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:
Ilyushin Il-96
Table title:
Specifications
Table:
<table id='hittask' contenteditable='False'>
<tr> <th colspan=1 rowspan=1 > Measurement </th><th colspan=1 rowspan=1 > Il-96-300 </th><th colspan=1 rowspan=1 > Il-96M </th><th colspan=1 rowspan=1 > Il-96T </th><th colspan=1 rowspan=1 > Il-96-400 </th></tr>
<tr> <td colspan=1 rowspan=1 > Length </td><td colspan=1 rowspan=1 > 55.3 m (181 ft 7 in) </td><td colspan=1 rowspan=1 > 64.7 m (212 ft 3 in) </td><td colspan=2 rowspan=1 > 63.939 m (209 ft 9.28 in) </td></tr>
<tr> <td colspan=1 rowspan=1 > Span </td><td colspan=4 rowspan=1 > 60.11 m (197 ft 3 in) </td></tr>
<tr> <td colspan=1 rowspan=1 > Wing area </td><td colspan=4 rowspan=1 > 350 m² (3767.9 ft²) </td></tr>
<tr> <td colspan=1 rowspan=1 > Wing sweep </td><td colspan=4 rowspan=1 > 30° </td></tr>
<tr> <td colspan=1 rowspan=1 > Flaps/Slats </td><td colspan=4 rowspan=1 > I – 2°/3° (275 KIAS), II 3°/25° (264 KIAS), III – 10°/25° (243 KIAS), IV – 25°/25° (210 KIAS) for Takeoff, V – 40°/25° (189 KIAS) for Landing </td></tr>
<tr> <td colspan=1 rowspan=1 > Cabin width </td><td colspan=4 rowspan=1 > 5.70 m (18.70 ft) </td></tr>
<tr> <td colspan=1 rowspan=1 > Fuselage Diameter </td><td colspan=4 rowspan=1 > 6.08 m (19.94 ft) </td></tr>
<tr> <td colspan=1 rowspan=1 > Height </td><td colspan=4 rowspan=1 > 15.7 m (57 ft 7 in) </td></tr>
<tr> <td colspan=1 rowspan=1 > Operating Empty Weight </td><td colspan=1 rowspan=1 > 120,400 kg (265,198 lb) </td><td colspan=1 rowspan=1 > 132,400 kg (291,630 lb) </td><td colspan=1 rowspan=1 > 116,400 kg (256,387 lb) </td><td colspan=1 rowspan=1 > 122,300 kg (269,383 lb) </td></tr>
<tr> <td colspan=1 rowspan=1 > Max. Zero Fuel Weight </td><td colspan=1 rowspan=1 > 180,000 kg (403,000 lb) </td><td colspan=1 rowspan=1 >  </td><td colspan=1 rowspan=1 > 208,400 kg (459,030 lb) </td><td colspan=1 rowspan=1 >  </td></tr>
<tr> <td colspan=1 rowspan=1 > Max. Landing Weight </td><td colspan=1 rowspan=1 > 183,000 kg (403,083 lb) </td><td colspan=1 rowspan=1 > 220,000 kg (484,581 lb) </td><td colspan=1 rowspan=1 > 220,000 kg (484,581 lb) </td><td colspan=1 rowspan=1 > 220,000 kg (484,581 lb) </td></tr>
<tr> <td colspan=1 rowspan=1 > Max. Take-off Weight </td><td colspan=1 rowspan=1 > 250,000 kg (551,000 lb) </td><td colspan=1 rowspan=1 > 270,000 kg (595,000 lb) </td><td colspan=1 rowspan=1 > 270,000 kg (594,713 lb) </td><td colspan=1 rowspan=1 > 265,000 kg (583,700 lb) </td></tr>
<tr> <td colspan=1 rowspan=1 > Max. Payload </td><td colspan=1 rowspan=1 > 40,000 kg (88,105 lb) </td><td colspan=1 rowspan=1 > 58,000 kg (127,753 lb) </td><td colspan=1 rowspan=1 > 92,000 kg (202,643 lb) </td><td colspan=1 rowspan=1 > 58,000 kg (127,753 lb) </td></tr>
<tr> <td colspan=1 rowspan=1 > Takeoff Run at MTOW </td><td colspan=1 rowspan=1 > 2,340 m (7,677 ft) </td><td colspan=1 rowspan=1 > 3,000 m (9,843 ft) </td><td colspan=1 rowspan=1 > 2,700 m (8,858 ft) </td><td colspan=1 rowspan=1 > 2,700 m (8,858 ft) </td></tr>
<tr> <td colspan=1 rowspan=1 > Landing Run </td><td colspan=1 rowspan=1 > 860 m (2,821 ft) </td><td colspan=1 rowspan=1 > 1,800 m (5,906 ft) </td><td colspan=1 rowspan=1 > 1,650 m (5,511 ft) </td><td colspan=1 rowspan=1 > 1,650 m (5,511 ft) </td></tr>
<tr> <td colspan=1 rowspan=1 > Cruising speed </td><td colspan=4 rowspan=1 > 0.78 to 0.84 Mach or 850 to 870 km/h TAS (459 to 469 KTAS) </td></tr>
