Appendix A
Minimum rated engine power P1min in kilowatts, for fixed-wing aircraft with maximum take-off mass of 900 kg
(Reference paragraph 4(b)(4))
Note: Due to inaccuracies in interpolating the above chart, the formula may be used for demonstrating compliance at maximum take-off masses below 500kg.
Figure A-ii
Minimum rated engine power P1min in kilowatts, for fixed-wing aircraft with maximum take-off mass of 900 to 1800 kg (Reference paragraph 4(b)(4))
Figure A-iii
Minimum rated engine power p2min in brake horsepower, for fixed-wing aircraft with maximum take-off mass of 0 to 2000 lb
(Reference paragraph 4(b)(4))
Note: Due to inaccuracies in interpolating the above chart, the formula may be used for demonstrating compliance at maximum take-off masses below 500kg
Figure A-iv
Minimum rated engine power P1min in brake horsepower, for fixed-wing aircraft with maximum take-off mass of 2000 to 4000 kg (Reference paragraph 4(a)(4))