolt Assembly, Special | End Item Identification: Helicopter model SH-60B | 33068 | |
| 348503-3 3485033 | 1620-00-242-0657 | Button, Spring Guide | General Characteristics Item Description: Cres, QQ-S-763 clas 440C, passivated, 0.355 in. O/a lg, 0.275 in.min. 0.280 in. max O/a dia, heat treat rockwell C54.0 to C58.0, 125MICROINCH finish all surfaces FSC Application Data: Hydraulic steering valve, acft | 33068 | |
| 220217-2 2202172 | 1620-00-908-9998 | Cage, Gear, Power Ste | 33068 | ||
| 3817002-3 38170023 | 1620-00-591-8509 | Cage, Gear, Power Ste | End Item Identification: C-5 aircraft | 33068 | |
| 4202011-3 42020113 | 1620-01-116-8551 | Carrier Assembly, Gear | General Characteristics Item Description: 3.300 in. 0/A lg, 3.080 in. max O/a dia End Item Identification: Aircraft model F-18 | 33068 | |
| 220208-3 2202083 | 1620-00-740-1543 | Collar and Gear Ass | 33068 | ||
| 6-41633-1 6416331 | 1620-00-011-0282 | Collar, Upper Torque | General Characteristics Item Description: Steel forging 4140, 1.190 in.W, 3.074 in.min 3.075 in. max inside dia End Item Identification: T-38 acft Reference Data and Literature: T.0. 4S2-61-4 | 33068 | |
| 14-41611-501 1441611501 | 1620-00-007-1787 | Collar, Upper, Torque arm, Landing | General Characteristics Item Description: Steel nai 1273 grade B 4340, 7.240 in. O/a lg, 5.748 in. min 5.750IN. max O/a W, 2.310 in. min 2.320 in. max O/a H, noted machinedsurfaces 32 63 125 microinch finish, nickel plate class 20.0004-0.00006 thk, heat treat 180000 to 200000 psi, component 2BUSHING no. 14-41685-21 End Item Identification: F-5E/F aircraft Reference Data and Literature: T.O.4S2-75-4 | 33068 |
