Aircraft and Missile Prime Movers Engine Fuel System Components: 02-14844, 02-14881, 02-14987
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 02-14844 0214844 | 2915-00-940-9405 | Body, Bearing, Fuel Pump | General Characteristics Item Description: Material bar cast W/30 percent lead bronze, lead indium plated, O/a dim. 1.9985 in. min to 1.9990 in. max dia by 1.125 in. min to 1.130 in. max lg, inside dim. 0.967 in. min to 0.977 in. max dia by 0.125 in. min to 0.130 in. max deep and 0.8766 in. min to 0.8771 in. max dia by 0.100 in. deep, front flange W/3 holes 0.188 in. dia by 0.030 in. min to 0.040 in. max deep, 2 grooves 0.062 in. W and 0.016 in. W by 0.005 in. min to 0.010 in. max deep, cutter 1.000 in. dia, left SIDEAGAVG43205086151 | Hamilton Sundstrand Corporation (99167) | |
| 02-14845 0214845 | 2915-00-940-9402 | Body, Bearing, Fuel Pump | III End Item Identification: 43205086151 General Characteristics Item Description: Material bar cast W/30 percent lead bronze, lead indium plated, O/a dim. 1.9985 in. min to 1.9990 in. max dia by 1.234 in. min to 1.239 in. max lg, inside dim. 0.967 in. min to 0.977 in. max dia by 0.125 in. min to 0.130 in. max deep and 0.8766 in. min to 0.8771 in. max dia by 1.109 in. deep, front flange W/3 holes 0.188 in. dia by 0.030 in. min to 0.040 in. max deep, 2 grooves 0.062 in. W and 0.016 in. W by 0.005 in. min to 0.010 in. max deep, cutter 1.000 in. dia, left side | Hamilton Sundstrand Corporation (99167) | |
| 02-14846 0214846 | 2915-00-940-9404 | Cover, Bearing, Fuel Pump | III End Item Identification: 43205086151 General Characteristics Item Description: Material bar cast W/30 percent lead bronze, lead indium plated, O/a dim. 1.9985 in. min to 1.9990 in. max dia by 1.234 in. min to 1.239 in. max deep, inside dim. 0.967 in. min to 0.977 in. max dia by 0.125 in. min to 0.130 in. max deep and 0.8760 in. min to 0.8767 in. max dia by 1.109 in. deep, front flange W/3 holes 0.188 in. dia by 0.030 in. min to 0.040 in. max deep, 2 grooves 0.063 in. W by 0.047 in. deep and 0.016 in. W by 0.005 in. min to 0.010 in. max deep, mtg flange W/5 holes, 0.219 in. dia by 0.336 in. min to 0.341 in. max deep, cutter 1.000 in. dia, right side, groove on side 0.180 in. min to 0.190 in. max W | Hamilton Sundstrand Corporation (99167) | |
| 02-14847 0214847 | 2915-00-940-9403 | Cover, Bearing, Fuel Pump | III End Item Identification: 43205086151 General Characteristics Item Description: Material bar cast W/30 percent lead bronze, lead indium plated, O/a dim 1.9985 in. min to 1.9990 in. max dia by 1.234 in. min to 1.239 in. max deep, inside dim. 0.967 in. min to 0.977 in. max dia by 0.125 in. min to 0.130 in. max deep and 0.8760 in. min to 0.8767 in max dia by 1.109 in. deep, front flange W/3 holes 0.188 in. dia by 0.030 in. min to 0.040 in. max deep, 2 grooves 0.063 in. W by 0.047 in. deep and 0.016 in. W by 0.005 in. min to 0.010 in. max deep, mtg flange W/5 holes, 0.219 in. dia by 0.336 in. min to 0.341 in. max deep, cutter 1.000 in. dia, right side, groove on side 0.180 in. min to 0.190 in. max W | Hamilton Sundstrand Corporation (99167) | |
| 02-14848 0214848 | 2915-00-940-9401 | Body, Bearing, Fuel Pump | III End Item Identification: 43205086151 General Characteristics Item Description: Material bar cast W/30 percent lead bronze, lead indium plated, O/a dim. 1.9985 in. min to 1.9990 in. max dia by 1.234 in. min to 1.239 in. max lg, inside dim. 0.967 in. min to 0.977 in. max dia by 0.125 in. min to 0.130 in. max deep and 0.8760 in. min to 0.8767 in. max dia by 1.109 in. deep, front flange W/3 holes 0.188 in. dia by 0.030 in. min to 0.040 in. max deep, 2 grooves 0.063 in. W by 0.047 in. deep and 0.016 in. W by 0.005 in. min to 0.010 in. max deep, cutter 1.000 in. dia, right side | Hamilton Sundstrand Corporation (99167) | |
