CTHRepealedLegislation
AD/ENG/4 Amdt 10 - Piston Engine Continuing Airworthiness Requirements
Take-off power shall be:Take-off power shall be:
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Take-off power shall be:
i. For a fixed pitch propeller aircraft - static RPM.
ii. For a constant speed propeller, normally aspirated engine aircraft, take-off power shall be maximum RPM at a manifold pressure, not less than 2” of static manifold pressure.
iii. For a turbocharged/supercharged engine aircraft, take-off power shall be maximum RPM at the manifold pressure detailed in the aircraft flight manual.