Non-Aircraft Engine Electrical System Components: 519833-1, 5199A, 51A10505C
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 519833-1 5198331 | 2920-01-112-9344 | Cover, Pump pad | III End Item Identification: Nha starter, engine; fscm 70210; pn 519892-1-1; nsn 2920-01-011-5789, E/I A10 hi press fuel sys General Characteristics Item Description: Matl 0.063 sht al aly 2024 QQ-A-250/4 cond T351OR al aly 6061 QQ-A-250/11 cond T6, 3 holes 0.210 in. dia III Fsc Application Data: Engine electrical system components, nonaircraft | Honeywell International Inc. (70210) | |
| 519858-5 5198585 | 2920-01-257-4718 | Starter, Engine, Electrical | Special Features: 13.92 in.O/a; 4.52 in. dia.; 1 neg. 3/16-24 UNF-2A thd; 2 ground terminals 3/25-24 UNF-3A thd; motor duty cycle 1 min. on 6 mins. off Voltage in Volts: 18.0 Shaft Rotation Direction: Clockwise | Honeywell International Inc. (70210) | |
| 519858-6 5198586 | 2920-01-356-9139 | Starter, Engine, Electrical | III End Item Identification: U/O apu installation, C-17 acft Special Features: 13.920 in. LG;4.600 in dia. minusthe terminals;positive terminal 3/8-24UNF-2A thread per federal handbook H28, torque tolerance of terminal nuts 75-80 in. lbs;negative terminal 5/16-24 UNF-2A thread per federal handbook H28, torque tolerance of terminal nuts 50-55 in. lbs;ground terminals 2 each 3/25-24 UNJF-3A thread per MIL-S-8879;NOMINAL performance DATA:5.0 H.P., 6500 rpm, 18 volts D.C., 300 amps | Honeywell International Inc. (99193) | |
| 519858-7 5198587 | 2920-01-481-2346 | Starter, Engine, Electrical | III End Item Identification: A310-222 airbus | Honeywell International Inc. (70210) | |
| 519858-8 5198588 | 2920-01-513-7801 | Starter, Engine, Electrical | III End Item Identification: Aircraft, airbus, A310 Special Features: Subassembly is JT9D-7R4 engine | Honeywell International Inc. (70210) | |
| 519892-2-1 51989221 | 2920-01-036-6617 | Starter, Engine, Electrical | III End Item Identification: Apu A-10 acft; U/O GTCP36-50 | Honeywell International Inc. (70210) | |
| 519892-2-2 51989222 | 2920-01-040-5042 | Starter, Engine, Electrical | III End Item Identification: Apu A-10 acft; U/O GTCP36-50 III Part Name Assigned By Controlling Agency: Motor, engine starter, electrical | Honeywell International Inc. (70210) | |
| 519892-3-3 51989233 | 2920-01-112-9308 | Motor, Engine Starter, Electrical | III End Item Identification: APU-A10 aircraft; used on GTCP36-50 Shaft Rotation Direction: Clockwise single end Terminal Type and Quantity: 4 threaded stud | Honeywell International Inc. (99193) | |
| 519892-4 5198924 | 2920-01-112-9308 | Motor, Engine Starter, Electrical | III End Item Identification: APU-A10 aircraft; used on GTCP36-50 Shaft Rotation Direction: Clockwise single end Terminal Type and Quantity: 4 threaded stud | Honeywell International Inc. (99193) | |
| 519892-4-1 51989241 | 2920-01-180-0453 | Starter, Engine, Electrical | III End Item Identification: Aviation ground power unit (ag-pu) (including electrical dc 28 V at 700 amp maximum; AC=115-230 V, 30 kv at 400 hz maximum; AC=110, 60HZ zt 500 W maximum; HYDRAULIC--3, 300 lb at 15 gpm maximum; PNEUDRAULIC--60 lb pm at 40 psi maximum) | Honeywell International Inc. (70210,99193) | |
| 519892-5 5198925 | 2920-01-112-9308 | Motor, Engine Starter, Electrical | III End Item Identification: APU-A10 aircraft; used on GTCP36-50 Shaft Rotation Direction: Clockwise single end Terminal Type and Quantity: 4 threaded stud | Honeywell International Inc. (70210) | |
| 519892-5-1 51989251 | 2920-01-180-0453 | Starter, Engine, Electrical | III End Item Identification: Aviation ground power unit (ag-pu) (including electrical dc 28 V at 700 amp maximum; AC=115-230 V, 30 kv at 400 hz maximum; AC=110, 60HZ zt 500 W maximum; HYDRAULIC--3, 300 lb at 15 gpm maximum; PNEUDRAULIC--60 lb pm at 40 psi maximum) | Honeywell International Inc. (70210) | |
| 519892-6 5198926 | 2920-01-441-5383 | Starter, Engine, Electrical | Shaft Rotation Direction: Clockwise | Honeywell International Inc. (70210) | |
| 519892-6-1 51989261 | 2920-01-460-1346 | Starter, Engine, Electrical | III End Item Identification: Aircraft, challenger 604 | Honeywell International Inc. (70210) | |
| 519896-3 5198963 | 2920-01-411-3999 | Motor, Engine Starter, Electrical | III End Item Identification: Pacer dawn;attaches to gearbox | Honeywell International Inc. (99193) | |
| 5199 | 2920-00-691-9891 | Cable Assy, Special | Champion Aerospace LLC (0AFL4) Ryan Equipment Co. Inc. (0AF14) | ||
| 5199295 | 2920-01-286-0054 | Impeller, Non-Aircra | MTU Detroit Diesel Inc. (72582) | ||
| 5199324 | 2920-00-353-4815 | Drive, Engine, Electrical Starter | Special Features: For use on 0.625 in. max dia shaft, secured by no. 6 woodruff key, 10 tooth pinion, 1.575 in. od, 1.375 in. pd, ccw rotation 9002A2 Overall Length: 4.520 inches minimum and 4.630 inches maximum Largest Outside Diameter: 2.060 inches nominal | MTU Detroit Diesel Inc. (72582) | |
| 5199A | 2920-00-691-9892 | Cable Assy, Special | Champion Aerospace LLC (0AFL4) Ryan Equipment Co. Inc. (0AF14) | ||
| 51A10505C | 2920-00-358-7577 | Regulator, Engine Generator | Mounting Hole Diameter: 0.250 inches nominal Mounting Style: 2 three hole triangular Radio Interference Shielding: Not provided | Ford Motor Co. (23040) |