Thanks Merv, but you won't see much from me , I hate typing. Did mean to ask you what Terry thought of it???
Macnoz, thanks, that would mean empty at about 325kg - better load then too.
Skydog, some J230 (factory built LSA NVFR version) Flight Manual numbers for you:
the following are RPM, litres/hr, TAS:
2600, 15, 100
2700, 18, 107
2800, 23, 110 - 75%
2850, 25, 115
2900, 28, 116
We tend to use 2700 RPM to limit fuel burn (& noise) - we are often wt limited to around 70 liters (empty wt 376.6 kg).
If a clean J230/ J400 will go close to VNE on 6 cylinders, why go looking for 8? I assume the 140+ / 150+ figures are TAS at altitude on a warm day - VNE is 140 KIAS.
Handling: most seem to prefere it over the J160 - climb is good but can get hot - so increase IAS, visibility better (more back windows - less stress in a busy CCT), landing not quirky - Glide & Vref 65 KIAS (same as J160) but stall lower - 40 & 45 KIAS. BUT all this for more $ so tends not to be the basic trainer which is probably a pity. Cockpit seems narrower - is this real or imagined??
Ultralights, J160 figures may vary because flying school ACFT may have bigger jets in the carby to improve cooling.