31 July 2011 C1 CIVIL AVIATION DEPARTMENT HONG KONG ...

pitch propeller.* 6.3 Piston engines in Aeroplanes.Piston engines not exceeding 500 kW (670 bhp) inAeroplanes/Rotorcraft/Airships.* 6.3.1 Piston engines, in Aeroplanes not exceeding 2730 kg MTWA.* 6.4 Jet-turbine engines in Aeroplanes not exceeding 22.25 kN (5000 lbf) staticthrust including where so endorsed the associated APU installations.* 6.5 Propeller turbine engines in aeroplanes including, where so endorsed, theassociated APU installations:-Garret Airesearch TPE 331* 6.6 Jet turbine engines, in aeroplanes, exceeding 22.25 kN (5000 lbf) static thrustincluding where so endorsed the associated APU installation.7 Certification Privileges - Rotorcraft* 7.1 Piston-engined rotorcraft.7.2 Reserved.* 7.3 Turbine-engined rotorcraft not exceeding 2730 kg MTWA.NOTE: This paragraph includes the Allison 250 and Turbomeca Arriel engines. For anengine annotated #, removal/replacement of main casings including those whoseremoval results in concurrent removal of a rotating assembly from the engine,provided this is accomplished solely by disconnecting at the casing flanges. Nodismantling of main rotating assemblies is permitted.* 7.4 Sikorsky S76 with Turbomeca Arriel #NOTE: For an engine annotated #, removal/replacement of main casings including thosewhose removal results in concurrent removal of a rotating assembly from the engine,provided this is accomplished solely by disconnecting at the casing flanges. Nodismantling of main rotating assemblies is permitted.8 Certification Privileges - Instruments(a)A Rating granted in relation to any of the sub-paragraphs 8.1 to 8.4 inclusive,includes all of the instruments fitted to those aircraft in which are installedsystems defined by or listed in that sub-paragraph excluding those aircraftlisted in paragraph 14, and as limited by paragraph 3 of this Notice.30 September 2008 AN-10 P.4