Helicopter Rotor Blades, Drive Mechanisms and Components: M61719-1, MMT61A034, MTA4201285-003
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| M61719-1 M617191 | 1615-01-421-0634 | Tube, Runout | III End Item Identification: 1520-01-106-9519 | Transdigm Inc. (04638) | |
| M61719-2 M617192 | 1615-01-421-6490 | Tube, Run out | III End Item Identification: 1520011069519, helicopter, apache AH-64. | Transdigm Inc. (04638) | |
| M80873 | 1615-01-421-0634 | Tube, Runout | III End Item Identification: 1520-01-106-9519 | Transdigm Inc. (04638) | |
| M80873 ITEM 7 M80873ITEM7 | 1615-01-421-0634 | Tube, Runout | III End Item Identification: 1520-01-106-9519 | Transdigm Inc. (04638) | |
| MB8667MB | 1615-01-525-4048 | Protector, Rotor Blade | III End Item Identification: H53 rotor BLADE;65170-11001-ALL Special Features: Protective tape 8667HS a simple easy and fast method of protecting a surface from corrossion, abrasion, erosion and minor impact damage; is a long-aging, solvent resistant, high sheer (hs) presure sensitive acrylic self adhesive that is protected with an easy-release plastic split-slit LINER;0.025 inch (0.63MM) backing; 0.003 inch (0.08MM) adhesive; III Part Name Assigned By Controlling Agency: Inavy:poly tape blade | 3M Co. (52152) | |
| MC4052-2 MC40522 | 1615-00-938-9994 | Coupling set | Ameridrives International LP (70487) | ||
| MIL-C-5541 MILC5541 | 1615-00-841-0722 | Clip, Oil Filter, Transmission | III End Item Identification: Bell helicopter models UH-1N, UH-1H, AH-1S, HH-1H General Characteristics Item Description: Aluminum alloy QQ-A-362 comp 2024-T3, surface treatment chemical film bps FW4182, shape, right angle, dim., 2.100 in. lg, 0.580 in. W, 1.000 in. ht, two rivet holes on top for MS20470AD4 rivetslocated 0.190 in. from left and right ends and 0.190 in. from back edge, lower left corner of top cut out 0.380 in.lg by 0.200 in. W, vertical lg 1.720 in. lg W/lower right section removed 1.120 in. lg by 0.540 in. W, upper right end chamfered 45.0 deg by 0.320 in. lg, right angle inner angle rounded by 0.160 in. radius, item used on oil filtermounting bracket | Military Specifications (81349) | |
| MIL-S-18729 MILS18729 | 1615-01-089-4435 | Plate, Locking, Gearbox | Military Specifications (81349) | ||
| MMR 009745 MMR009745 | 1615-01-506-5683 | Chafing Strip | III End Item Identification: Model 369-MD500, helicopter | MD Helicopters Inc. (1KVX4) | |
| MMT61A034 | 1615-00-589-8443 | Guide Shaft, Tail Ro | Consolidated Tool and Manufacturing (13184) | ||
| MODELE3597 | 1615-01-089-8578 | Chart, Corrector | Eurocopter France ETS DE Marignane (F0210) | ||
| MRH19-206-3 MRH192063 | 1615-00-217-6854 | Shield, Stationary Star | General Characteristics Item Description: Aluminum; 7.812 in. id, 8.625 in.od; 6 0.562 in. holes equally spaced; 6 jig drill nr 5(.2055) holes equally spaced | Hardman Aircraft Inc. (83115) | |
| MRX2 | 1615-00-970-1262 | Trunnion Assembly, Swashplate | General Characteristics Item Description: Steel, comp 52100 inner and outer race and rollers, steel, comp 9310 or 3312 rod end and housing, beryllium copper retainer, core rockwell hardnessrating C scale 35 to 40, casehardened outer race of shank, inner race of eye and rod end rockwell hardness C scale 60 min, cadmium-plated QQ-P-416 cl 2 TY1 exposed surfaces, dim., 2.850 in. max O/a lg, 1.559 in. min, 1.564 in. max housing lg, 2.260 in. max lg bore- center to housing end, 1.2495 in. min, 1.2500 in. max housing od, 1.140 in. min, 1.180 in. max rod end od, 0.3119 in. min, 0.3122 in. max rod end id, 0.750 in. min, 0.765 in. max outer member W, 0.872 in. min, 0.875 in. max inner member W, tapered roller bearing data, rbec 2 tolerance, 0.0005 in. tightto 0.0005 in. loose internal radial clearance, 13 rollers 0.210 in. lg, 33 short rollers 0.150 in. lg, rod end fitted W/2 shafer G3 grease fittings and bearing prelubricated MIL-G-25537 grease, housing drilled thru W/two holes 0.155 in. min, 0.161 in. max dia 180 deg apart 0.790 in. nom from housing end, | Rexnord Industries LLC (77896) | |
| MSP1219 | 1615-00-767-7997 | Counterweight, Main Rotor | General Characteristics Item Description: Steel, QQ-S-633 comp sae 1010 or 1018 or 1020 or 1025 or 1112, 30000 psi min tensile strength, dim., 3.187 in. nom od, 0.374 in. min, 0.381 in. max id, 1.000 in. nom lg, one side counterbored 0.890 in. dia by 0.320 in. deep, max surface finish, all surfaces 125 microinches aa, machined surfaces or centerlines flat, square or parallel within 0.001 in. and/or concentric to 0.010 tir | Machinery Spare Parts And (17854) | |
| MTA4201219-501 MTA4201219501 | 1615-01-388-5684 | Shoe and Liner Assy | III End Item Identification: MH-53J aircraft III Fsc Application Data: Helicopter rotor blades, drive mechanisms an components | Israel Aircraft Industries LTD (S6092) | |
| MTA4201281-101 MTA4201281101 | 1615-01-355-6006 | Shoe Assy, Clutch | III End Item Identification: H-53 General Characteristics Item Description: Improved a.P.P.(wet) clutch, shoe and shank without bonded lining III Fsc Application Data: Helicopter rotor and components | Israel Aircraft Industries LTD (S6092) | |
| MTA4201282-301 MTA4201282301 | 1615-01-282-2919 | Drum Assembly, Clutch | III Fsc Application Data: H-53 helicopter | Israel Aircraft Industries LTD (S6092) | |
| MTA4201283-001 MTA4201283001 | 1615-01-282-2920 | Drum Cover, Clutch | III Fsc Application Data: H-53 helicopter | Israel Aerospace Industries Bedex (SD664) Israel Aircraft Industries LTD (S6092) | |
| MTA4201284-501 MTA4201284501 | 1615-01-282-2918 | Disc Driving Assembly | III Fsc Application Data: H-53 helicopter | Israel Aircraft Industries LTD (S6092) | |
| MTA4201285-003 MTA4201285003 | 1615-01-282-2926 | Plate, Seal | III Fsc Application Data: H-53 helicopter | Israel Aircraft Industries LTD (S6092) |