Please read the following table in HTML format from a webpage and then answer the question in detail according to the table. Each table cell is defined by a <td> and a </td> tag. Each table row starts with a <tr> and ends with a </tr> tag. 'rowspan=m' and 'colspan=n' represents a cell spaning over 'm' rows and 'n' columns.

Webpage title:
Beechcraft King Air
Table title:
Specifications
Table:
<table id='hittask' contenteditable='False'>
<tr> <th colspan=1 rowspan=1 > King Air </th><th colspan=1 rowspan=1 > C90GTi </th><th colspan=1 rowspan=1 > B100 </th></tr>
<tr> <td colspan=1 rowspan=1 > Crew </td><td colspan=2 rowspan=1 > 1–2 </td></tr>
<tr> <td colspan=1 rowspan=1 > Passengers </td><td colspan=1 rowspan=1 > 7 max </td><td colspan=1 rowspan=1 > 13 max </td></tr>
<tr> <td colspan=1 rowspan=1 > Length </td><td colspan=1 rowspan=1 > 35 ft 6 in / 10.82 m </td><td colspan=1 rowspan=1 > 39 ft 11 in / 12.17 m </td></tr>
<tr> <td colspan=1 rowspan=1 > Span </td><td colspan=1 rowspan=1 > 50 ft 3 in / 15.32 m </td><td colspan=1 rowspan=1 > 45 ft 11 in / 14.0 m </td></tr>
<tr> <td colspan=1 rowspan=1 > Height </td><td colspan=1 rowspan=1 > 14 ft 3 in / 4.34 m </td><td colspan=1 rowspan=1 > 15 ft 5 in / 4.7 m </td></tr>
<tr> <td colspan=1 rowspan=1 > Area </td><td colspan=1 rowspan=1 > 294 ft² / 27 m² </td><td colspan=1 rowspan=1 > 279.7 ft² / 26.0 m² </td></tr>
<tr> <td colspan=1 rowspan=1 > Empty Weight </td><td colspan=1 rowspan=1 > 6,950 lb / 3,150 kg </td><td colspan=1 rowspan=1 > 7,092 lb / 3,212 kg </td></tr>
<tr> <td colspan=1 rowspan=1 > MTOW </td><td colspan=1 rowspan=1 > 10,100 lb / 4,580 kg </td><td colspan=1 rowspan=1 > 11,800 lb / 5,352 kg </td></tr>
<tr> <td colspan=1 rowspan=1 > Powerplant </td><td class="highlighted"  colspan=1 rowspan=1 > 2xPT6A-135A </td><td colspan=1 rowspan=1 > 2xTPE-331-6-251B or -252 </td></tr>
<tr> <td colspan=1 rowspan=1 > Power </td><td class="highlighted"  colspan=1 rowspan=1 > 550/ 410 kW </td><td colspan=1 rowspan=1 > 715 shp / 533 kW </td></tr>
<tr> <td colspan=1 rowspan=1 > Propellers </td><td colspan=1 rowspan=1 > Hartzell HC-E4N-3N </td><td colspan=1 rowspan=1 > 4-bladed </td></tr>
<tr> <td colspan=1 rowspan=1 > Cruise TAS </td><td colspan=1 rowspan=1 > 226 kn / 416 km/h </td><td colspan=1 rowspan=1 >  </td></tr>
<tr> <td colspan=1 rowspan=1 > Max TAS </td><td colspan=1 rowspan=1 > 270 kn / 500 km/h </td><td colspan=1 rowspan=1 > 265 kn / 491 km/h </td></tr>
<tr> <td colspan=1 rowspan=1 > Stall IAS (flaps down) </td><td colspan=1 rowspan=1 > 78 kn / 145 km/h </td><td colspan=1 rowspan=1 >  </td></tr>
<tr> <td colspan=1 rowspan=1 > Range </td><td colspan=1 rowspan=1 > 1,321 nmi / 2,446 km </td><td colspan=1 rowspan=1 > 1,325 nmi / 2,455 km </td></tr>
<tr> <td colspan=1 rowspan=1 > Fuel consumption </td><td colspan=1 rowspan=1 >  </td><td colspan=1 rowspan=1 > 2.08 lb/nmi (0.51 g/m) </td></tr>
<tr> <td colspan=1 rowspan=1 > Ceiling </td><td colspan=1 rowspan=1 > 30,000ft / 9,144 m </td><td colspan=1 rowspan=1 > 24,850 ft / 7,574 m </td></tr>
<tr> <td colspan=1 rowspan=1 > Climb rate </td><td colspan=1 rowspan=1 > 2,000 ft/min / 10.2 m/s </td><td colspan=1 rowspan=1 > 2,140 ft/min / 10.87 m/s </td></tr>
<tr> <td colspan=1 rowspan=1 > Wing loading </td><td colspan=1 rowspan=1 > 34.3 lb/ft² / 170 kg/m² </td><td colspan=1 rowspan=1 > 42.2 lb/ft² / 205.84 kg/m² </td></tr>
<tr> <td colspan=1 rowspan=1 > Power/weight </td><td colspan=1 rowspan=1 > 0.099 hp/lb / 179 W/kg </td><td colspan=1 rowspan=1 > 0.121 hp/lb / 199.17 W/kg </td></tr>
</table>
Question:
What engine was the C90GT fitted with and how much power did it make?
Answer:
The C90GT was fitted with PT6A-135As and 550 shp (410 kW).