The following standards apply to turboprop engines with rated output at or above 1,000 kW:
SN = 187·rO-0.168
40 C.F.R. §1031.40
The following standards apply to turboprop engines with rated output at or above 1,000 kW:
SN = 187·rO-0.168
40 C.F.R. §1031.40