Airworthiness Manual Advisory (AMA)

Appendix A

Figure A-i

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

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

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
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))

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