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:
General Electric CF6
Table title:
Specifications
Table:
<table id='hittask' contenteditable='False'>
<tr> <th colspan=1 rowspan=1 > Variant </th><th colspan=1 rowspan=1 > CF6-6 </th><th colspan=1 rowspan=1 > CF6-50 </th><th colspan=1 rowspan=1 > CF6-80A </th><th colspan=1 rowspan=1 > CF6-80C2 </th><th colspan=1 rowspan=1 > CF6-80E1 </th></tr>
<tr> <th colspan=1 rowspan=1 > Type </th><td colspan=5 rowspan=1 > Dual rotor, axial flow, high bypass ratio turbofan, annular combustor </td></tr>
<tr> <th colspan=1 rowspan=1 > Compressor </th><td colspan=1 rowspan=1 > Fan & 1LP + 16HP </td><td colspan=2 rowspan=1 > Fan & 3LP + 14HP </td><td colspan=2 rowspan=1 > Fan & 4LP + 14HP </td></tr>
<tr> <th colspan=1 rowspan=1 > Turbine </th><td colspan=1 rowspan=1 > 2HP + 5LP </td><td colspan=2 rowspan=1 > 2HP + 4LP </td><td colspan=2 rowspan=1 > 2HP + 5LP </td></tr>
<tr> <th colspan=1 rowspan=1 > Length </th><td colspan=1 rowspan=1 > 188 in (478 cm) </td><td colspan=1 rowspan=1 > 183 in (465 cm) </td><td colspan=1 rowspan=1 > 167 in (424 cm) </td><td colspan=2 rowspan=1 > 168 in (427 cm) </td></tr>
<tr> <th colspan=1 rowspan=1 > Diameter </th><td colspan=3 rowspan=1 > 105 in (267 cm) </td><td colspan=1 rowspan=1 > 106 in (269 cm) </td><td colspan=1 rowspan=1 > 114 in (290 cm) </td></tr>
<tr> <th colspan=1 rowspan=1 > Blade Count </th><td colspan=4 rowspan=1 > 38 </td><td colspan=1 rowspan=1 > 34 </td></tr>
<tr> <th colspan=1 rowspan=1 > Takeoff thrust </th><td colspan=1 rowspan=1 > 41,500 lbf 185 kN </td><td colspan=1 rowspan=1 > 51,500–54,000 lbf 229–240 kN </td><td class="highlighted"  colspan=1 rowspan=1 > 48,000–50,000 lbf 210–220 kN </td><td colspan=1 rowspan=1 > 52,200–61,960 lbf 232.2–275.6 kN </td><td colspan=1 rowspan=1 > 65,800–69,800 lbf 293–310 kN </td></tr>
<tr> <th colspan=1 rowspan=1 > Pressure ratio </th><td colspan=1 rowspan=1 > 25–25.2 </td><td colspan=1 rowspan=1 > 29.2–31.1 </td><td colspan=1 rowspan=1 > 27.3–28.4 </td><td colspan=1 rowspan=1 > 27.1–31.8 </td><td colspan=1 rowspan=1 > 32.4–34.8 </td></tr>
<tr> <th colspan=1 rowspan=1 > Bypass ratio </th><td colspan=1 rowspan=1 > 5.76–5.92 </td><td colspan=1 rowspan=1 > 4.24–4.4 </td><td colspan=1 rowspan=1 > 4.59–4.66 </td><td colspan=1 rowspan=1 > 5–5.31 </td><td colspan=1 rowspan=1 > 5–5.1 </td></tr>
<tr> <th colspan=1 rowspan=1 > Max. power TSFC </th><td colspan=1 rowspan=1 > 0.35 lb/lbf/h 9.9 g/kN/s </td><td colspan=1 rowspan=1 > 0.368–0.385 lb/lbf/h 10.4–10.9 g/kN/s </td><td colspan=1 rowspan=1 > 0.355–0.357 lb/lbf/h 10.1–10.1 g/kN/s </td><td colspan=1 rowspan=1 > 0.307–0.344 lb/lbf/h 8.7–9.7 g/kN/s </td><td colspan=1 rowspan=1 > 0.332–0.345 lb/lbf/h 9.4–9.8 g/kN/s </td></tr>
<tr> <th colspan=1 rowspan=1 > Application </th><td colspan=1 rowspan=1 > DC-10-10 </td><td colspan=1 rowspan=1 > B747, DC-10-15/30 A300 </td><td class="highlighted"  colspan=1 rowspan=1 > A310, B767 </td><td colspan=1 rowspan=1 > A300/310, B747-400 B767, MD-11, C-5M </td><td colspan=1 rowspan=1 > A330 </td></tr>
<tr> <th colspan=1 rowspan=1 > TCDS </th><th colspan=1 rowspan=1 > CF6-6 </th><th colspan=1 rowspan=1 > CF6-50 </th><th colspan=1 rowspan=1 > CF6-80A </th><th colspan=1 rowspan=1 > CF6-80C2 </th><th colspan=1 rowspan=1 > CF6-80E1 </th></tr>
<tr> <th colspan=1 rowspan=1 > Weight </th><td colspan=1 rowspan=1 > 8,176 lb 3,709 kg </td><td colspan=1 rowspan=1 > 8,825–9,047 lb 4,003–4,104 kg </td><td colspan=1 rowspan=1 > 8,760–8,776 lb 3,973–3,981 kg </td><td colspan=1 rowspan=1 > 9,480–9,860 lb 4,300–4,470 kg </td><td colspan=1 rowspan=1 > 11,225 lb 5,092 kg </td></tr>
<tr> <th colspan=1 rowspan=1 > Max. LP RPM </th><td colspan=1 rowspan=1 > 3,810 </td><td colspan=1 rowspan=1 > 4,102 </td><td colspan=1 rowspan=1 > 4,016 </td><td colspan=1 rowspan=1 > 3,854 </td><td colspan=1 rowspan=1 > 3,835 </td></tr>
<tr> <th colspan=1 rowspan=1 > Max. HP RPM </th><td colspan=1 rowspan=1 > 9,925 </td><td colspan=1 rowspan=1 > 10,761 </td><td colspan=1 rowspan=1 > 10,859 </td><td colspan=1 rowspan=1 > 11,055 </td><td colspan=1 rowspan=1 > 11,105 </td></tr>
<tr> <th colspan=1 rowspan=1 > Thrust-to-weight ratio </th><td colspan=1 rowspan=1 > 5.08 </td><td colspan=1 rowspan=1 > 5.84–5.97 </td><td colspan=1 rowspan=1 > 5.48–5.7 </td><td colspan=1 rowspan=1 > 5.51–6.28 </td><td colspan=1 rowspan=1 > 5.86–6.22 </td></tr>
</table>
Question:
What is the thrust range of the CF6-80A and to which aircraft is is applicable?
Answer:
The CF6-80A has a thrust of 48,000 to 50,000 lb, which is applicable for Airbus A310.