The following standards apply to new turbofan or turbojet aircraft engines with rated output at or below 26.7 kN thrust that are installed in subsonic aircraft:
SN = 83.6·rO-0.274
40 C.F.R. §1031.50
The following standards apply to new turbofan or turbojet aircraft engines with rated output at or below 26.7 kN thrust that are installed in subsonic aircraft:
SN = 83.6·rO-0.274
40 C.F.R. §1031.50