Aircraft and Missile Prime Movers Engine Fuel System Components: 49139, 4928925-511, 492897
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 49139 | 2915-00-858-8460 | Shaft Assembly, Thro | III End Item Identification: AH-1, UH-1, OV-1 turbine engine | Goodrich Corporation (11599) | |
| 49141 | 2915-00-708-2560 | Lever, Governor cam | Goodrich Corporation (11599) | ||
| 49142 | 2915-00-708-2561 | Lever, Spring Seat | Goodrich Corporation (11599) | ||
| 491420 | 2915-00-903-0721 | Fuel Control, Main, Turbine Engine | Reference Number Differentiating Characteristics: United aircraft corp pratt and whitney aircraft div source control dwg no. 491420 | United Technologies Corporation (77445) | |
| 49155 | 2915-00-775-7829 | Support, Gearshaft, Fuel Pump | III End Item Identification: Engine, acft, T53 General Characteristics Item Description: Bronze, high lead, promet 2S, FSCM96834, 0.540 in. min, 0.550 in. max O/a lg, 1.0925 in. min, 1.0928 in. min, flange od, 0.2970 in. min, 0.2995 in. max flange W, 0.7169 in. min, 0.7172 in. max body od | Goodrich Corporation (11599) | |
| 49163 | 2915-00-775-7827 | Support, Gearshaft, Fuel Pump | III End Item Identification: Engine, T53 General Characteristics Item Description: Bronze, leaded per chandler-evans spec CEPS111, 0.530 in. O/a lg, 1.0925 in. min, 1.0928 in. max flange W, 0.7169 in. min, 0.7172 in. max body od | Goodrich Corporation (11599) | |
| 491-947K 491947K | 2915-01-505-6699 | Valve, Fuel System | III End Item Identification: Super piper cub L21B | Piper Aircraft Inc. (77294) | |
| 49-199 49199 | 2915-00-049-3700 | Pin, Air Metering jet | General Characteristics Item Description: Steel, 1.219 in. O/a lg, 0.2585 in. min, 0.2595 in. max dia | Borg-Warner Corp. (96152) | |
| 492-009 492009 | 2915-01-502-5306 | Washer, Fuel Valve | III End Item Identification: L21B super piper cub | Piper Aircraft Inc. (77294) | |
| 492022 | 2915-01-495-5416 | Valve, Fuel Pressurizing and Drai | III End Item Identification: Super piper cub aircraft Special Features: E-z valve | Piper Aircraft Inc. (77294) | |
| 4920811-1 49208111 | 2915-01-103-9205 | Nozzle | Boeing Company, The (88277) | ||
| 49209 | 2915-00-673-0899 | Shaft, Pump Assembly, Water Inject | III End Item Identification: 43208090271 | Goodrich Corporation (11599) | |
| 492102 | 2915-00-987-3778 | Parts kit, Fuel Nozz | United Technologies Corporation (77445) | ||
| 4923T41P08 | 2915-01-576-4731 | Impeller, Pump, Centrifugal | III End Item Identification: TCT7-17 turboprop engine Special Features: 30 degree backsweep centrifugal compressor impeller;old part number 6071T86P03 | General Electric Company (99207) | |
| 49280 | 2915-00-873-8236 | Gage Assy, Fuel Nozz | General Motors Corp. (71934) | ||
| 492877 | 2915-00-942-5276 | Piston Assembly, Afterburner Igni | III End Item Identification: TF30-P-1 aircraft engine fuel control General Characteristics Item Description: Hardcoat and anodized finish, 1.6235 in. min to 1.6240 in. max O/a dia, 2 holes 0.060 in. min to 0.062 in. max dia on side, 3 holes 0.100 in. min to 0.110 in. max dia equally spaced thru sleeve, includes P/ns 492875, 492876 and AN150210 | United Technologies Corporation (77445) | |
| 492892 | 2915-00-942-5277 | Tube, Transfer, Packing, Fuel Contr | III End Item Identification: TF30-P-1 aircraft engine fuel control General Characteristics Item Description: Ams 4120 aluminum alloy, O/a dim. 0.370 in. min to 0.372 in. max dia by 0.600 in. min to 0.620 in. max lg, 0.183 in. min to 0.193 in. max inside dia, 2 grooves 0.095 in. min to 0.105 in. max W around side | United Technologies Corporation (77445) | |
| 4928925-509 4928925509 | 2915-01-105-3206 | Valve | Boeing Company, The (88277) | ||
| 4928925-511 4928925511 | 2915-01-105-3207 | Valve | Boeing Company, The (88277) | ||
| 492897 | 2915-00-942-5278 | Valve, Pressure, Afterburner Ignit | III End Item Identification: TF30-P-1 aircraft engine fuel control General Characteristics Item Description: Ams 5616 stainless steel W/rockwell-C 35 to 40 hardness, O/a dim. 0.665 in. min to 0.671 in. max dia by 0.478 in. min to 0.499 in. max lg, 0.100 in. min to 0.101 in. max dia by 0.128 in. min to 0.129 in. max lg middle section, 8 grooves equally spaced around each end on 0.560 in. min to 0.580 in. max dia surface | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) |