| 02-14849 0214849 | 2915-00-941-6386 | Support, Fuel Pump | III End Item Identification: Aircraft engine fuel control, P/N 022664-021-06 General Characteristics Item Description: Material bar, cast W/30 percent lead bronze, O/a dim. 1.9985 in. min to 1.9990 in. max dia, edged to straight surface on bottom, by 1.125 in. min to 1.130 in. max lg, 0.967 in. min to 0.977 in. max inside dia, 1.3410 in. min to 1.3415 in. max small end dia, flange approx 0.125 in. min to 0.130 in. max thk W/3 holes 0.188 in. dia by 0.030 in. min to 0.040 in. max deep, 2 grooves 0.063 in. W by 0.047 in. deep and 0.016 in. W by 0.005 in. min to 0.040 in. max deep, cutter 1.000 in. dia | Hamilton Sundstrand Corporation (99167) | |
| 02-14855 0214855 | 2915-00-941-6592 | Seat, Inlet Valve, Fuel Control | III End Item Identification: TF30-P-1 aircraft engine fuel afterburner pump P/N 024536-202-04 | Hamilton Sundstrand Corporation (99167) | |
| 02-14859 0214859 | 2915-00-941-6593 | Retainer, Seal, Fuel Control | III End Item Identification: TF30-P-1 aircraft engine fuel afterburner pump P/N 024536-202-04 | Hamilton Sundstrand Corporation (99167) | |
| 02-14875-02 021487502 | 2915-00-889-9466 | Poppet, Valve, Fuel | III End Item Identification: Fuel pump P/N 024536-206 General Characteristics Item Description: Steel per MIL-S-6709 or AMS6470 1.609 in. lg | Hamilton Sundstrand Corporation (99167) | |
| 02-14881 0214881 | 2915-00-941-9593 | Liner, Inlet Valve, High Pressure | III End Item Identification: TF30-P-1 aircraft engine fuel afterburner pump P/N 024536-202-04 | Hamilton Sundstrand Corporation (99167) | |
| 02-14911-02 021491102 | 2915-00-113-0946 | Coupling, Govenor Drive | General Characteristics Item Description: Steel, one end splined, 9 extenal splines, pressure angle 30 deg, majordia 0.2436 in. nom, minor dia 0.2318 in. min, 0.2398 in. max, pitch DIA0.2812 in. nom, 5620 in. lg of splines, one end 8 internal teeth, pressureangle 45 deg, major dia 0.1958 in. min, 0.2028 in. max, minor dia 0.1878, pitch dia 0.1667 in. nom, 0.307 in. min, 0.312 in. max O/a dia, 1.275 in.min, 1.280 in. max O/a lg | Hamilton Sundstrand Corporation (99167) | |
| 02-14911-03 021491103 | 2915-01-017-5165 | Coupling, Pump | Hamilton Sundstrand Corporation (99167) | ||
| 02-14912 0214912 | 2915-00-941-9596 | Shaft, Inducer, Fuel Control | III End Item Identification: TF30-P-1 aircraft engine fuel afterburner pump P/N 024536-202-04 | Hamilton Sundstrand Corporation (99167) | |
| 02-14970-01 021497001 | 2915-01-187-0310 | Shaft, Drive | Hamilton Sundstrand Corporation (99167) | ||
| 02-14971 0214971 | 2915-00-088-0933 | Nozzle, Spray | Hamilton Sundstrand Corporation (99167) | ||
| 02-14973 0214973 | 2915-00-088-0938 | Retainer, Seal | Hamilton Sundstrand Corporation (99167) | ||
| 02-14981 0214981 | 2915-00-943-1734 | Guide, Filter Cover | Hamilton Sundstrand Corporation (99167) | ||
| 02-14982 0214982 | 2915-00-947-4556 | Filter Element, Fluid | III Fsc Application Data: Fuel control, engine, acft Media for Which Designed: Fuel/oil, hydrocarbon Style Designator: A6 cylindrical W/out container | Hamilton Sundstrand Corporation (99167) | |
| 02-14983 0214983 | 2915-00-940-9399 | Retainer, Filter, Fuel Control | General Characteristics Item Description: Material aluminum alloy, anodized finish, O/a dim. 3.848 in. dia by 1.518 in. min to 1.533 in. max, 2.120 in. min to 2.130 in. max small end dia | Hamilton Sundstrand Corporation (99167) | |
| 02-14987 0214987 | 2915-00-932-2051 | Insert, Wear, Drive Shaft | III End Item Identification: Aircraft engine fuel pump assembly, axial piston, P/ns 024692-106-18, 024692-109-18, 025285-101-01, 025285-103-01 and 102-1193 General Characteristics Item Description: Material metal | Hamilton Sundstrand Corporation (99167) |