<tr> <td colspan=1 rowspan=1 > Maximum speed (Vmo) </td><td colspan=4 rowspan=1 > 0.84 Mach or 900 km/h IAS (485 KIAS) </td></tr>
<tr> <td colspan=1 rowspan=1 > Service ceiling </td><td colspan=4 rowspan=1 > 13,100 m (43,000 Ft) </td></tr>
<tr> <td colspan=1 rowspan=1 > Cruise Altitude </td><td colspan=4 rowspan=1 > 9,000 to 12,000 m (29,527 to 39,370 Ft) </td></tr>
<tr> <td colspan=1 rowspan=1 > Range with max. payload </td><td colspan=1 rowspan=1 > 11,500 km (6,209 nmi) </td><td colspan=1 rowspan=1 > 12,800 km (6,907 nmi) </td><td colspan=1 rowspan=1 > 5,000 km (2,699 nmi) </td><td colspan=1 rowspan=1 > 10,000 km (5,400 nmi) </td></tr>
<tr> <td colspan=1 rowspan=1 > Range with max. fuel </td><td colspan=1 rowspan=1 > 13,500 km (7,289 nmi) </td><td colspan=1 rowspan=1 > 15,000 km (8,100 nmi) </td><td colspan=1 rowspan=1 > 12,000 km (6,479 nmi) </td><td colspan=1 rowspan=1 > 12,000 km (6,479 nmi) </td></tr>
<tr> <td colspan=1 rowspan=1 > Max. Fuel capacity </td><td colspan=4 rowspan=1 > 152,620 l (40,322 US gal) </td></tr>
<tr> <td class="highlighted"  colspan=1 rowspan=1 > Engines (x4) </td><td colspan=1 rowspan=1 > Aviadvigatel PS-90A </td><td colspan=1 rowspan=1 > Pratt & Whitney PW2037 </td><td colspan=1 rowspan=1 > Pratt & Whitney PW2337 or Aviadvigatel PS-90A1 </td><td class="highlighted"  colspan=1 rowspan=1 > Aviadvigatel PS-90A1 </td></tr>
<tr> <td colspan=1 rowspan=1 > Thrust (x4) </td><td colspan=1 rowspan=1 > PS-90A: 156.9 kN (35,242 lb) N2:10,425 RPM </td><td colspan=1 rowspan=1 > 170.1 kN (38,250 lb) N2:12,360 RPM </td><td colspan=1 rowspan=1 > PW2337: 166.8 kN (37,500 lb) N2:12,360 RPM </td><td colspan=1 rowspan=1 > PS-90A1: 170.7 kN (38,326 lb) </td></tr>
<tr> <td colspan=1 rowspan=1 > Engine Dry Weight (x4) </td><td colspan=1 rowspan=1 > 2,950 kg (6,497 lb) </td><td colspan=1 rowspan=1 > 3,314 kg (7,300 lb) </td><td colspan=1 rowspan=1 > PW2337: 3,314 kg (7,300 lb) </td><td colspan=1 rowspan=1 > 2,950 kg (6,497 lb) </td></tr>
<tr> <td colspan=1 rowspan=1 > Cockpit crew </td><td colspan=1 rowspan=1 > Three </td><td colspan=2 rowspan=1 > Two </td><td colspan=1 rowspan=1 > Two (op. Three) </td></tr>
<tr> <td colspan=1 rowspan=1 > 3-class Seating capacity </td><td colspan=1 rowspan=1 > 237 </td><td colspan=1 rowspan=1 > 307 </td><td colspan=1 rowspan=1 >  </td><td colspan=1 rowspan=1 > 315 </td></tr>
<tr> <td colspan=1 rowspan=1 > 2-class Seating capacity </td><td colspan=1 rowspan=1 > 263 </td><td colspan=1 rowspan=1 > 340 </td><td colspan=1 rowspan=1 >  </td><td colspan=1 rowspan=1 > 386 </td></tr>
<tr> <td class="highlighted"  colspan=1 rowspan=1 > 1-class Seating capacity </td><td colspan=1 rowspan=1 > 300 </td><td colspan=1 rowspan=1 > 420 </td><td colspan=1 rowspan=1 >  </td><td class="highlighted"  colspan=1 rowspan=1 > 436 </td></tr>
<tr> <td colspan=1 rowspan=1 > Cargo Capacity </td><td colspan=1 rowspan=1 > F.H.1: 9,000 kg (Front) F.H.2: 15,000 kg (Back) F.H.3: 1,000 kg (Back) 6 LD3 (front) 10 LD3 (Rear) </td><td colspan=1 rowspan=1 >  </td><td colspan=1 rowspan=1 > 580 m³ main deck 114 m³ front lower deck 82 m³ rear lower deck 18 LD3 (Front) 14 LD3 (Rear) </td><td colspan=1 rowspan=1 > 114 m³ front lower deck 82 m³ rear lower deck 18 LD3 (Front) 14 LD3 (Rear) </td></tr>
</table>
Question:
What kind of engines and first-class seating are found on the Ilyushin Il-96 400?
Answer:
Ilyushin Il-96 400 is powered by four Aviadvigatel PS-90A1 and can carry up to 436 first class passengers.