Item__20_ELA-T-38_AC_Loading_TO_data-ECM_Pod.xlsx
XLSX spreadsheet 19 KB Posted
- Attached to
- T-38A/B and A-10 Automatic Dependent Surveillance-Broadcast (ADS-B) Federal contract opportunity
- Solicitation number
- FA822017R0001
About this file
AC Loading
View the file
Other files for this federal contract opportunity
Show all 26
On GovTribe
Work with this file on GovTribe
- Download the original file
- Contacts named in this file
- Similar government files
- Ask GovTribe AI about this file
Text version
Sheet1 Data extracted from the 2002 updated T.O. # 1T-38A-2-7 (page 2-7). Judgement of separtation of items by flight conditions then made.
| RIGHT GENERATOR BUS LOAD DISTRIBUTION | |||||||||||
| Phase A Power in VA's | Phase B Power in VA's | Phase C Power in VA's | |||||||||
| SYSTEM | T-Off / Land | Cruise | Pre-Flight | SYSTEM | T-Off / Land | Cruise | Pre-Flight | SYSTEM | T-Off / Land | Cruise | Pre-Flight |
| Left Flap Actuator | 575 | Left Flap Actuator | 816 | Left Flap Actuator | 690 | ||||||
| Right Flap Actuator | 575 | Right Flap Actuator | 816 | Right Flap Actuator | 690 | ||||||
| Right Fuel Pump | 380 | 380 | 380 | Right Fuel Pump | 380 | 380 | 380 | Right Fuel Pump | 380 | 380 | 380 |
| Instr pwr Seat | 553 | Eng Ign, R Autosyn inst | 257 | ||||||||
| Radio Trans Relay | 40 | 40 | 40 | Flood & | 111 | Right Fuel Qty | 35 | 35 | 35 | ||
| Utility Light | 15 | Nose Equip Cooling | 658 | ||||||||
| Nose Equipment Cooling |
alva.maynor: alva.maynor:
If TCTo 1T-38-655 is not accomplished.
alva.maynor: alva.maynor:
If TCTO 1T-38-655 not accomplished
| AN/ARN-118 | 515 | |||
| Student Pwr Seat & | 553 | |||
| Elect Test | 40 |
| T/R #2 | 256 | 256 | 256 | T/R #2 | 256 | 256 | 256 | T/R #2 | 256 | 256 | 256 | |
| Bus Monitor | 40 | 40 | 40 | Bus Monitor | 40 | 40 | 40 | Bus Monitor | 40 | 40 | 40 | |
| Cabin Air Valves | 183 | Pitot Heater | 300 | Oxy Qty & | 102 | |||||||
| Canopy Seal | 58 | Attitude Gyro | 167 | Cabin Cond | 67 | |||||||
| Eng Anti-ice | 430 | Attitude Ind Flt Comp | 80 | Attitude Gyro | 129 | |||||||
| Rate Gyro, Attitude Gyro | 129 | Caution & Warning Ind | 70 | |||||||||
| Trim Cntrl | 50 | |||||||||||
| 1866 | 1566 | 1649 | 0 | 2308 | 1904 | 1486 | 2749 | 1079 | 711 |
| LEFT GENERATOR BUS LOAD DISTRIBUTION. | |||||||||||
| Phase A Power in VA's | Phase B Power in VA's | Phase C Power in VA's | |||||||||
| Position Lights | 275 | 275 | 275 | Landing-Taxing Lamp | 1002 | Beacon Light | 126 | ||||
| console light | 38 | 38 | 38 | Landing-Taxing Lamp Cntrl | 248 | Inst Light | 63 | ||||
| left fuel pump | 380 | 380 | 380 | Left Fuel Pump | 380 | 380 | 380 | Left Fuel Pump | 380 | 380 | 380 |
| T/R #1 | 256 | 256 | 256 | T/R #1 | 256 | 256 | 256 | T/R #1 | 256 | 256 | 256 |
| Bus Mon | 40 | 40 | 40 | Bus Mon | 40 | 40 | 40 | Bus Mon | 40 | 40 | 40 |
| Angle of Attack Heater | 140 | Angle-attack comp | 44 | AN/APX-64 AIMS | 84 | 84 | 84 | ||||
| Aims Comp | 45 | 45 | 45 | ||||||||
| Left Fuel Qty, Autosyn inst | 132 | 132 | 132 | Stability Augmenter | 10 | Stability Augmenter | 42 | ||||
| ECM Power | 575 | ECM Power | 575 | ECM Power | 575 | ||||||
| 1121 | 1836 | 1121 | 1926 | 1305 | 676 | 994 | 1422 | 805 | |||
| Total Right Gen | 1866 | 1566 | 1649 |
alva.maynor: alva.maynor:
TCTO 1T-38-655 accomplished alva.maynor: alva.maynor:
If TCTO 1T-38-655 accomplished alva.maynor: alva.maynor:
If TCTo 1T-38-655 is not accomplished.
alva.maynor: alva.maynor:
If TCTO 1T-38-655 not accomplished
| 0 | 2308 | 1904 | 1486 | 0 | 2749 | 1079 | 711 | |||||||
| Total Left Gen | 1121 | 1836 | 1121 | 0 | 1926 | 1305 | 676 | 0 | 994 | 1422 | 805 | |||
| 2987 | 3402 | 2770 | 0 | 4234 | 3209 | 2162 | 0 | 3743 | 2501 | 1516 | ||||
| AC power consumed | ||||||||||||||
| Based on T/Rs loading | Total AC Load T-off/Land (VA) | 10964 | Total Load if ECM Active | 12689 | ||||||||||
| = (Amps DC)(28)/.9 | Total AC Load Cruise (VA) | 9112 | ||||||||||||
| = ( 25 A )( 28V ) /0.91 | Total AC Load Taxi (VA) | 6448 | Total Load if ECM Active | 8173 | ||||||||||
| = 778 VA total 3-phases |
ECM Power requirements based on max current draw of 5 amps per phase
File details come from the government source that posted it. Updated .