Page 152 - Aeronautical Engineer Data Book

36 089 0.75 3307 0.196 0.61 1.373 3197 3 1+1L 6I 7HP 1HP 1IP 3LP

35 000 0.85 11813 0.195 ISA+10 0.57 3.175 2.192 9670 3 1LP 7IP 6HP 1HP 1IP 3LP

35 000 0.8 2550 0.184 0.69 2.59 1.52 2951 2 1+3LP 12HP 2HP 3LP

35 000 0.82 11500 0.162 ISA+10 0.565 3.912 2.474 10 550 3 1LP 8IP 6HP 1HP 1IP 4LP

35 000 0.83 4.869 2.845 13 700 2 1+6LP 11HP 2HP 7LP

35 000 0.8 4.143 2.535 14 350 2 1+5LP 11HP 2HP 5LP

35 000 0.8 3.879 2.477 9400 2 1+4LP 11HP 2HP 4LP

35 000 0.8 3.879 2.477 9400 2 1+4LP 11HP 2HP 4LP

35 000 0.8 5725 0.174 ISA+10 0.574 3.204 1.681 5230 2 1+4LP 10HP 2HP 5LP

35 000 0.8 5185 0.2 ISA+10 0.574 3.204 1.681 5252 2 1+4LP 10HP 2HP 5LP

35 000 0.83 0.545 5.181 3.404 16 644 2 1+3LP 10HP 2HP 6LP

0.562 4.343 2.794 10 726 2 1+4LP 14HP 2HP 5LP

2.616 1.245 1670 2 1F +14cHP 2HP 4LP

35 000 0.8 0.545 2.616 1.945 5700 2 1+4LP 9HP 1HP 5LP

40 000 0.8 1310 0.645 2.514 1.219 1325 2 1+5LP +1CF 2HP 3LP

0.414 1.62 1.272 1385 2 various 2HP 2LP

Cruise Altitude (ft) Mach number Thrust (lb) Thrust lapse rate Flat rating (°C) SFC (lb/hr/lb) Dimensions Length (m) Fan diameter (m) Basic eng. weight (lb) Layout Numbe