Helicopter Rotor Blades, Drive Mechanisms and Components: 114R1504-12, 114R1529-1, 114R1702-37
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 114R1504-12 114R150412 | 1615-00-040-8232 | Fairing Assembly, in | The Boeing Company (77272) | ||
| 114R1504-14 114R150414 | 1615-00-040-8232 | Fairing Assembly, in | The Boeing Company (77272) | ||
| 114R1505-23 114R150523 | 1615-00-040-8118 | Fairing Assembly, Ro | The Boeing Company (77272) | ||
| 114R1505-31 114R150531 | 1615-00-040-8118 | Fairing Assembly, Ro | The Boeing Company (77272) | ||
| 114R1522-3 114R15223 | 1615-00-131-2012 | Washer, Anchor Fitting | General Characteristics Item Description: Cres, MIL-S-5059 comp aise 301 cond 1/4 hard, dim., 2.122 in. nom lg, 1.240 in. nom W at 0.477 in. dia hole, 0.025 in. nom thick, sides taperedw/one end rounded by 0.310 in. radius and opposite end rounded by 0.620 in.radius, one hole 0.475 in. min, 0.479 in. max dia drilled on verticalcenterline 0.620 in. from bottom and dimpled W/90 deg total angle, one holedrilled and dimpled for MS20427-M4 rivet 0.310 in. from top W/1.192 in.center to center distance between holes, washer bent 0.812 in. from top ofnarrow end to form 170 deg angle | The Boeing Company (77272) | |
| 114R1528 | 1615-01-019-3040 | Backing Plate, Bulkhead | Special Features: 2 nipples 0.312UNF-2A thds Material: Aluminum alloy Overall Length: 2.300 inches nominal | The Boeing Company (77272) | |
| 114R1528-1 114R15281 | 1615-01-019-3040 | Backing Plate, Bulkhead | Special Features: 2 nipples 0.312UNF-2A thds Material: Aluminum alloy Overall Length: 2.300 inches nominal | The Boeing Company (77272) | |
| 114R1529-1 114R15291 | 1615-01-019-3039 | Wedge, Bulkhead | The Boeing Company (77272) | ||
| 114R1560-5 114R15605 | 1615-00-181-3998 | Weight, Droop Snoot | The Boeing Company (77272) | ||
| 114R1560-7 114R15607 | 1615-00-181-4017 | Weight, Droop, Snoot | The Boeing Company (77272) | ||
| 114R1570-2 114R15702 | 1615-00-181-3989 | Nose cap, Blade, Rota | The Boeing Company (77272) | ||
| 114R1572-17 114R157217 | 1615-00-731-5265 | Cover, Tip, Rotary Wi | The Boeing Company (77272) | ||
| 114R1572-18 114R157218 | 1615-00-922-5807 | Cover, Tip, Rotary Wi | The Boeing Company (77272) | ||
| 114R1574-1 114R15741 | 1615-00-008-3275 | Mount, Indicator | The Boeing Company (77272) | ||
| 114R1586-1 114R15861 | 1615-00-891-8371 | Weight, Rotary Wing Blade | General Characteristics Item Description: Steel, MIL-T-21014 type 2, dim., 1.335 in. min, 1.365 in. max square, 0.085 in. min, 0.115 in. thk, ends rounded by 0.120 in. radius, two holes 0.401 in. min, 0.411 in. max dia W/centers on vertical centerline 0.300 in. from edge and 0.750 in. between centers | The Boeing Company (77272) | |
| 114R1591-14 114R159114 | 1615-00-181-3991 | Fitting Balance Sup | The Boeing Company (77272) | ||
| 114R1701/2 114R17012 | 1615-01-342-7950 | Strip, Erosion, Blade | Special Features: Used on a chinook helicopter | The Boeing Company (77272) | |
| 114R1702-21 114R170221 | 1615-01-087-4289 | Blade, Rotary Wing | III End Item Identification: Helicopter, cargo transport 47C | The Boeing Company (77272) | |
| 114R1702-22 114R170222 | 1615-01-082-8194 | Blade, Rotary Wing | III End Item Identification: Helicopter, cargo, model CH-47 | The Boeing Company (77272) | |
| 114R1702-37 114R170237 | 1615-01-145-7109 | Blade, Rotary Wing | III End Item Identification: CH-47 series helicopters Special Features: Made of figerglass;test data DOCUMENT:C77272-114R1702 | The Boeing Company (77272) |